List of Contents - ICAS 2016 · 1 List of Contents Welcome from ICAS and KSAS Presidents 2 ICAS Organization and Committees 4 ICAS 2016 Local Organizing Committee 6 ICAS Member Societies

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List of Contents

Welcome from ICAS and KSAS Presidents 2 ICAS Organization and Committees 4 ICAS 2016 Local Organizing Committee 6 ICAS Member Societies & Associates 7 Programme & Session Overview 11 Detailed Technical Programme 13 List of Standby and Poster papers 23 Technical Tours 33 Social Programme 35 General Information 36 Accommodation 40 Tour Information 43 Travel 48

Welcome to 30th ICAS Congress in DAEJEON, KOREA!

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Welcome from the President of the International Council of the Aeronautical Sciences

For over 55 years now, the International Council of the Aeronautical Sciences (ICAS) has provided for the world’s aerospace engineers, scientists, technologists and managers, the pre-eminent forum to present

and discuss the latest developments in aeronautics. This remarkable apolitical organization founded by Theodore von Kármán and his international colleagues, continues to build on its impressive heritage, to be even more relevant to the global aerospace industries. This world congress staged biennially by ICAS is the key opportunity for those committed to serving those industries to meet, present, discuss and create opportunities that can only be done in such an international environment.

The pace of technological developments and the diversity of business challenges facing those working in aeronautics are greater than ever today. The knowledge, skills, facilities and finance necessary to progress our profession and associated businesses are no longer found in one place or even close to home. Therefore, in such an environment with seemingly limitless availability of unfiltered information from a diversity of sources, ICAS Congresses represent unique opportunities every two years to learn and interact with the leaders in the field from around 40 countries.

The topics addressed at ICAS Congresses are typically diverse and reflections of the challenges and opportunities of the day. The

foundations of the industry, the aeronautical disciplines of aerodynamics and performance, stability and control, materials and structures, and propulsion and systems, always feature strongly, however every Congress brings new topics. In recent times, there has been considerable growth in sessions on air traffic management and systems, manufacturing and the supply chain, safety and security, and of course the environment and operations. As we prepare for the next Congress, it is clear that there will again be increased focus on unmanned air vehicles and systems, and operational challenges for the global air transport system.

It is therefore with great pleasure that we

ICAS President Dr. Christian Mari

We look forward to receiving your paper and to welcoming you in Daejeon in 2016.

invite you to consider participating in the 30th ICAS Congress, and at this time, to commence the preparation of a paper detailing your most important work conducted over the past two-year period. As a guide to authors, the list of ICAS 2016 topic headings is appended. However, this list should not be regarded as exhaustive and papers from other relevant areas were welcome.

The 30th ICAS Congress is to be held in Daejeon, and this is the first time the Congress will be held in Korea. Following the great success of the most recent Congress held in St. Petersburg, Russia, for which a record number of papers were submitted, we anticipate that there will be very strong interest in participating in this next historic meeting.

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Welcome from the President of KSAS (Korean Society for Aeronautical and Space Sciences)

As the president of the Korean Society for Aeronautical and Space Sciences (KSAS), I would like to warmly invite you to attend the 30th Congress of the International Council of the Aeronautical Sciences in Daejeon, Korea, Sep. 25–30, 2016.

The 30th ICAS Congress will be a fantastic and memorable event. Since the first ICAS congress at Madrid in 1958, ICAS has been growing and gaining recognition in the field of aeronautics and related technologies. The KSAS and

the local organizing committee will continue this legacy and provide the best ever experience with industry experts and researchers worldwide.

The ICAS Congress will be held at the Daejeon Convention Center (DCC), located at next to Gapcheon River which crosses the heart of Daejeon. From its conception in the 1970s as a R&D innovation cluster, INNOPOLIS Daedeok has been leading the advancement of Korean science and technology via the support of government policy, government research institutes, academics and industries.

I look forward to seeing you in Daejeon!

Warm Regards,

Dr. In Hee Hwang

President, The Korean Society for Aeronautical and Space Sciences (KSAS)

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ICAS Organization and Committees

THE INTERNATIONAL COUNCIL OF THE AERONAUTICAL SCIENCES

ICAS was founded by Theodore von Karman in 1957 as a non-government not-for-profit scientific organization to encourage the free international exchange of information on aeronautical research and technology. The mission of ICAS is to provide regularly scheduled events and publications that enable a better understanding of engineering science and practice and an improved level of cooperation among aeronautical engineering professionals from around the world. ICAS currently serves as the only international support organization to representative aeronautical engineering professional societies and their members in 30 countries. ICAS functions under three primary bodies: Council (meets biennially), Executive Committee (meets at least twice each year) and Programme Committee (meets annually). ICAS holds an International Congress in the fields of Aeronautical Sciences on a biennial basis. The venue is chosen by the Council and changes from Congress to Congress. Furthermore ICAS organizes a thematic workshop in the year between the congresses in connection with the meeting of the Program Committee. ICAS COUNCIL Representatives of Member Societies

C. Bil, Australia H. Deconinck, Belgium E. Belo, Brazil Y. Z. Zhang, P.R. of China A. Pistek, Czech Republic M. Kanerva, Finland B. Stoufflet, France J. Szodruch, Germany T. Tsitinidis, Greece J. Rohacs, Hungary H: Bhatia, India H. Djojodihardjo, Indonesia O. Rand, Israel S. Ricci, Italy

K. Rinoie, Japan S. Lee, Korea C.Hermanns, The Netherlands Z. Goraj, Poland L. Campos, Portugal D. Prunario,, Romania S. Chernyshev, Russia B. Rasuo, Serbia J. Monk, South Africa M. Olivier, Spain R. Karlsson, Sweden J. Wildi, Switzerland R. Parker, United Kingdom S. Magnus, U.S.A.

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ICAS EXECUTIVE COMMITTEE Officers President: C. Mari, France P.C. Chair: S. Ying, U.S.A. Treasurer: G. Holmberg, Sweden Past President: M. Scott, Australia Executive Secretary: A. Probst, Germany

Members C. Atkin, United Kingdom J. Azevedo, Brazil A. Filatyev, Russia F. Abbink, The Netherlands D. Mavris, U.S.A. M. Peters, The Netherlands S. Suzuki, Japan R. Henke, Germany J. Cho, Korea (ICAS 2016)

ICAS SECRETARIAT The ICAS Secretariat is hosted by the Deutsche Gesellschaft für Luft-und Raumfahrt (DGLR) and located in Bonn, Germany. Axel Probst is the ICAS Executive Secretary and is assisted by Bodo Heinrichs as the ICAS Coordinator. Address: ICAS Secretariat, c/o DGLR, D-53175 BONN, Germany Phone: +49-(0)228-30805-0, Fax: +49-(0)228-30805-24, E-mail: [email protected]

ICAS PROGRAMME COMMITTEE All members of ICAS Programme Committee are listed on the ICAS Web-Site. Below are listed those who took part in the preparation meeting for ICAS 2016.

Abbink, Fred Fu, Yongling Mari, Christian Rinoie, Kenichi

Amiryants, Gennady Gao, Zhenghong Mavris, Dimitri Scott, Murray Atkin, Chris Goraj, Zdobyslaw Melkert, Joris Stoufflet, Bruno Azevedo, Joao Götzendorf, Tomasz Michaut, Christiane Stumpf, Eike Bayandor, Javid Gustafsson, Anders Mirzoyan, Artur Sun, Jian Belo, Eduardo Han, Jae-Hung Monk, John Suzuki, Shinji Bigarella, Enda Harigae, Masatoshi Müller-Wiesner, Detlef Szodruch, Joachim Bil, Cees Haselbach, Frank Ogilvie, Frank Toebben, Helmut Breitsamter, Christian Holmberg, Gunnar Persiani, Franco Ueda, Tetsuhiko Cho, Jinsoo Isikveren, Askin Peters, Michel Voevodenko, Nina Collier, Fayette Itoh, Eri Pistek, Antonin Wan, Tung del Rosario, Ruben Karneva, Mikko Poll, Ian Ying, Susan Djojodihardjo, Harijono Kim, Youdan Rand, Omri Zan, Steve Filyatjev, Alexander Kimmel, Bill Rein-Weston, Karl Zhang, Xinguo Fredriksson, Billy Krus, Petter Remy, Sebastien Zhang, Y. Z. Fu, Song Manfriani, Leonardo Ricci, Sergio

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ICAS 2016 Local Organizing Committee Chair Youdan Kim (Seoul National Univ.)

Administrative Advisor Min Jea Tahk (KAIST) Dae Sung Lee (KARI)

General Secretary Soo-Seok Yang (KARI)

Operations & Logistics Kwanjung Yee (Seoul National Univ.)

Finance & Contracts Chang-Kyung Ryoo (Inha Univ.)

Public Relations & Media Sangkyung Sung (Konkuk Univ.)

Local Arrangement Hong-Gye Sung (Korea Aerospace Univ.) Jae-Hung Han (KAIST) Seungkeun Kim (Chungnam National Univ.)

Exhibition & Sponsorship Taekyu Reu (ADD) Ji Hong Kim (KAI)

Local Secretariat Hyoun Jin Kim (Seoul National Univ.) Wongi Kang (KSAS) Jongmin Hong (Genicom Co., Ltd.)

Industrial Committee Members Sangbeom Kim (Hanwha Corporation) Jaekeun Song (UCON System) Hong Dae Kim (Korean Air) Chul Moon Yum (LIGNex1) Jaeho Choi (Hanwha Techwin)

ICAS 2016 Local Secretariat

Genicom Co., Ltd.

2F, 927 Tamnip-dong, Yuseong-gu, Daejeon, Korea 34036

Email: [email protected] / Fax: +82-42-472-7459

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ICAS Member Societies & AssociatesICAS MEMBER SOCIETIES

616 69 Brno

Finland The Finnish Association of Graduate Engineers TEK Ratavartijankatu 2 00520 Helsinki France AAAF - Association Aéronautique et Astronautique de France 6, rueGalilée 75782 Paris Cedex 16 Germany DGLR - Deutsche Gesellschaft für Luft und Raumfahrt Godesberger Allee 70 53175 Bonn Greece HAES - Hellenic Aeronautical Engineers Society 3, Karitsi Street 10561 Athens Hungary GTE - Scientific Society of Mechanical Engineers PO Box 433 1371 Budapest India AeSI - Aeronautical Society of India 13-B, Indra Pasthra Estate New Dehli - 110002 Indonesia IAAI - Institute of Aeronautics and Astronautics Indonesia Institut Teknologi Bandung JalanGanesha 10 40132 Bandung

Israel Israel Society of Aeronautics and Astronautics PO Box 2956 Tel-Aviv 61028 Italy AIDAA - Associazione Italiana Di Aeronautica e Astronautica Casella Postale 227 00187 Roma V. R. Japan JSASS - Japan Society for Aeronautics and Space Sciences MeikouBldg. Bekkan, 1-18-2 Shinbashi Minato-ku Tokyo 105 Korea KSAS - Korean Society for Aeronautical and Space Sciences #635-4, Yeogsam-dong, Gangnam-gu, Seoul 135-703 Poland Polish Society of Aerospace Sciences c/o Warsaw University of Technology ul. Nowowiejska 24 00-665 Warsaw Portugal CCTAE - Centro de Ciencias e Tecnologias Aeronauticas e Espaciasis Av. Rovisco Pais 1069 Lisboa Cedex

ChinaCSAA - Chinese Society of Aeronautics and Astronautics No.2 Beiyuan, Andingmenwai Chaoyang District, Beijing 100012 Post Box 761-2, Beijing Czech Republic CSM - Czech Society for Mechanics c/o Brno University of Technology Institute for Aerospace Engineering Engineering Technicka 2

Australia The Royal Aeronautical Society - Australian Division PO Box 573 Mascot, NSW 2020 Belgium Royal Flemish Association of Engineers c/o Technological Institute, Aeronautical Section Desguinlei 214 BE-2018 Antwerpen Brazil ABCM - Associação Brasileira de Engenharia e Ciencias Mecanicas Av. Rio Branco, Centro 20040-001 Rio de Janeiro

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ICAS MEMBER SOCIETIES (CONT.)

Romania Commission d'Astronautique de l'Académie de Roumanie 125 Calea Victoriei S.1 71102 Bucuresti Russian Federation TsAGI - Central Aerohydrodynamic Institute 1, Zhukovski Street Zhukovski Moscow Region 140160 Republic of Serbia Serbian Aerospace Society c/o Faculty of Mechanical Engineering, University of Belgrade, Kraljice Marije 16, 11120 Belgrade 35

Republic of South Africa AeSSA - Aeronautical Society of South Africa P.O. Box 14717 Sinoville 0129 Spain Asociación de Ingenieros Aeronáuticos de España, AIAE C/ Francisco Silvela, 71 28028 Madrid Sweden SSAA - Swedish Society of Aeronautics and Astronautics PO Box 4207 17154 Solna Switzerland SvFW - Schweizerische Vereinigung Für Flugwissenschaften c/o RUAG Aerospace CH-6032 Emmen

The Netherlands NVvL - The Netherlands Association of Aeronautical Engineers Anthony Fokkerweg 2, 1059 CM, Amsterdam United Kingdom RAeS - Royal Aeronautical Society 4 Hamilton Place London W1V 0BQ United States AIAA - American Institute of Aeronautics and Astronautics 1801 Alexander Bell Drive Suite 500 Reston, VA, 20091

ICAS ASSOCIATES

Canada Aerospace NRC Montreal Road, Ottawa, Ontario, K1A 0R6 China AASRC - Taiwan, China Room R3-211,No.300, Jhongda Rd., Jhongli City, Taoyuan County 320

CAE - Chinese Aeronautical Establishment P.O. Box 761, No.2 Anwai, Beiyuan Beijing 100012

COMAC - Commercial Aircraft Corporation of China, Ltd. Zhang Yang Road 25, Shanghai 200120

China (cont.) The Hong Kong University of Science and Technology Clear Water Bay, Kowloon, Hong Kong Czech Republic VZLU - Aeronautical Research and Test Institute Beranovych 130, 199 05 Praha – Letnany France ONERA - French Aeronautics and Space Research Center BP 72, 92322 ChatillonCedex

SAFRAN 2 bd du Général Martial Valin 75724 Paris Cedex 15

Australia Advanced Composite Structures Australia198 Lorimer Street, Port Melbourne, Victoria 3207

DST Group - Defence Science and Technology Group 506 Lorimer Street, Fishermans Bend, Victoria 3207 Belgium VKI - Von Kàrmàn Institute for Fluid Dynamics Chaussée de Waterloo 72, 1640 Rhode – St. Genese Brazil Embraer S.A. Av. Brigadeiro Faria Lima, 2.170 12227-901 – São José dos Campos – SP

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ICAS ASSOCIATES (CONT.)

Germany DLR - German Aerospace Center Linder Höhe, 51147 Köln

Bauhaus Luftfahrt e.V. Willi-Messerschmitt.Str. 1, 85521 Ottobrunn

Munich Aerospace e.V. Willi-Messerschmitt. Str. 1, 82024 Taufkirchen Italy C.I.R.A. Via Maiorise 81043 Capua (CE)

University of Naples Department of Aerospace Engineering Via Claudio, 21, 80125 Napoli Japan JAXA - Institute of Aeronautical Technology (IAT) 7-44-1 Jindaiji-higashimachi, Chofu, Tokyo 182-8522

ENRI - Electronic Navigation Research Institute 7-42-23 Jindaiji-higashi-machi, Chofu, Tokyo 182-0012 Lithuania Vilniaus Gedimino technikos universitetas - VGTU Saulėtekioalėja 11,Vilnius 10223 Malaysia University Putra Malaysia 4th Floor, Administrative Building 43400 UPM Serdang, Selangor Pakistan Institute of Space Technology 1, Islamabad Highway, Islamabad 44000

Poland ILOT - INSTITUTE OF AVIATION Al. Krakowska 110/114 02-256 Warsaw Russia CIAM - Central Institute of Aviation Motors 2, Aviamotornaya St. 111116 Moscow

MAI - Moscow Aviation Institute 4 Volokolamskoyeshosse 125993 Moscow

Russian Academy of Engineering Moscow Republic of South Africa CSIR - DPSS PO Box 395 Pretoria 0001 Spain INTA Institutional Relations Directorate Carretera de Ajalvir Km.4 28850 Torrejon de Ardoz Sweden SAAB AB SE-58188 Linköping

FOI - Swedish Defence Research Agency SE-16490 Stockholm The Netherlands Airbus Group N.V. PO Box 32008 2303 DA Leiden

NLR - National Aerospace Laboratory PO Box 90502 1006 BM Amsterdam

United Kingdom Rolls-Royce PO Box 31 Derby DE24 8BJ

Poll Aerosciences 114 High Street Cranfield - Bedfordshire - MK43 0DG United States The Boeing Company WEO&T Enterprise Technology Strategy, External Technical Affiliations P.O. Box 3707, MC 03-FR Seattle, WA 98124-2207

Honda Aircraft Company 6430 Ballinger Rd Greensboro, NC 27410

Monday, 26. Sep 2016

07:00-08:00 Registration (ICAS-2016-0.1)

08:00-09:00 Opening ceremony (ICAS-2016-0.2)

09:00-10:00 ICAS DANIEL & FLORENCE GUGGENHEIM MEMORIAL LECTURE - Chair: Mari C. ICAS President FR Seung Jo Kim, Design, Development and Flight test of Vertical Take-Off and Landing UAV, Cyclocopter (ICAS-2016-0.3)

10:00-10:30 Break

10:30-12:00 1.1 Unconventional

Aircraft

2.1 Fluid-Structure

Interaction

3.1 Experiments in Flow Control

4.1 Super- and Hypersonic

Aerodynamics 1

5.1 Avionics & Real Time Monitoring

6.1 Structural

System Design

7.1 Advanced Engines 1

8.1 Flight Control 1

9.1 UAV Control 1

10.1 Experiments on Basic

Flows

11.1 Network

Operations

12.1 ISABE 1

12:00-13:00 Lunch

13:00-14:30 1.2 MDO Application

2.2 Vortical Flows

3.2 Intake

Aerodynamics

4.2 Super- and Hypersonic

Aerodynamics 2

5.2 Thermal Modeling

6.2 Loads

7.2 Advanced Engines 2


9.2 UAV Control 2

10.2 Synthetic Jets

11.2 Formation Flight

12.2 Experimental

14:30-15:00 Break

15:00-18:00 General Lecture 1 - Chair: Mari C. ICAS President FR tbd, CTO Discussion (ICAS-2016-0.4)

Tuesday, 27. Sep 2016

08:00-09:00

09:00-10:00 Poster presentations (ICAS-2016-0.6)

10:00-12:00 1.3 Design Method 1

2.3 CFD Applications

1

3.3 Wing

Aerodynamics

4.3 Vortical Flow

5.3 Operations &

Sustainment 1

6.3 Structural Design

1 SHELLS

7.3 Fan &

Compressors: MDO


9.3 UAV Test & Integration

10.3 Flow Separation and

Control

11.3 Airport Capacity

12.3 Vehicle

Optimization and Design

12:00-13:00 Lunch

13:00-13:45 ICAS \"PAUL KEUK CHANG\" LECTURE FOR INNOVATION IN AERONAUTICS - Chair: Suzuki Shinji PPSC Chair JP Gregg Pyers, The JSF Lift System (ICAS-2016-0.7)

14:00-15:30 1.4

Innovative Concept-Super Heavy Cargo

2.4 CFD Applications

2

3.4 Wind Tunnel Technology

4.4 Propeller/Wing Aerodynamics

5.4 Landing Gear &

Taxiing


2 BLADES

7.4 Hybrid / Electric

Propulsion

8.4 Flight

Optimization

9.4 UAV Design

Configuration 1

10.4 Lateral Jets

11.4 Environment

Friendly Operations

12.4 Estimation and

Testing

15:30-16:00 Break

16:00-18:00 1.5

Education 2.5

High AOA and Unsteady

Aerodynamics

3.5 Flow

Visualisation 1

4.5 Special Topics

5.5 Modeling and

Tests of Systems & Subsystems 1


3

7.5 Turbines

8.5 Flight Dynamics & Identification

9.5 Operations & Sustainment 2

10.5 Transition Forcing and

Control

11.5 History of

Aeronautics

12.5 Boundary Layer

Asymptotic Analysis

18:00-19:30 Airbus Fly your Ideas student challenge (ICAS-2016-0.8)

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General Lecture 2 Kenji Yoshida, D-SEND#2 - Flight tests for low sonic boom design technology (ICAS-2016-0.5)

Wednesday, 28. Sep 2016

08:00-09:00 GENERAL LECTURE 3 Ed Crawley, Complex System Architecture (ICAS-2016-0.9)

09:00-09:30 Break

09:30-12:00 1.6 Design Method 2

2.6 Current

Developments in CFD

3.6 High

Lift/Multielement Aerodynamics

4.6 Design

Optimization 1

5.6 Advanced Materials

6.6 Aeroelasticity 1

7.6 Inlet, Fan and Compressors

8.6 Handling Quality

9.6 UAV Nav & Operations

10.6 Hybrid-Electric and

Distributed Propulsion Aircraft 1

11.6 Flow

Management

12.6 Aircraft

Operations and Safety

12:00-13:00 Lunch

13:00-13:45 GENERAL LECTURE 4 - Chair: Fualdes Chantal tbd, Experience and Lessons of a full composite passenger aircraft development (ICAS-2016-0.10)

14:00-15:30

1.7 Design for

Uncertainty

2.7 CFD for Wind Tunnel Effects

3.7 Education in

Systems Engineering and

Integration

4.7 MAV-related

Aerodynamics

5.7 Operations &

Sustainment 3

6.7 Impact

7.7 Propeller

8.7 Flight Testing

9.7 UAV Design

Configuration 2

10.7 Reduced Order

Modeling

11.7 Noise & Emission

12.7 Icing & Jet

Engine Safety

15:30-16:00 Break

16:00-18:00 1.8

UAS 2.8

Hypersonic Aerodynamics

3.8 Flow

Visualisation 2

4.8 (Aerodynamic)

Control Methods

5.8 Damage

Tolerance


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7.8 System of

Systems Design & Operation

8.8 Flight Trajectory

Design

9.8 Modeling and

Tests of Systems & Subsystems 2

10.8 Shock Waves and

Control

11.8 Separation

Management

12.8 Humans in the

Loop

Thursday, 29. Sep 2016

08:00-09:30 GENERAL LECTURE 5 tbd, IFAR Plenary Lecture (ICAS-2016-0.11)

09:30-10:00 Break

10:00-12:30

1.9 Environmentally

Responsible Aviation

2.9 Turbulence

Modeling and Transition

3.9 Student Final

4.9 Design

Optimization 2

5.9 Fatigue and Corrosion

6.9 Aeroelasticity 2

7.9 Systems

Engineering & Integration

8.9 Hybrid-Electric and Distributed

Propulsion Aircraft 2

9.9 UAV

Collaborative Operations

10.9 Transsonic Buffet

Control

11.9 Trajectories

12.9 Safety &

Operations of Unmanned

Aircraft Systems 12:30-14:00 Lunch

14:00-15:30 1.10 High Speed and Access to Space

2.10 Space Vehicle Configurations

3.10 Scale Model

Flight Testing

4.10 HEXAFLY-INT

Project

5.10 ISABE 2

6.10 Structural Dynamics

7.10 Combustion and

High Speed

8.10 Flight Modeling &

Simulation

9.10 UAV Flight Dynamics

10.10 Hypersonic/Transitional

Boundary Layers

15:30-16:00 Break

16:00-17:00

17:00-17:30 CLOSING CEREMONY (ICAS-2016-0.13)

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VON KARMAN LECTURE - Chair: Susan Ying Chair ICAS Programme Committee CN Gordon McConnel, Didier Evard, The Airbus 350 XWB Programme (ICAS-2016-0.12)

0.1 07:00 - 08:00 Registration Chair:

07:00

0.2 08:00 - 09:00 Opening ceremony Chair:

08:00

0.3 09:00 - 10:00 ICAS DANIEL & FLORENCE GUGGENHEIM MEMORIAL LECTURE Chair: C. Mari ICAS President

09:00 Design, Development and Flight test of Vertical Take-Off and Landing UAV, Cyclocopter Seung Jo Kim

10:00 - 10:30 Break

1.1 10:30 - 12:00 Unconventional Aircraft

Chair: Wong, K.C., Sec. Chair: Rinoe, K. Track1

01 - Aircraft and Systems Integration 10:30 (1.1.1) UNCONVENTIONAL CONFIGURATIONS – DESIGN AND

OPTIMIZATION TGG Goetzendorf-Grabowski, Warsaw University of Technology, Poland

11:00 (1.1.2) INFLUENCE OF POWER UNIT CONFIGURATION LAYOUT OF A REGIONAL JET ON PERFORMANCE AND DIRECT OPERATING COST Z.J. Goraj, Warsaw University of Technology, Poland

11:30 (1.1.3) ON THE DESIGN OF A STRUT-BRACED WING CONFIGURATION IN A COLLBORATIVE DESIGN ENVIRONMENT D. Böhnke, DLR e.V., Germany

2.1 10:30 - 12:00 Fluid-Structure Interaction Chair: Lott, M., Sec. Chair: Wolkov, A.

Track 2 02.1 - Aerodynamics - CFD Methods and

Validation

10:30 (2.1.1) AERODYNAMIC AND STRUCTURAL ANALYSIS OF A BAT WING IN FLIGHT J Feaster, Virginia Tech, United States

11:00 (2.1.2) EFFECT OF ELASTIC DEFORMATION ON FLIGHT DYNAMICS OF PROJECTILES WITH LARGE SLENDERNESS RATIO RH,H Hua, Northwestern Polytechnical University, China

11:30 (2.1.3) COMPUTATIONAL INVESTIGATIONS OF MODEL WING DEFORMATION INFLUENCE ON AERODYNAMIC CHARACTERISTICS I.A. Kursakov, Russia

3.1 10:30 - 12:00 Experiments in Flow Control Chair: Consigny, H.

Track 3 02.2 - Experimental Aerodynamics

10:30 (3.1.1) WAKE CHARACTERISTICS OF VANE-TYPE VORTEX GENERATOR H. J Shim, KAIST, South Korea

11:00 (3.1.2) OPEN CAVITY FLOW CONTROL USING STEADY JETS N A al haddabi, university of Glasgow, United Kingdom

11:30 (3.1.3) EXPERIMENTAL INVESTIGATION OF WING LOAD CONTROL USING FLUIDIC DEVICES A. Krzysiak, Institute of Aviation, Poland

4.1 10:30 - 12:00 Super- and Hypersonic Aerodynamics 1 Chair: ,

Track 4 02.4 - Applied Aerodynamics

10:30 (4.1.1) THE EFFECT OF LEADING EDGE ROUNDING ON A CARET WAVERIDER CONFIGURATION AT MACH 8.2 S. A. Prince, Cranfield University, United Kingdom

11:00 (4.1.2) EFFECTS OF STEP HEIGHT AND POSITION ON THE FLOWFIELD STRUCTURE OF A HYPERSONIC FLOW OVER COMBINED GAP/STEP GEOMETRIES W. F. N. Santos, National Institute for Space Research (INPE), Brazil

11:30 (4.1.3) AEROTHERMODYNAMICS OF SHARP LEADING EDGE OF HYPERSONIC VEHICLE Huang fei, China

5.1 10:30 - 12:00 Avionics & Real Time Monitoring Chair: Huysseune, J., Sec. Chair: Ying, S.

Track 5 06 - Systems, Subsystems and

Equipment 10:30 (5.1.1) GENERAL MESSAGE RACES IN DATA DISTRIBUTION SERVICE

PROGRAMS FOR AIRBORNE SOFTWARE H.-J. Kim, Gyeongsang National University, South Korea

11:00 (5.1.2) A KNOWLEDGE-BASED REAL TIME MONITORING AND DIAGNOSITC APPROACH FOR AIRCRAFT BREAKING SYSTEM X.-C Chen, Shanghai Aircraft Customer Service Company, China

11:30 (5.1.3) AUTOMATIC CONTROL OF REDUNDANCY FOR A HETEROGENEOUS ONBOARD COMPUTER V.B. Bukov, JSC "Institute of Aircraft Equipment", Russia

6.1 10:30 - 12:00 Structural System Design Chair: Park, J., Sec. Chair:

Track 6 03.2 - Structural Analysis and Design, Structural

Dynamics, Aeroelasticity

Degenhardt, 10:30 (6.1.1) EVALUATION OF CONCEPTUAL DESIGN BASED ON

MANUFACTURED ACTUAL UNMANNED SOLAR PLANE N Arai, Tokai University, Japan

11:00 (6.1.2) NEW DESIGN SCENARIO FOR FUTURE COMPOSITE LAUNCHER STRUCTURES R Degenhardt, DLR, Germany

11:30 (6.1.3) MULTIDISCIPLINARY TOPOLOGY-BASED OPTIMIZATION IN DESIGN OF AIRCRAFT STRUCTURAL LAYOUTS K.A. Balunov, Central Aerohydrodynamic Institute (TsAGI), Russia

7.1 10:30 - 12:00 Advanced Engines 1 Chair: ,

Track 7 04 - Propulsion

10:30 (7.1.1) KEY TECHNOLOGIES FOR THE NEXT GENERATION OF CIVIL AIRCRAFT ENGINES F. Haselbach, Rolls-Royce plc, United Kingdom

11:00 (7.1.2) THE ROLLS-ROYCE PLC ULTRAFAN™ HEAT MANAGEMENT CHALLENGE M J Ryemill, Rolls-Royce plc, United Kingdom

11:30 (7.1.3) DEVELOPMENT OF TECHNOLOGY ADVANCE FOR FUTURE PROPULSION SYSTEMS OF HAUL AIRCRAFT A.I. Lanshin, CIAM, Russia

8.1 10:30 - 12:00 Flight Control 1 Chair: Che, J., Sec. Chair: Abbasi, H.

Track 8 05.1 - Flight Dynamics and Control (Control &

Modelling) 10:30 (8.1.1) AUGMENTED POLYNOMIAL GUIDANCE FOR TERMINAL VELOCITY

CONSTRAINT G.-H. Moon¹, S.-W. Shim¹, M.-J. Tahk¹; ¹KAIST, South Korea 11:00 (8.1.2) IMPACT ANGLE CONTROL GUIDANCE CONSIDERING GRAVITY

EFFECT H.-G. Kim, Seoul National University, South Korea 11:30 (8.1.3) TERMINAL IMPACT ANGLE AND ANGLE-OF-ATTACK CONTROL

GUIDANCE FOR SURFACE-TO-AIR MISSILE USING TVC S.-M. Hong, KAIST, South Korea

9.1 10:30 - 12:00 UAV Control 1 Chair: Maroney, D., Sec. Chair: Krus, P.

Track 9 05.2 - Flight Dynamics and Control (UAV

related) 10:30 (9.1.1) ADAPTIVE NEURAL NETWORK CONTROLLER DESIGN FOR

BLENDED-WING UAV WITH COMPLEX DAMAGE KIM KIJOON, South Korea 11:00 (9.1.2) MODELING AND CONTROL OF HIGHLY FLEXIBLE FLYING-WING

UAV WITH MULTIPLE ELEVONS AND PROPELLERS R Wang, Northwestern Polytechnical University, China

11:30 (9.1.3) ON SAFETY ASSESSMENT OF NOVEL APPROACH TO ROBUST UAV FLIGHT CONTROL IN GUSTY ENVIRONMENTS V Golubev, ERAU, United States

10.1 10:30 - 12:00 Experiments on Basic Flows Chair: Zhang, W., Sec. Chair: Manfriani, L.

Track 10 02.3 - Basic Fluid Dynamics and Flow

Control

10:30 (10.1.1) INFLUENCE OF A SURFACE FRACTAL MICROSTRUCTURE ON THE CHARACTERISTICS OF A TURBULENT BOUNDARY LAYER M.A. Brutyan, TsAGI, Russia

11:00 (10.1.2) GEOMETRIC ROUGHNESS EFFECTS ON THE AERODYNAMIC CHARACTERISTICS OF A SPINNING CYLINDER IN CROSSFLOW S. A. Prince, Cranfield University, United Kingdom

11:30 (10.1.3) STAGGERED THREE-DIMENSIONAL CAVITIES: POSSIBLE METHOD FOR SKIN FRICTION DRAG REDUCTION E. R. G Gowree, City University London, United Kingdom

11.1 10:30 - 12:00 Network Operations Chair: Jeon, D., Sec. Chair: Hoekstra, J.

Track 11 08 - Air Transport System Efficiency

10:30 (11.1.1) AN EXPLORATION OF EVOLUTION PATHS FOR AIR TRANSPORTATION NETWORKS J.-H. Lewe, Georgia Institute of Technology, United States

11:00 (11.1.2) A CLASSIFICATION SCHEME OF THE AIR TRANSPORTATION NETWORK RESEARCH K.-S. Song, Georgia Institute of Technology, United States

11:30 (11.1.3) IDENTIFICATION OF AIRPORT QUEUING FLIGHT AND PASSENGER DELAYS USING PASSING H Idris, Engility Corporation, United States

12.1 10:30 - 12:00 ISABE 1 Chair: , Track 12

10:30 (12.1.1) RTO\'S AND TECHNOLOGY DE-RISKING I.J. Potter, National Research Council Canada, Canada

12:00 - 13:00 Lunch

1.2 13:00 - 14:30 MDO Application

Chair: Prince, S., Sec. Chair: Ogilvie, F. Track1

01 - Aircraft and Systems Integration 13:00 (1.2.1) DEFINITION AND ASSESSMENT OF AEROELASTIC COUPLING

TECHNIQUES IN A COLLABORATIVE AIRCRAFT MDO ENVIRONMENT P.D. Ciampa, DLR, German Aerospace Center, Germany

13:30 (1.2.2) STRUCTURAL CONSTRAINTS INVESTIGATION IN WING AERODYNAMIC/STRUCTURAL OPTIMIZATION K.S. Zhang, Northwestern Polytechnical University, China

14:00 (1.2.3) MULTIDISCIPLINARY DESIGN OPTIMIZATION FOR FIGHTER AIRCRAFT CONFIGURATION C.L. Lee, Korea Aerospace Industries, LTD.,

13

South Korea 2.2 13:00 - 14:30 Vortical Flows

Chair: Winckelmanns, G., Sec. Chair: Stumpf, E.


Validation 13:00 (2.2.1) OPTIMIZATION OF CHINE-SHAPED FOREBODY OF AN AIRCRAFT IN

TERMS OF PROVIDING DIRECTIONAL STABILITY K. A. Makarov, TsAGI, Russia

13:30 (2.2.2) APPLICATION OF INCREMENTAL 4D VARIATIONAL DATA ASSIMILATION METHOD FOR WAKE TURBULENCE J.H. Cho, Seoul National University, South Korea

14:00 (2.2.3) LARGE-SCALE VORTEX STRUCTURE OF FLOW IN THE NEAR WAKE BEHIND AN AIRLINER DURING TAKEOFF AND LANDING Yu. M. Tsirkunov, Baltic State Technical University, Russia

3.2 13:00 - 14:30 Intake Aerodynamics Chair: Haselbach, F.


13:00 (3.2.1) INLET DUCT ENGINE TEST FACILITIES IN INDONESIA LOW SPEED TUNNEL (ILST) SB Subagyo, UPT-LAGG BPPT, Indonesia

13:30 (3.2.2) AERODYNAMIC TESTING OF HELICOPTER NOVEL AIR INTAKES F. Knoth, Institute of Aerodynamics and Fluid Mechanics, TU München, Germany

14:00 (3.2.3) KAI SURION HELICOPTER FULL-SCALE AIR INTAKE TESTING AT CIRA ICING WIND TUNNEL A.C. de Bruin, NLR, Netherlands

4.2 13:00 - 14:30 Super- and Hypersonic Aerodynamics 2 Chair: ,


13:00 (4.2.1) LOW-DRAG / LOW-BOOM SHAPE OPTIMIZATION OF A BIPLANE WING / TWIN-BODY FUSELAGE SST CONFIGURATION N. Ban, Nagaoka University of Technology, Japan

13:30 (4.2.2) AERODYNAMICS CAUSED BY ATTITUDE MOTION OF A SUPERSONIC FLIGHT EXPERIMENT VEHICLE WITH A CRANKED-ARROW MAIN WING K Mizobata, Muroran institute of Technology, Japan

14:00 (4.2.3) AERODYNAMIC CHARACTERISTICS OF BUSEMANN’S BIPLANE AIRFOIL FOR SUPERSONIC TRANSPORT AIRCRAFT WING AT VARIOUS AOA RO Bura, Faculty of Mechanical and Aerospace Engineering, ITB, Indonesia

5.2 13:00 - 14:30 Thermal Modeling Chair: Fu, Y., Sec. Chair: Dezzion, J.C.


Equipment 13:00 (5.2.1) FINITE ELEMENT ANALYSIS OF THERMOELECTRIC-

GALVANOMAGNETIC INTERACTIONS AND THEIR AEROSPACE APPLICATION S. Abouali Sanchez, Universitat Politècnica de València, Spain

13:30 (5.2.2) SPECIAL CONSIDERATIONS TO THERMAL BEHAVIOR MODELING AND SIMULATION OF AN AEROSPACE ELECTROMECHANICAL ACTUATION SYSTEM J FU, Beihang University, China

14:00 (5.2.3) COUPLED EMC-THERMAL MODELING OF ELECTRICAL HARNESSES WITHIN “MORE ELECTRICAL AIRCRAFT” F MAHIDDINI, ONERA, France

6.2 13:00 - 14:30 Loads Chair: Han, J., Sec. Chair: Pasyhev, S.


Dynamics, Aeroelasticity 13:00 (6.2.1) AERODYNAMIC LOAD SENSING FROM MEASURED STRAIN C.-g.

Pak, NASA Armstrong Flight Research Center, United States 13:30 (6.2.2) EPISTEMIC UNCERTAINTY QUANTIFICATION FOR MULTIFIDELITY

AEROELASTIC LOADS ANALYSIS B. Johnson¹, D. Mavris¹; ¹Georgia Institute of Technology, United States

14:00 (6.2.3) FLIGHT TESTING AN ADAPTIVE GUST LOADS ALLEVIATION ON A FLEXIBLE AIRCRAFT Y. Wang, China Academy of Aerospace Aerodynamics, China

7.2 13:00 - 14:30 Advanced Engines 2 Chair: Parker, R., Sec. Chair: Remy, S.


13:00 (7.2.1) MISSION BASED COMPARISON OF SINGLE- AND COUNTER-ROTATING FAN DESIGNS T. Otten, German Aerospace Center (DLR), Germany

13:30 (7.2.2) LBM APPLIED TO TURBOFAN FAN COMPARTMENT THERMAL LOADS MANAGEMENT AT GROUND IDLE OPERATING CONDITIONS T. FEDERICI, SAFRAN Snecma, France

14:00 (7.2.3) AERODYNAMIC OPTIMIZATION OF AIRPLANE PROPULSION SYSTEM WITHIN THE FRAMEWORK OF AGILE PROJECT K.S. Anisimov, TsAGI, Russia

8.2 13:00 - 14:30 Flight Control 2 Chair: Vian, J., Sec. Chair: Han-Lim, C.


Modelling) 13:00 (8.2.1) DESIGN AND TESTING OF A LOW-COST FLIGHT CONTROL

SYSTEM FOR UNSTABLE SUBSCALE RESEARCH AIRCRAFT A. Sobron, Linköping University, Sweden

13:30 (8.2.2) NONLINEAR MISSILE AUTOPILOT DESIGN USING CONTROL CONTRACTION METRICS BASED ON SUM-OF-SQUARES OPTIMIZATION H.-H. Kwon, KAIST, South Korea

14:00 (8.2.3) FLIGHT CONTROL LAW CLEARANCE USING WORST-CASE INPUTS J. Z. Ben-Asher, Aerospace Enginnering, Technion, Israel

9.2 13:00 - 14:30 UAV Control 2 Chair: Posse, C., Sec. Chair: Bil, C.


related) 13:00 (9.2.1) GUIDANCE AND CONTROL OF AUTOMATIC SHORT LANDING WITH

STEEP GLIDE SLOPE J.H.Moon Moon, KOREANAIR, South Korea 13:30 (9.2.2) NONLINEAR DYNAMIC INVERSION WITH NEURAL NETWORKS FOR

THE FLIGHT CONTROL OF A LOW COST TILT ROTOR UAV E. D'Amato, Second University of Naples, Italy

14:00 (9.2.3) DEPTH IMAGE BASED DIRECT SLAM FOR SMALL UAVS S.-Y. Park, KAIST, South Korea

10.2 13:00 - 14:30 Synthetic Jets Chair: Wood, N., Sec. Chair: Goraj, Z.


Control 13:00 (10.2.1) HIGH-BANDWIDTH PULSED ACTUATORS: DEVELOPMENT AND

APPLICATIONS IN HIGH-SPEED FLOWS P. Kreth, Florida Center for Advanced Aero-Propulsion, United States

13:30 (10.2.2) EXPERIMENTAL STUDY ON AERODYNAMIC LOAD CONTROL USING SYNTHETIC JET ACTUATORS H.W.M. Hoeijmakers, University of Twente, Netherlands

14:00 (10.2.3) INVESTIGATION OF SYNTHETIC JET ARRAY PERFORMANCE ON THE AERODYNAMICS OF THE WING A. Ali, Universiti Teknologi Malaysia, Malaysia

11.2 13:00 - 14:30 Formation Flight Chair: Jansen, J., Sec. Chair: Lundström, D.


13:00 (11.2.1) PLANNING AIR TEAM MISSIONS WITH MULTIPLE OBJECTIVES T. Erlandsson, University of Skövde, Sweden

13:30 (11.2.2) APPLYING REQUIRED NAVIGATION PERFORMANCE CONCEPT FOR TRAFFIC MANAGEMENT OF SMALL UNMANNED AERIAL SYSTEMS JW Jung, NASA, United States

14:00 (11.2.3) INFLUENCE OF AIRCRAFT TYPE AND ORDER ON FUEL SAVINGS GAINED BY TWO-AIRCRAFT FORMATIONS T. Marks, DLR Air Transportation Systems, Germany

12.2 13:00 - 14:30 Experimental Chair: Ricci, S., Sec. Chair: Djojodihardjo, H.


Dynamics, Aeroelasticity 13:00 (12.2.1) DEFORMATION MEASUREMENT IN THE WIND TUNNEL FOR AN

UAV LEADING EDGE WITH A MORPHING MECHANISM M. Radestock, German Aerospace Center, Germany

13:30 (12.2.2) SEMI-ACTIVE VIBRATION SUPPRESSION OF AIRCRAFT PANEL USING PIEZO-ACTUATORS WITH SYNCHRONIZED SWITCH DAMPING TECHNIQUE K LI, Aircraft strength research institute, China

14:00 (12.2.3) DESIGN, MANUFACTURING AND VALIDATION OF A GUST GENERATOR FOR WIND TUNNEL TEST OF A LARGE SCALE AEROELASTIC MODEL S. Ricci, Politecnico di Milano, DAER, Italy

14:30 - 15:00 Break

0.4 15:00 - 18:00 General Lecture 1 Chair: C. Mari ICAS President

15:00 CTO Discussion tbd

0.5 08:00 - 09:00 General Lecture 2 Chair:

0.6 09:00 - 10:00 Poster presentations Chair:

09:00 1.3 10:00 - 12:00 Design Method 1

Chair: Lee, D., Sec. Chair: Mavris, D. Track1

01 - Aircraft and Systems Integration 10:00 (1.3.1) KNOWLEDGE-BASED FUTURE COMBAT AIRCRAFT OPTIMIZATION

R.C Munjulury, Linköping university, Sweden 10:30 (1.3.2) COLLABORATIVE AIRCRAFT DESIGN USING AN INTEGRATED AND

DISTRIBUTED MULTIDISCIPLINARY PRODUCT DEVELOPMENT PROCESS E. Moerland, German Aerospace Center (DLR), Germany

11:00 (1.3.3) USING OPENVSP IN A CONCEPTUAL AIRCRAFT DESIGN ENVIRONMENT IN MATLAB S. Herbst, Institute of Aircraft Design, Technical University Munich, Germany

11:30 (1.3.4) INTEGRATED CONCEPTUAL DESIGN METHOD CONSIDERING ADVANCED AIRCRAFT SYSTEMS AND AIRCRAFT TRAJECTORY K. Rinoie, The University of Tokyo, Japan

14

08:00 D-SEND#2 - Flight tests for low sonic boom design technology Kenji Yoshida

2.3 10:00 - 12:00 CFD Applications 1

Chair: Rezende, O., Sec. Chair: Zhan, H.


Validation 10:00 (2.3.1) MAIN ROTOR-BODY ACTION FOR VIRTUAL BLADES MODEL A.N.

Kusyumov, KNRTU-KAI, Russia 10:30 (2.3.2) NUMERICAL SIMULATION OF 3D ICING BASED ON

UNSTRUCTURED GRIDS L ZHANG, Northwestern Polytechnical University, China

11:00 (2.3.3) ON THE SIMULATION OF 3-D FLAPPING-WING INSECT\'S FLIGHT PERFORMANCE UNDER ABNORMAL ATMOPHERIC CONDITIONS T. Wan, Tamkang Univ., Taiwan

3.3 10:00 - 12:00 Wing Aerodynamics Chair: Atkin, C.


10:00 (3.3.1) AN EXPERIMENTAL INVESTIGATION ON THE FREESTREAM TURBULENCE UPSTREAM OF A SWEPT WING I. Fumarola, City University London, United Kingdom

10:30 (3.3.2) EFFECTS OF REYNOLDS NUMBER ON THE ONSET OF LEADING EDGE VORTEX SEPARATION ABOVE BLUNT-EDGE DELTA WING VFE-2 CONFIGURATIONS M SAID, Aeronautical Laboratory, Malaysia

11:00 (3.3.3) DETERMINATION OF FLIGHT PERFORMANCE OF A FLAPPING AND FOLDING WING ORNITHOPTER THROUGH EXPIRMENTATION A.M. Matta, United States

11:30 (3.3.4) EXPERIMENTAL ANALYSIS OF A POROUS FLAP SIDE-EDGE L.T. Lima Pereira, University of São Paulo, Brazil

4.3 10:00 - 12:00 Vortical Flow Chair: ,


10:00 (4.3.1) FORMATION FLIGHT MECHANICS T. Melin, Linkoping University, Sweden

10:30 (4.3.2) THE NUMERICAL SIMULATION ON THE DRAG REDUCTION OF THE UPSWEPT TAIL OF A TRANSPORT AIRCRAFT USING VORTEX GENERATORS Y Liu, AVIC Aircraft Co,. Ltd, China

11:00 (4.3.3) SIMULATION OF UNSTEADY SHIP AIRWAKES W Yuan, National Research Council Canada , Canada

11:30 (4.3.4) EXTRACTION OF LINEAR INFLOW MODEL FOR MANEUVERING HELICOPTER FROM FREE-WAKE ANALYSIS O. Rand, Technion - IIT, Israel

5.3 10:00 - 12:00 Operations & Sustainment 1 Chair: Liao, M., Sec. Chair: Anderson, K.

Track 5 11 - Operations and Sustainment

10:00 (5.3.1) TRANSFORMING MILITARY AEROSPACE SUSTAINMENT D Holmes, Defence Science & Technology Group, Australia

10:30 (5.3.2) RELIABILITY ASSURANCE PROCESS FOR MILITARY UNMANNED AERIAL VEHICLE 82-10-8931-3981 SUL, KOREANAIR/AEROSPACE ENGINEERING TEAM, South Korea

11:00 (5.3.3) TOTAL LIFECYCLE COST(LCC) ESTIMATION AND CASE STUDY USING RELIABILITY, MAINTAINABILITY ANALYSIS LSY LEE, Korean Air / Aerospace Engineering Institute, South Korea

11:30 (5.3.4) INVESTIGATIONS OF ON GROUND INFRASTRUCTURES FOR UAS FLIGHT MONITORING S. Cresto Aleina, Politecnico di Torino, Italy

6.3 10:00 - 12:00 Structural Design 1 SHELLS Chair: Yeon, C., Sec. Chair: Pranata, B.



10:00 (6.3.1) INFLUENCE OF GEOMERICAL AND TECHNOLOGICAL CONSTRAINTS ON WEIGHT&COST PARAMETERS OF LATTICE COMPOSITE FUSELAGE STRUCTURES A.S. Shanygin, 140180, Russia

10:30 (6.3.2) WEIGHT REDUCTION OF CYLINDRICAL GRID STRUCTURES USING AXIAL-HELICAL DESIGN M. Beerhorst, DLR Braunschweig, Germany

11:00 (6.3.3) CHAOS THEORY APPLIED TO BUCKLING ANALYSIS OF COMPOSITE CYLINDRICAL SHELL C. Bisagni, TU Delft, Netherlands

11:30 (6.3.4) DEVELOPMENT OF LIGHTWEIGHT AND RELIABLE JOINTS FOR AIRFRAMES BASED ON UNIDIRECTIONAL COMPOSITE ELEMENTS A.V. Chernov, Central Aerohydrodynamic Institute (TsAGI), Russia

7.3 10:00 - 12:00 Fan & Compressors: MDO Chair: Mari, C., Sec. Chair: Chen, H.


10:00 (7.3.1) MULTI-POINT DESIGN OPTIMIZATION OF A HIGH BYPASS RATIO FAN BLADE Qiu Sheng, AVIC Commercial Aircraft Engine CO.LTD, China

10:30 (7.3.2) DEVELOPMENT OF THE FAN STAGE WITH ULTRA-LOW ROTATIONAL SPEED S.V. Pankov, CIAM, Russia

11:00 (7.3.3) DVANCED PROPULSION COLLISION DAMAGE DUE TO UNMANNED AREIAL VEHICLE INGESTION Y.K. Song, Virginia Tech, United States

11:30 (7.3.4) MULTI-DISCIPLINARY DESIGN OF HIGH-SPEED COMPRESSORS FOR PROSPECTIVE TURBO-SHAFT ENGINE A. Startsev, Central Institute of Aviation Motors, Russia

8.3 10:00 - 12:00 Flight Control 3 Chair: Moreira, F., Sec. Chair: Kim, H.


Modelling)

10:00 (8.3.1) PRECISION LANDING BASED ON ATMOSPHERIC DISTURBANCE MONITORING AND AND MODEL PREDICTIVE CONTROL N. Siepenkötter, RWTH Aachen, FSD, Germany

10:30 (8.3.2) PITCH STABILISATION WITH TAILORED CANARD COMPLIENCE P. Krus, Linköping university, Sweden

11:00 (8.3.3) ELASTIC MODES ADAPTIVE CANCELLATION ALGORITHM FOR THE A330 MRTT FLYING BOOM CONTROL LAWS R.R.R. Rodney Rodríguez Robles¹, A.S.B. Alberto Sanz de Blas¹; ¹Airbus Defence & Space, Spain

11:30 (8.3.4) ON STABILITY MARGIN OF A LQR-BASED VEHICLE NETWORK Y Kim, Gyeongsang National University, South Korea

9.3 10:00 - 12:00 UAV Test & Integration Chair: Vian, J., Sec. Chair: Rein Weston, K.


related)

10:00 (9.3.1) LAND-BASED FLIGHT TEST FOR SHIPBOARD LANDING OF TILT ROTOR UAV C.S. Yoo, Korea Aerospace Research Institute, South Korea

10:30 (9.3.2) ANALYSIS ON OFFLINE AND ONLINE IDENTIFICATION METHODS FOR UAV STABILITY AND CONTROL DERIVATIVES D. Ding, China Aerodynamic Research and Development Center, China

11:00 (9.3.3) FLIGHT PATH RECONSTRUCTION FOR AN UNMANNED AERIAL VEHICLE USING LOW-COST SENSORS C Göttlicher, Technische Universität München, Germany

11:30 (9.3.4) SYSTEM IDENTIFICATION OF A SCALE HELICOPTER IN HOVERING FLIGHT F. C. Reis, Escola de Engenharia de São Carlos - USP, Brazil

10.3 10:00 - 12:00 Flow Separation and Control Chair: Prince, S., Sec. Chair: Atkin, C.


Control 10:00 (10.3.1) ACTIVE VORTEX FLOW CONTROL ON A GENERIC DELTA WING A.

Buzica, Institute of Aerodynamics and Fluid Mechanics, TUM, Germany 10:30 (10.3.2) EFFECTIVENESS OF VORTEX GENERATORS IN HIGHLY 3D

FLOWS H. S. M Mudhar, City University London, United Kingdom 11:00 (10.3.3) EXPERIMENTAL INVESTIGATION OF FLOW AROUND AN AIRFOIL

WITH AN UNDULATED LEADING EDGE J. Pellicer-Collado, United Kingdom 11:30 (10.3.4) PASSIVE CONTROL OF AN AIRFOIL M. Rosti, Afghanistan 11.3 10:00 - 12:00 Airport Capacity

Chair: Reichmuth, J., Sec. Chair: Curran, R. Track 11

08 - Air Transport System Efficiency 10:00 (11.3.1) SCENARIO DEVELOPMENT FOR TRAJECTORY-BASED TAXI

OPERATIONS ENABLED BY DISPATCH TOWING TECHNOLOGIES T. Bernatzky¹, S. Baumann¹, U. Klingauf¹; ¹Technische Universitaet Darmstadt, Germany

10:30 (11.3.2) IMPROVEMENT OF PUSHBACK TIME ASSIGNMENT UNDER UNCERTAINTIES R. Mori, Electronic Navigation Research Institute, Japan

11:00 (11.3.3) TAXIING ROUTE PLANNING BASED ON AIRPORT HOTSPOTS WJ.PAN pan, CAFUC, China

11:30 (11.3.4) IDENTIFICATION OF THE IDEAL TRADE-OFF BETWEEN OPTIMAL PROFILE DESCENTS AND RUNWAY THROUGHPUT G. Enea, TASC Inc., United States

12.3 10:00 - 12:00 Vehicle Optimization and Design Chair: Yee, K., Sec. Chair: Hua, J.


Validation 10:00 (12.3.1) KNOWLEDGE-BASED INTEGRATED AIRCRAFT WINDSHIELD

OPTIMIZATION R.C Munjulury, Linköping university, Sweden 10:30 (12.3.2) OPTIMISATION OF A WING-BODY-TAIL CONFIGURATION WITH AN

ALTERNATIVE LOW DRAG FUSELAGE AND BODY TRAILING EDGE L Smith, University of Pretoria, South Africa

11:00 (12.3.3) DESIGN OPTIMIZATION OF HELICOPTER BLADE USING CLASS SHAPE FUNCTION BASED GEOMETRY REPRESENTATION Ariyarit A. Ariyarit, Tokyo Metropolitan University, Japan

11:30 (12.3.4) ROBUST OPTIMIZATION FOR THE DESIGN OF ROTORCRAFT AIRFOILS F. Fusi¹, A. Guardone¹, G. Quaranta¹, P. M. Congedo, INRIA Bordeaux Sud-Ouest, France; ¹Politecnico di Milano, Italy

12:00 - 13:00 Lunch

0.7 13:00 - 13:45 ICAS \"PAUL KEUK CHANG\" LECTURE FOR INNOVATION IN AERONAUTICS Chair: Shinji Suzuki PPSC Chair

13:00 The JSF Lift System Gregg Pyers

1.4 14:00 - 15:30 Innovative Concept-Super

Heavy Cargo Chair: Spieck, M., Sec. Chair: Szodruch, J.

Track1 01 - Aircraft and Systems

Integration 14:00 (1.4.1) A CONCEPTUAL DESIGN OF SUPER HEAVY CRYOGENIC

CONTAINER AIRCRAFT E.A. Pigusov, TsAGI (Central Aerohydrodynamic Institute), Russia

14:30 (1.4.2) FEASIBILITY STUDY OF A CARGO TRANSPORTATION SYSTEM BASED ON HYDROGEN-POWERED UNMANNED ULTRA LARGE AIRCRAFT

15

G La Rocca, Delft University of Technology, Netherlands 15:00 (1.4.3) ULTRA LARGE GROUND EFFECT VEHICLES RUNNING ON

CRYOGENIC FUEL – GREENER FUTURE FOR FAST CONTAINER FREIGHT A.A. Krutov, TsAGI (Central Aerohydrodynamic Institute), Russia

2.4 14:00 - 15:30 CFD Applications 2 Chair: Pavlenko, A., Sec. Chair: Bigarella, E.


Validation 14:00 (2.4.1) STORE SEPARATION FROM AIRCRAFT WEAPON BAYS M.G. Tutty,

RAAF, Australia 14:30 (2.4.2) DEVELOPMENT AND VALIDATION OF A COMPUTER CODE FOR

PREDICTING TRANSIENT MISSILE SURFACE TEMPERATURE B. Simsek¹, B. Kuran¹, M.-A. Ak¹, S. Uslu, TOBB University of Economics and Technology, Turkey; ¹Roketsan Missiles Industries Inc., Turkey

15:00 (2.4.3) STABILITY AND CONTROL FOR UNSTEADY HYDRODYNAMIC STINGRAY ROBOT B. Gater, Virginia Tech, United States

3.4 14:00 - 15:30 Wind Tunnel Technology Chair: Hunter, D.


14:00 (3.4.1) HYPERPARAMETERS OPTIMIZATION FOR ADAPTIVE DESIGN OF EXPERIMENTS APPLIED TO WIND TUNNEL TESTING H Jin, KAIST, South Korea

14:30 (3.4.2) A STUDY ON ENHANCEMENTS OF EFFICIENCY AND PRODUCTIVITY IN WIND TUNNEL TESTS USING DESIGN OF EXPERIMENTS K.-B. Kwon, Republic of Korea Air Force Academy, South Korea

15:00 (3.4.3) DESIGN AND TEST OF THE HIGH AERODYNAMIC PERFORMANCE LOW-NOISE FAN OF 5.5M BY 4M ACOUSTIC WINDTUNNEL X.l Xiaoli, China Aerodynamic Research and Development Center, China

4.4 14:00 - 15:30 Propeller/Wing Aerodynamics Chair: Monk, J.


14:00 (4.4.1) LOW REYNOLDS PROPELLER MODEL DESIGN FOR MULTIDICIPLYNARY OPTIMIZATION FM Catalano, Aeronautics Engineering depto/University of Sao Paulo, Brazil

14:30 (4.4.2) DISTRIBUTED PROPELLERS SLIPSTREAM EFFECTS ON WING AT LOW REYNOLDS NUMBER K.-L. Wang, Northwestern Polytechnical University, China

15:00 (4.4.3) NUMERICAL SIMULATION OF THE PROPELLER/WING INTERACTIONS AT LOW REYNOLDS NUMBER H.-B. Wang, Northwestern Polytechnical University, China

5.4 14:00 - 15:30 Landing Gear & Taxiing Chair: Mari, C., Sec. Chair: Vecchio, A.


Equipment 14:00 (5.4.1) LABORATORY INVESTIGATIONS ON LANDING GEAR GROUND

REACTIONS (LOAD) MEASUREMENT I. Paprzycki, Institute of Aviation, Poland 14:30 (5.4.2) EXPERIMENTAL AND SIMULATION STUDY OF THE DYNAMICS OF

AN ELECTRO-MECHANICAL LANDING GEAR ACTUATOR G. Di Rito, Università di Pisa - DICI, Italy

15:00 (5.4.3) GREEN TAXIING, SMART OPERATION ON GROUND (SOG) S Jaber, Safran Messier-Bugatti-Dowty, France

6.4 14:00 - 15:30 Structural Design 2 BLADES Chair: Park, J., Sec. Chair: Nakamichi, J.



14:00 (6.4.1) AUTOMATED SELECTION OF THE FAN BLADE PS-90A MATERIAL A.E. Kishalov¹, D.A. Akhmedzyanov¹, K.V. Markina¹; ¹USATU, Russia

14:30 (6.4.2) MULTIDISCIPLINARY DESIGN CHAIN FOR MODEL ROTOR BLADES B van de Kamp, DLR, Germany

15:00 (6.4.3) COUPLING GENETIC ALGORITHMS WITH MESO-SCALE COMPOSITE MODELING FOR BLADE CASING DESIGN B. Horton, Virginia Tech, United States

7.4 14:00 - 15:30 Hybrid / Electric Propulsion Chair: Isikveren, A., Sec. Chair: Mirzoyan, A.


14:00 (7.4.1) INTEGRATION OF HYBRID PROPULSION SYSTEM IN A CS23 COMMUTER DESIGN M Strack, Germany

14:30 (7.4.2) INVESTIGATION OF ARCHITECTURE AND CHARACTERISTICS OF OIL SYSTEM WITH ELECTRICALLY DRIVEN PUMPS FOR GAS TURBINE ENGINE Y.M. Shchurovskiy, Central Institute of Aviation Motors (CIAM), Russia

15:00 (7.4.3) METHODS FOR IMPROVING THE RELIABILITY OF FUEL SUPPLY SYSTEM OF GAS TURBINE ENGINES WITH USING ELECTRICALLY DRIVEN PUMPS A. I. Goulienko, Central Institute of Aviation Motors (CIAM), Russia

8.4 14:00 - 15:30 Flight Optimization Chair: Ueno, S., Sec. Chair: Sato, M.


Modelling)

14:00 (8.4.1) THE SUCCESSIVE BACKWARD SWEEP METHOD AUGMENTED WITH A HOMOTOPY ALGORITHM DH Cho, Airforce Academy, South Korea

14:30 (8.4.2) PRELIMINARY STUDY ON A RETURN FLIGHT TRAJECTORY OF A

SUBORBITAL VEHICLE A.K. Kwiek, Warsaw University of Technology, Poland 15:00 (8.4.3) INFERENCE OF FLIGHT INTENT BASED ON INVERSE OPTIMAL

CONTROL N. Yokoyama, National Defense Academy, Japan

9.4 14:00 - 15:30 UAV Design Configuration 1 Chair: Garth, J., Sec. Chair: Krus, P.


related) 14:00 (9.4.1) OVERVIEW OF THE INVERTED JOINED WING SCALED

DEMONSTRATOR PROGRAMME CRG Galinski, Institute of Aviation, Poland 14:30 (9.4.2) FLIGHT DYNAMICS MODELLING AND CONTROLLER DESIGN OF A

FLYING WING QUADROTOR UNMANNED AERIAL VEHICLE J.-C. Kim, Korea Aerospace Research Institute, South Korea

15:00 (9.4.3) OPTIMAL CONTROL SURFACE ALLOCATION AND HANDLING QUALITIES EVALUATION OF AN UNCONVENTIONAL UAV E Miles, CSIR, South Africa

10.4 14:00 - 15:30 Lateral Jets Chair: Dala, L., Sec. Chair: Atkin, C.


Control 14:00 (10.4.1) NUMERICAL INVESTIGATION OF UNSTEADY INTERACTION

CHARACTERISTIC INDUCED BY IMPULSIVE JET J.-L. Bo, CAAA, China 14:30 (10.4.2) EXPERIMENTAL INVESTIGATION OF LATERAL PULSE JET

INTERACTION FLOWFIELD IN HYPERSONIC FLOW Z.-Y. Ni, CAAA, China 15:00 (10.4.3) COMPUTATIONS OF SUPERSONIC LATERAL JET J. Huh¹, S. Lee¹,

E. Lee, Agency for Defense Development, South Korea; ¹Inha univ., South Korea 11.4 14:00 - 15:30 Environment Friendly

Operations Chair: Reichmuth, J.

Track 11 10 - Challenge of the

Environment 14:00 (11.4.1) PROJECTION OF GREEN-HOUSE-GAS EMISSION FROM KOREAN

AIR CARRIERS HJ. JOO, SEJONG UNIVERSITY, South Korea 14:30 (11.4.2) CONCEPT OF OPERATIONS OF AN ATC TOOL FOR TRAJECTORY

OPTIMIZATION K Chircop, University of Malta, Malta 15:00 (11.4.3) FLEET DEVELOPMENT PLANNING OF AIRLINES:

INCORPORATING THE AIRCRAFT OPERATING ECONOMICS FACTOR O. Oguntona, Germany

12.4 14:00 - 15:30 Estimation and Testing Chair: Hwang, I., Sec. Chair: Kanerva, M.

Track 12 03.1 - Materials issues, Fatigue and Damage

Tolerance

14:00 (12.4.1) DETERMINATION OF DESIGN ALLOWABLES FOR AIRCRAFT COMPOSITE STRUCTURES J.Y. CHOUNG, KARI, South Korea

14:30 (12.4.2) REAL-TIME VISUALIZATION AND ANALYSIS OF TENSOMETRY DATA IN THE COURSE OF STATIC STRENGTH TESTS D.V. Kurulyuk, Central Aerohydrodynamic Institute (TsAGI), Russia

15:00 (12.4.3) A STRESS INTENSITY FACTOR SOLUTION INSPIRED BY SOAP BUBBLES FRAMEWORK R. de Moura Pinho, SNECMA Villaroche, France

15:30 - 16:00 Break

1.5 16:00 - 18:00 Education

Chair: Zhuraylev, V., Sec. Chair: Szodruch, J.


Integration 16:00 (1.5.1) USING INTERNATIONAL COLLABORATIVE AIRCRAFT DESIGN

PROJECTS TO ENHANCE UNDERGRADUATE DESIGN EDUCATION: LESSONS LEARNED P. Raj, Virginia Tech/ AOE, United States

16:30 (1.5.2) AIRCRAFT DESIGN – AN OPEN EDUCATIONAL RESOURCE (OER) FOR HAMBURG OPEN ONLINE UNIVERSITY (HOOU) D. Scholz, Hamburg University of Applied Sciences, Germany

17:00 (1.5.3) STUDENT DESIGN PROCESSES IN INTERDISCIPLINARY COLLABORATION ACTIVITIES IN AERONAUTICS ENGINEERING EDUCATION J. Kimura, The University of Tokyo, Japan

2.5 16:00 - 18:00 High AOA and Unsteady Aerodynamics Chair: Hauser, A., Sec. Chair: Mani, M.

Track 2 02.1 - Aerodynamics - CFD Methods

and Validation 16:00 (2.5.1) MODELLING NONLINEAR HIGH-PRECISION UNSTEADY

AERODYNAMICS FOR ADVANCED AIRCRAFT AT HIGH ANGLE OF ATTACK Bai-Gang: B.-G. Mi, Northwestern Polytechnical University, China

16:30 (2.5.2) EFFECTS OF THE BOUNDARY LAYER TRANSITION ON THE GLOBAL AERODYNAMIC COEFFICIENTS J. L. Azevedo, Instituto de Aeronautica e Espaco, Brazil

17:00 (2.5.3) EFFECTS OF SOME NUMERICAL FORMULATION ASPECTS IN HIGH-LIFT CONFIGURATION SIMULATIONS E.D.V. Bigarella, Embraer, Brazil

17:30 (2.5.4) CFD OF BLENDED WING BODY UCAV WITH VORTEX GENERATOR K. Chang, Hanseo University, South Korea

3.5 16:00 - 18:00 Flow Visualisation 1 Chair: Goraj, Z.


16

16:00 (3.5.1) NON-INTRUSIVE UNSTEADY PSP TECHNIQUE FOR INVESTIGATION OF TRANSONIC BUFFETING S Sugioka, Tohoku University, Japan

16:30 (3.5.2) UNSTEADY AERODYNAMIC INFORMATION EXTRACTION USING FFT-BASED UNSTEADY PRESSURE-SENSITIVE PAINT MEASUREMENT K. Nakakita, Japan Aerospace Exploration Agency, Japan

17:00 (3.5.3) FLOW UNSTEADINESS RESEARCHES ON THE BLUNT FIN-INDUCED SHOCK/BOUNDARY LAYER INTERACTIONS X.J. Zhao, China Academy of Aerospace Aerodynamics, China

17:30 (3.5.4) EXPERIMENTAL STUDY OF GEOMETRIC VARIATIONS EFFECTS ON THE FLOW PATTERNS ON A HAMMERHEAD SATELLITE LAUNCH VEHICLE A.-C Avelar, Instituto de Aeronáutica e Espaço, Brazil

4.5 16:00 - 18:00 Special Topics Chair: ,


16:00 (4.5.1) STORE SEPARATION SIMULATION BASED ON CFD AND AERODYNAMIC MODEL Y Lei, School of Aeronautics, Northwestern Polytechnical University, China

16:30 (4.5.2) AERODYNAMIC SIMULATIONS OF PARACHUTE CHARACTERISTICS UNDER SEVERE WEATHER T. Wan, Tamkang Univ., Taiwan

17:00 (4.5.3) NUMERICAL SIMULATION OF WATER FILM FLOW ON AIRCRAFT ANTI-ICING SURFACE W Dong, Shanghai Jiao Tong University, China

17:30 (4.5.4) NUMERICAL SIMULATION OF DROPLET IMPINGEMENT ON A MULTI-ELEMENT HIGH-LIFT AIRFOIL L . Prince Raj¹, Rho Shin Myong¹; ¹Gyeongsang National University, South Korea

5.5 16:00 - 18:00 Modeling and Tests of Systems & Subsystems 1 Chair: Stoufflet, B.


Equipment 16:00 (5.5.1) SURROGATE MODELING TECHNIQUE FOR THE CONCEPTUAL AND

PRELIMINARY DESIGN OF EMBEDDED ACTUATION SYSTEMS AND COMPONENTS F. Sanchez, Institut Clément Ader/Paul Sabatier University, France

16:30 (5.5.2) SELECTION OF AN UAV CONFIGURATION LAYOUT FOR OPTIMISATION OF TELEDETECTION MISSION USING HYPERSPECTRAL SENSORS R. Fusaro, Politecnico di Torino, Italy

17:00 (5.5.3) STATISTICAL MODELING OF AIRCRAFT ENGINE FUEL FLOW RATE Y. S. Chati, Massachusetts Institute of Technology, United States

17:30 (5.5.4) AUTOMATED MODEL VALIDATION – APPLIED ON A SIMULATION MODEL OF THE SAAB GRIPEN FIGHTER ENVIRONMENTAL CONTROL SYSTEM M. Eek, Saab Aeronautics, Sweden

6.5 16:00 - 18:00 Structural Design 3 Chair: Bisagni, C., Sec. Chair: Kim, I.



16:00 (6.5.1) GENERATIVE DESIGN: ADVANCED DESIGN OPTIMIZATION PROCESSES FOR AERONAUTICAL APPLICATIONS S. Bagassi¹, F. Lucchi¹, F. De Crescenzio¹, F. Persiani¹; ¹University of Bologna, Italy

16:30 (6.5.2) DESIGNING OF AIRFRAMES HAVING MINIMUM MASS UNDER SEVERAL LOADINGS (NOT FULLY STRESSED) A.I. Danilin, Samara State Aerospace University (National Research University), Russia

17:00 (6.5.3) APPLICATIONS OF KO DISPLACEMENT THEORY TO DEFORMED SHAPE PREDICTIONS OF THE GIII SWEPT WING STRUCTURE S.-F Lung, Jacobs Technology Inc., United States

17:30 (6.5.4) FAIRING OPTIMIZATION DESIGN OF WING STRUCTURE R.-Z Zhang, CAE, China

7.5 16:00 - 18:00 Turbines Chair: Melkert, J.


16:00 (7.5.1) NUMERICAL INVESTIGATION OF THE SURFACE ROUGHNESS EFFECTS ON TURBINE VANE HEAT TRANSFER L.K Kai, China

16:30 (7.5.2) EFFECT OF REYNOLDS NUMBER, OPERATING MODE, TURBULENCE PARAMETERS ON PROFILE AND SECONDARY LOSSES OF LPT AIRFOILS A. Nepomnyashchiy, Central Institute of Aviation Motors, Russia

17:00 (7.5.3) EFFECT OF THE STRUCTURE OF RADIAL VANE CAVITY ON PERFORMANCE OF TURBINE INTER-VANE BURNER BASED ON JET-VORTEX FLOW ZHF haifei, Shanghai Aircraft Design and Research Institute, China

17:30 (7.5.4) INVESTIGATION THE EFFICIENCY OF VARIOUS COOLING SCHEMES OF HIGH-TEMPERATURE TURBINE BLADES S. Kharkovskiy, CIAM, Russia

8.5 16:00 - 18:00 Flight Dynamics & Identification Chair: Korsun, O., Sec. Chair: Choi, K.

Track 8 05.1 - Flight Dynamics and Control

(Control & Modelling)

16:00 (8.5.1) A FLIGHT DATA INDEXING METHOD FOR AIRCRAFT CHARACTERISTIC ESTIMATIONS AND FAULT DETECTIONS M. Naruoka, Japan Aerospace Exploration Agency, Japan

16:30 (8.5.2) CONTROL-RELEVANT SYSTEM IDENTIFICATION OF TWIN ROTOR MULTI-INPUT MULTI-OUTPUT SYSTEM IN HOVERING POSITION S. Kang, Korea Aerospace University, South Korea

17:00 (8.5.3) WIND VELOCITY ESTIMATION WITHOUT AN AIR VELOCITY SENSOR USING KALMAN FILTER WITH CONSIDERING COLORED

MEASUREMENT NOISE P.-Y Park, South Korea 17:30 (8.5.4) FLIGHT VEHICLE PARAMETER IDENTIFICATION BASED ON

PARTICLE FILTER INFORMATION FUSION WITH COKRIGING METHOD T.-J Jing, Schoolof Aeronautics, Northwestern Polytechnical University, China

9.5 16:00 - 18:00 Operations & Sustainment 2 Chair: Holmes, D., Sec. Chair: Scott, M.


16:00 (9.5.1) RESEARCH DEVELOPMENTS IN NONDESTRUCTIVE EVALUATION AND STRUCTURAL HEALTH MONITORING FOR THE SUSTAINMENT OF COMPOSITE AER K. E. Cramer, NASA, United States

16:30 (9.5.2) IN-FLIGHT VIBRATION-BASED STRUCTURAL HEALTH MONITORING OF AIRCRAFT WINGS E Neu, FH Aachen, Germany

17:00 (9.5.3) QUALIFICATION OF KAI KUH-1M ON BOARD ROKN SHIPS USING THE DUTCH APPROACH J. van der Vorst, NLR, Netherlands

17:30 (9.5.4) 3D IMAGING OF GEOMETRICAL STRUCTURE AND DEFECT LOCATION OF INNER CAVITY IN AVIATION DEVICES BY POSITRON INJECTION Hui: H Xiao, College of Automation Engineering, Nanjing University of Aeronau, China

10.5 16:00 - 18:00 Transition Forcing and Control Chair: Gowree, E., Sec. Chair: Breitsamter, C.


Control

16:00 (10.5.1) EXPERIMENTAL STUDY OF AEROFOIL-WAKE INDUCED TRANSITION IN BOUNDARY LAYERS D Veerasamy, City University, United Kingdom

16:30 (10.5.2) DISTURBANCES IN AN ACCELERATED BOUNDARY LAYER UNDER INFLUENCE OF MODERATE FREE-STREAM TURBULENCE D.S. Sboev, Central aerohydrodynamic institute n.a. Prof. N.E. Zhukovsky (Ts, Russia

17:00 (10.5.3) CONTROL OF CROSSFLOW INSTABILITY USING PLASMA ACTUATORS Z F Wang, Tsinghua University, China

17:30 (10.5.4) NUMERICAL MODELING OF LAMINAR-TURBULENT TRANSITION CONTROL BY MULTIPLE-ELECTRODES DBD ACTUATORS M.V. Ustinov, TsAGI, Russia

11.5 16:00 - 18:00 History of Aeronautics Chair: Tahk, M., Sec. Chair: Kim, Y. Track 11

16:00 (11.5.1) HISTORY OF RAPID GROWTH IN KOREAN AERONAUTICAL INDUSTRY D.M. AHN, HANSEO UNIV., South Korea

16:30 (11.5.2) DEVELOPMENT OF SMART TILTROTOR UAS AND THE BEGINNING OF KOREAN CIVIL DRONES C.H. LIM, Korea Aerospace Research Institute, South Korea

17:00 (11.5.3) FROM 500MD TO LAH - CHALLENGE TOWARD VERTICAL LIFT IN KOREA J.B. YIM, AGENCY FOR DEFENSE DEVELOPMENT, South Korea

17:30 (11.5.4) THE SANTOS-DUMONT LEGACY TO AERONAUTICS M. P. Brandao, ITA - DCTA, Brazil

12.5 16:00 - 18:00 Boundary Layer Asymptotic Analysis Chair: Hall, P., Sec. Chair: Atkin, C.

Track 12 02.3 - Basic Fluid Dynamics and

Flow Control 16:00 (12.5.1) THE FLOW AROUND THE TRIANGULAR WING IN THE REGIME OF

STRONG VISCOUS-INVISCID INTERACTION G. N. DUDIN, TsAGI, Russia 16:30 (12.5.2) DISTURBED FLOW IN THE LAMINAR BOUNDARY LAYER DUE TO

THE LOCAL UNSTEADY SURFACE HEATING I.I. Lipatov, TsAGI, Russia 17:00 (12.5.3) LOCAL SCATTERING THEORY AND ROLES OF A SCATTER ON

BOUNDARY-LAYER INSTABILITY AND ACOUSTIC RADIATION M. Dong, Tianjin University, China

17:30 (12.5.4) TRANSITION CONTROL THROUGH LOCALISED HEATING D. O. Odido, University of Pretoria, South Africa

0.8 18:00 - 19:30 Airbus Fly your Ideas student challenge Chair:

18:00

0.9 08:00 - 09:00 GENERAL LECTURE 3 Chair:

08:00 Complex System Architecture Ed Crawley

09:00 - 09:30 Break

1.6 09:30 - 12:00 Design Method 2

Chair: Prince, S., Sec. Chair: Ogilvie, F. Track1

01 - Aircraft and Systems Integration 09:30 (1.6.1) IDENTIFYING THE BEST DESIGN FOR UNCERTAIN MARKETS A. A.

Desai, The University of Manchester, United Kingdom 10:00 (1.6.2) DESIGN OF A BLENDED-WING-BODY CONCEPT FOR COMMERCIAL

TRANSPORT MISSIONS J. GAUVRIT-LEDOGAR, ONERA, France 10:30 (1.6.3) KNOWLEDGE-BASED DESIGN OPTIMIZATION FOR AIRCRAFT

CONTROL N Cavus, German Aerospace Center, Germany 11:00 (1.6.4) ROTORCRAFT SYSTEMS MODELLING FOR TWIN-ENGINE MEDIUM

17

HELICOPTER F. Hashim, Cranfield University, United Kingdom 11:30 (1.6.5) ENHANCING THE EXPLORATION OF AIRCRAFT CHANGEABILITY

DURING CONCEPTUAL DESIGN A.S.J. van Heerden, Cranfield University, United Kingdom

2.6 09:30 - 12:00 Current Developments in CFD Chair: Aoyama, T., Sec. Chair: Gao, Z.


Validation 09:30 (2.6.1) DEVELOPMENT OF HIGH ORDER AND HIGH RESOLUTION

SCHEMES FOR EFFICIENT SHOCK CAPTURING IN HIGH-SPEED FLOWS M.-H Ahn, KAIST, South Korea

10:00 (2.6.2) COMPUTATIONAL EFFICIENCY AND QUALITY OF DIFFERENT VERSIONS OF DISCONTINUOUS GALERKIN METHOD FOR LES/DES APPLICATIONS A.V. Wolkov, TsAGI, Russia

10:30 (2.6.3) DEVELOPMENT OF HIGH-ORDER NONLINEAR INTERPOLATION FOR OVERSET GRIDS F. Liao, Northwestern Polytechnical University, China

11:00 (2.6.4) EXTENDED VALIDATION OF A TRANSONIC LATTICE BOLTZMANN METHOD ON THE EXAMPLE OF THE NASA COMMON RESEARCH MODEL B. Koenig, Exa GmbH, Germany

11:30 (2.6.5) EFFICIENT MULTI-RESOLUTION ANALYSIS FOR IMPLICIT TEMPORAL INTEGRATION USING SCHUR COMPLEMENT S. Chae, Seoul National University, South Korea

3.6 09:30 - 12:00 High Lift/Multielement Aerodynamics Chair: ,


09:30 (3.6.1) IMPROVED DESIGN OF A HIGH LIFT SYSTEM FOR GENERAL AVIATION AIRCRAFT D. Steenhuizen, TU Delft, Netherlands

10:00 (3.6.2) PARAMETRIC DEVELOPMENT OF A SERRATED LEADING EDGE HIGH-LIFT DEVICE J.W. Viljoen, University of Pretoria , South Africa

10:30 (3.6.3) FLOW CONTROL ON HELICOPTER-ROTOR BLADES VIA ACTIVE GURNEY FLAP W. STALEWSKI, INSTITUTE of AVIATION, Poland

11:00 (3.6.4) STUDY ON THE SYSTEM INTEGRATION FOR MULTI-ELEMENT AIRFOIL AERODYNAMIC ANALYSIS B. Kim, Chungnam National University, South Korea

11:30 (3.6.5) THE INFLUENCE OF A LOCAL CHANGE IN WING DIHEDRAL ON THE LOW SPEED FLOW CHARACTERISTICS OF RECTANGULAR PLANFORM WINGS K P Garry, Cranfield University, United Kingdom

4.6 09:30 - 12:00 Design Optimization 1 Chair: ,


09:30 (4.6.1) INTEGRATED AIRCRAFT WING DESIGN OPTIMIZATION A. Ronzheimer, DLR, Institute of Aerodynamics and Flow Technology, Germany

10:00 (4.6.2) FUSELAGE SHAPE OPTIMIZATION AIMED AT AERODYNAMIC DRAG REDUCTION AT SUPERSONIC SPEEDS N. Ageev, TsAGI, Russia

10:30 (4.6.3) AERODYNAMIC SHAPES DESIGN ON THE BASE OF DIRECT NEWTON TYPE OPTIMIZATION METHOD S.A. Takovitskii, Central Aerohydrodynamic institute, Russia

11:00 (4.6.4) CFD-BASED AERODYNAMIC SHAPE OPTIMIZATION OF A MANNED REENTRY VEHICLE M. Mohammadi-Amin, Aerospace Research Institute, Iran

11:30 (4.6.5) AERODYNAMIC SHAPE OPTIMIZATION WITH A PARALLEL EVOLUTI ALGORITHM AND NUMERICAL FLOW MODELLING A JAHANGIRIAN, Amirkabir University of Technology, Iran

5.6 09:30 - 12:00 Advanced Materials Chair: Ikeda, T., Sec. Chair: Blom, A.


Tolerance

09:30 (5.6.1) PLASTIC DEFORMATION OF POWDER METALLURGY TUNGSTEN ALLOY FOILS FOR SATELLITE ENCLOSURES M. Kanerva¹, E. Sarlin, Tampere University of Technology, Department of Material Science, Finland; A. Hållbro, Plansee Group, Sweden; J. Jokinen¹; ¹Aalto University, Department of Mechanical Engineering, Finland

10:00 (5.6.2) MODERN MATERIAL IN AEROSPACE INDUSTRY - MAGNESIUM ALLOY CONTROL SYSTEM LEVER OF THE UNMANNED ILX - 27 HELICOPTER M. Wojtas, Institute of Aviation, Poland

10:30 (5.6.3) MULTISCALE EVALUATION OF EQUIVALENT STIFFNESS AND STRENGTH OF NON-CRIMP FABRIC COMPOSITES C. Yong, Northwestern Polytechnical University, China

11:00 (5.6.4) NONLINEAR FREE VIBRATION OF FG CARBON NANOTUBES BASED ON MODIFIED COUPLE STRESS AND VON KARMAN THEORIES H. Dastoom-L, Sharif University of Technology, Iran

6.6 09:30 - 12:00 Aeroelasticity 1 Chair: Amiryants, G., Sec. Chair: Jung, I.


Dynamics, Aeroelasticity 09:30 (6.6.1) THE ACTIVE AEROELASTICITY CONCEPT. MAIN STAGES AND

PROSPECTS OF DEVELOPMENT G. Amiryants, Central aerohydrodynamics institute – TsAGI, Russia

10:00 (6.6.2) ANALYSIS AND COMPUTATIONAL STUDY OF THE AERODYNAMICS, AEROELASTICITY AND FLIGHT DYNAMICS OF FLAPPING WING ORNITHOPTER Harijono Djojodihardjo, Private and Universiti Putra Malaysia, Malaysia

10:30 (6.6.3) DESIGN, MANUFACTURE AND FREQUENCY EXPERIMENT OF A NOVEL FLUTTER MODEL FOR AGARD WING 445.6 WITH STRUCTURE-

SIMILARITY W Qian, Dalian University of Technology, China 11:00 (6.6.4) GROUND VIBRATION TEST AND FLUTTER ANALYSIS OF

DIVISIONAL UNMANNED AIRCRAFT SYSTEM M.S. Park, Korean Air/R&D Center, South Korea

11:30 (6.6.5) FLUID-STRUCTURE INTERACTION ANALYSIS FOR FLAPPING WING USING CO-ROTATIONAL SHELL ELEMENT H. Cho, Seoul National Univ., South Korea

7.6 09:30 - 12:00 Inlet, Fan and Compressors Chair: Pankov, S., Sec. Chair: Melkert, J.


09:30 (7.6.1) COUPLED UNSTEADY NUMERICAL SIMULATIONS OF A THREE STAGE TRANSONIC COMPRESSOR WITH INTAKE GEOMETRY T. Kächele, University of the German Federal Armed Forces, Germany

10:00 (7.6.2) UNSTEADY FLOW MEASUREMENTS IN A SCALED ENGINE TEST BED FOR ENGINE INLET DESIGN R.P.M. Rademakers, Institute of Jet Propulsion, Germany

10:30 (7.6.3) CHARACTERIZATION OF FLUID FLOW ALONG ADVANCED HIGH-BYPASS PROPULSION SYSTEM Y.K Song, Virginia Tech, United States

11:00 (7.6.4) ANALYSES OF AIRFLOW AROUND DUCTED FAN PROPULSION SYSTEM IN PUSHER CONFIGURATION USING PIV AND CFD METHODS P. Ruchala¹, K. Bogdanski, Politechnika Warszawska, Poland; W. Stryczniewicz¹; ¹Instytut Lotnictwa, Poland

11:30 (7.6.5) THE INVESTIGATION OF TIP CLEARANCE EFFECTS IN DUCTED ROTOR AERODYNAMICS CHARACTERISTICS USED IN UNMANNED AERIAL VEHICLES X.-H. LI, national university of defense technology, China

8.6 09:30 - 12:00 Handling Quality Chair: Zaichik, L., Sec. Chair: Quagliotti, F.


Modelling) 09:00 (8.6.1) NOVEL PILOT CONTROL MODEL WITH STOCHASTIC AND

PERIODICAL MOVEMENT R. Mori, Electronic Navigation Research Institute, Japan

09:30 (8.6.2) THE FLYING QUALITIES IMPROVEMENT FOR THE VEHICLES WITH TIME DELAY IN THEIR DYNAMICS A.V. Efremov , Moscow Aviation Institute, Russia

10:00 (8.6.3) PILOT\'S CG LOCATION AND ATTITUDE CONTROL FOR LATERAL MANEUVER OF A HANG GLIDER Y. Ochi, National Defense Academy, Japan

10:30 (8.6.4) AERIAL REFUELING BOOM SYSTEM (ARBS) DEVELOPMENT AND HANDLING QUALITIES EVALUATION ANTONIO ANTON DIEZ¹, FRANCISCO ASENSIO NIETO¹; ¹AIRBUS DEFENCE & SPACE, Spain

11:30 (8.6.5) EFFECT OF INCEPTOR FEEL SYSTEM CHARACTERISTICS ON PILOT-AIRCRAFT SYSTEM PERFORMANCE K. Grinev, Central Aerohydrodynamic Institute (TsAGI), Russia

9.6 09:30 - 12:00 UAV Nav & Operations Chair: Esteban-Campillo, D., Sec. Chair: Rein Weston, K.


(UAV related) 09:30 (9.6.1) APPROXIMATE THREE-DIMENSIONAL PATH GENERATION FOR

UAV PATH-FOLLOWING N. Cho, Seoul National University, South Korea

10:00 (9.6.2) DEVELOPMENT OF PEST\'S BIOLOGICAL CONTROL TOOL USING VTOL UAV SYSTEMS RKR Rangel, BRVANT / BRV UAV& Flight Systems, Brazil

10:30 (9.6.3) OPTICAL FLOW ON A FLAPPING WING MICRO AIR VEHICLE TO AVOID COLLISIONS AND STEER S, W, Ryu, Seoul National University, South Korea

11:00 (9.6.4) FLIGHT TESTS OF THE VISION-BASED TARGET SENSING AND APPROACHING S. Cho¹, Y. Jung, Korea Aerospace Research Institute, South Korea; D.H. Shim¹; ¹Korea Advanced Institute of Science and Technology, South Korea

11:30 (9.6.5) REAL-TIME GENERATION OF WAYPOINTS ENHANCING UAV SURVIVABILITY C.-K. Ryoo, Inha University, South Korea

10.6 09:30 - 12:00 Hybrid-Electric and Distributed Propulsion Aircraft 1 Chair: Isikveren, A., Sec. Chair: del Rosario, R.

Track 10 01 - Aircraft and Systems

Integration 09:30 (10.6.1) A REVIEW OF RECENT AIRCRAFT CONCEPTS EMPLOYING

SYNERGISTIC PROPULSION-AIRFRAME INTEGRATION J. Bijewitz, Bauhaus Luftfahrt e.V., Germany

10:00 (10.6.2) THE E-FAN ALL ELECTRICAL AIRCRAFT DEMONSTRATOR AND ITS INDUSTRIALIZATION D. Mueller Wiesner, Airbus, Germany

11.6 09:30 - 12:00 Flow Management Chair: Eijkman, M., Sec. Chair: Nakajima, T.


09:30 (11.6.1) A STUDY ON SAFETY ASSURANCE FOR INCREASINGLY AUTONOMOUS TRAFFIC FLOW MANAGEMENT SYSTEM Y. Wu, University of Missouri St. Louis D of Maths and Computer Science, United States; T. A. Lauderdale, NASA Ames Research Center / Aviation Systems Division, United States; H. Chen, Johnson C. Smith University Computer Science & Engineering Dept., United States

10:00 (11.6.2) ASSESSING THE SESAR DYNAMIC AIRSPACE CONFIGURATION CONCEPT IN REIMS ACC AIRSPACE T. dubot, ONERA, France

10:30 (11.6.3) TOWARDS A MORE HARMONISED AND WIDER USE OF SHORT-TERM ATFCM MEASURES (STAM) P Choroba, EUROCONTROL, France

18

11:00 (11.6.4) VISUALIZATION OF AIRSPACE COMPLEXITY BASED ON AIR TRAFFIC CONTROL DIFFICULTY H. Hirabayashi, Electronic Navigation Research Institute, Japan

11:30 (11.6.5) AN ADVANCED ATCO WORKSTATION DEVELOPMENT D. Rohacs, Budapest University of Technology and Economics, Hungary

12.6 09:30 - 12:00 Aircraft Operations and Safety Chair: Franchi, B.

Track 12 09 - Safety and Security

09:30 (12.6.1) DESIGN OF AN AUTOMATIC ELECTRONIC POSITION INDICATING RADIO BEACON EJECTION SYSTEM FOR LOCATING AIRCRAFT ON WATER L. Peters, RMIT University, Australia

10:00 (12.6.2) AIRCRAFT SECURITY ENHANCEMENT ROTATING MACHINERY FAULT DIAGNOSIS AND HEALTH ASSESSMENT USING MANIFOLD LEARNING AND DTW Y. Tian¹, C. Lu¹, Z.-L. Wang¹; ¹School of Reliability and Systems Engineering,Beihang University, China

10:30 (12.6.3) ANALYSIS OF AIRCRAFT\'S STATIC PRESSURE INSTALLATION RESIDUAL ERROR REQUIREMENTS H-Y Hui, China

11:00 (12.6.4) PASSENGER AND CABIN LUGGAGE WEIGHT SURVEY IN AUSTRALIA C. Bil, RMIT University, Australia

11:30 (12.6.5) FUEL STARVATION CAUSED BY HUB CLOSURE C. Wang¹, L. Drees¹, F. Holzapfel¹; ¹Technische Universität München, Germany

12:00 - 13:00 Lunch

0.10 13:00 - 13:45 GENERAL LECTURE 4 Chair: Chantal Fualdes

13:00 Experience and Lessons of a full composite passenger aircraft development tbd

1.7 14:00 - 15:30 Design for Uncertainty

Chair: Ravachol, M., Sec. Chair: Rinoe, K. Track1

01 - Aircraft and Systems Integration 14:00 (1.7.1) LINKING TECHNOLOGY READINESS TO UNCERTAINTY

REDUCTION K Gatian, Georgia Institute of Technology, United States 14:30 (1.7.2) EXPLORING OF THE PROPAGATING OF UNCERTAINTIES IN A

MULTI-DISCIPLINARY AIRCRAFT DESIGN ANALYSIS FRAMEWORK T.P. Pfeiffer, DLR, Germany

15:00 (1.7.3) UNCERTAINTY QUANTIFICATION OF ADVANCED PROPELLER MODELS H. D Schwartz, Georgia Institute of Technology, United States

2.7 14:00 - 15:30 CFD for Wind Tunnel Effects Chair: Catalano, F., Sec. Chair: Hunter, D.


Validation

14:00 (2.7.1) EXPERIENCE IN AERODYNAMICAL TESTS AND CFD SIMULATIONS OF OVERSIZED WING DEMONSTRATOR IN LARGE LOW-SPEED WIND TUNNEL A. Lysenkov, Russia

14:30 (2.7.2) STUDY OF MODEL DEFORMATION AND STING INTERFERENCE TO THE AERODYNAMIC ESTIMATION OF THE CAE-AVM MODEL M. Zhong, Chinese Aeronautical Establishment, China

15:00 (2.7.3) NUMERICAL INVESTIGATION OF THE CONTROLLED BOUNDARY LAYER FOR THE WALL INTERFERENCE REDUCTION IN TRANSSONIC WIND TUNNELS E.V. Streltsov, TsAGI, Russia

3.7 14:00 - 15:30 Education in Systems Engineering and Integration Chair: Müller-Wiesner, D.

Track 3 07 - Systems Engineering and

Supply Chain 4.7 14:00 - 15:30 MAV-related Aerodynamics

Chair: , Track 4

02.4 - Applied Aerodynamics 14:00 (4.7.1) AN EXPERIMENTAL STUDY OF MICRO-ELECTROMECHANICAL

FLYING INSECT FLAPPING WINGS AERODYNAMIC PERFORMANCE A. Zyluk, Air Force Academy, Poland; K.-S. Sibilski, Air Force Institute of Technology, Poland; P. Czekalowski, Institute of Aviation, Poland

14:30 (4.7.2) PARAMETRIC STUDY ON FLAPPING TRAJECTORY OF MAVS\' FLEXIBLE WING H. Jeong, South Korea

15:00 (4.7.3) ANALYTICAL, CFD AND EXPERIMENTAL AERODYNAMICS AND FLIGHT DYNAMIC STUDIES OF COAND? MAV FOR DESIGN Harijono Djojodihardjo, Private/Retired and Universiti Putra Malaysia, Malaysia

5.7 14:00 - 15:30 Operations & Sustainment 3 Chair: Cramer, E., Sec. Chair: Zan, S.


14:00 (5.7.1) RESEARCH ADVANCES ON AIRCRAFT STRUCTURAL INTEGRITY AND SUSTAINMENT AT NRC Min Liao, National Research Council Canada, Canada

14:30 (5.7.2) DESIGN AND PRELIMINARY EVALUATION OF AN INTEGRATED AIRCRAFT OPERATION SYSTEM FOR DISASTER RELIEF A. Andreeva-Mori, Japan Aerospace Exploration Agency, Japan

15:00 (5.7.3) ASSESSMENT OF FUTURE AIRCRAFT CABIN CONCEPTS WITH

ENHANCED TURNAROUND PERFORMANCE M. Schmidt, Munich Aerospace e.V., Germany; M. Engelmann¹, M. Hornung¹; ¹Bauhaus Luftfahrt e.V., Germany

6.7 14:00 - 15:30 Impact Chair: Kim, C., Sec. Chair: Zichenkov, M.


Dynamics, Aeroelasticity 14:00 (6.7.1) FRACTURE BEHAVIOR OF RIVETED LAP JOINTS DUE TO

PROJECTILE IMPACTS T-M Matsuda, CHURYO ENGINEERING CO., LTD., Japan

14:30 (6.7.2) MODELING AND ANALYSIS METHOD ON CRASHWORTHINESS OF CIVILIAN AIRCRAFT FUSELAGE STRUCTURES HY Huang, China

15:00 (6.7.3) AIRFRAME STRUCTURAL SURVIVABILITY STUDY THROUGH HYDRODYNAMIC RAM OF WELDED METALLIC WATER TANKS J. Kim, Agency for Defense Development, South Korea

7.7 14:00 - 15:30 Propeller Chair: Remy, S., Sec. Chair: Startsev, A.


14:00 (7.7.1) ANALYSIS OF SWIRL RECOVERY VANES FOR INCREASED PROPULSIVE EFFICIENCY IN TRACTOR PROPELLER AIRCRAFT L.L.M. Veldhuis, Delft University of Technology, Netherlands

14:30 (7.7.2) MULTI-OBJECTIVE OPTIMAL DESIGN OF THE PROPELLER FOR HIGH ALTITUDE AIRSHIPS BASED ON HIGH EFFICIENCY AND LIGHT WEIGHT J.-J JIAO, School of Aeronautics, Northwestern Polytechnical University, China

15:00 (7.7.3) SMALL HEIGHT DUCT DESIGN FOR MULTICOPTER FAN M.E. Arkhipov, Moscow Institute of Physics and Techtology, Russia

8.7 14:00 - 15:30 Flight Testing Chair: Yanagihara, M., Sec. Chair: Esteban-Campillo, D.


(Control & Modelling) 14:00 (8.7.1) WIND TUNNEL FREE-FLIGHT TEST FOR FLIGHT DYNAMICS AND

CONTROL SYSTEM EXPERIMENTS F. Cen¹, B.-W. Nie¹, H.-S. Sun¹; ¹China Aerodynamics Research and Development Center, China

14:30 (8.7.2) WIND TUNNEL THREE-DEGREE-OF-FREEDOM DYNAMIC RIG FOR CONTROL VALIDATION D.I. Ignatyev, Central Aerohydrodynamic Institute (TsAGI), Russia

15:00 (8.7.3) INVESTIGATION OF FLIGHT DATA VIA MODERN ANALYSIS METHODS FOR AIRCRAFT DURING LANDING PHASE T. Wan, Tamkang Univ., Taiwan

9.7 14:00 - 15:30 UAV Design Configuration 2 Chair: Vian, J., Sec. Chair: Bil, C.


related) 14:00 (9.7.1) DYNAMIC MODELING AND STABILITY ANALYSIS OF HIGH

ALTITUDE AIRSHIP R.-P Hun, Indian Institute of Technology, India 14:30 (9.7.2) TRAJECTORY OPTIMIZATION OF PERCH LANDING ASSISTED BY

THRUSTER S.Y. Han, KAIST FDCL, South Korea 15:00 (9.7.3) ADAPTIVE SLIDING MODE CONTROLLER DESIGN FOR

RECONFIGURATION OF ORGANIC FLIGHT ARRAY J. Jeong¹, S. Kim¹, J. Suk¹; ¹Chungnam National University, South Korea

10.7 14:00 - 15:30 Reduced Order Modeling Chair: Görtz, S., Sec. Chair: Breitsamter, C.


Control

14:00 (10.7.1) ON APPLYING PISTON THEORY IN INTERFERENCE FLOWS M.-C. Meijer, University of Pretoria, South Africa

14:30 (10.7.2) UNSTEADY AERODYNAMICS MODELLING AND ITS APPLICATION IN AEROELASTIC STABILITY ANALYSIS X.-T Li, School of aeronautics, Northwestern Polytechnical University, China

15:00 (10.7.3) SOURCE TERM MODEL FOR STREAMWISE AIR-JET VORTEX GENERATOR MODELLING T.D. Kwiatkowski, Institute of Aviation, Poland

11.7 14:00 - 15:30 Noise & Emission Chair: Zhang, X.

Track 11 10 - Challenge of the Environment

14:00 (11.7.1) ACOUSTICAL COMPARISON OF CONVENTIONAL TAXIING AND DISPATCH TOWING – TAXIBOT´S CONTRIBUTION TO GROUND NOISE ABATEMENT K Hein, TU Darmstadt, Germany

14:30 (11.7.2) ON THE ANNALUSIS AND SYNTHESIS OF THE NOISE FROM LOCO AND HIGH-SPEED PROPELLERS F. J. P. Lau F. J. P. Lau, Portugal

15:00 (11.7.3) QUANTITATIVE EMISSIONS OF NOX, CO AND CO2 DURING AIRCRAFT OPERATIONS P.J. Glowacki, Institute of Aviation, Poland

12.7 14:00 - 15:30 Icing & Jet Engine Safety Chair: Parker, R.

Track 12 09 - Safety and Security

14:00 (12.7.1) EULERIAN METHOD FOR IN-ENGINE ICING: WITH APPLICATION TO ICE CRYSTALS IN A GENERIC TURBOFAN COMPRESSOR E. Norde¹, E.T.A. van der Weide¹, H.W.M. Hoeijmakers¹; ¹University of Twente, Netherlands

14:30 (12.7.2) RESEARCH ON AIRWORTHINESS REQUIREMENTS OF SUPERCOOLED LARGE DROP ?SLD? ICING PROTECTION FOR AIRCRAFT T.H. Hu, China Aero-Polytechnology Establishment, China

19

15:00 (12.7.3) RESTARTING OF A JET ENGINE DURING FLYING AND FLIGHT SAFETY M Kowalski, Air Force Institute of Technology, Poland

15:30 - 16:00 Break

1.8 16:00 - 18:00 UAS

Chair: Miyazawa, Y., Sec. Chair: Kimmel, W. Track1

01 - Aircraft and Systems Integration 16:00 (1.8.1) CONCEPTUAL STUDY OF AN INNOVITIVE HIGH ALTITUDE SOLAR

POWERED FLIGHT VEHICLE Jiang Hanjie, The First Aircraft Institute of AVIC, China, China

16:30 (1.8.2) TOWARDS THE TRAFFIC MANAGEMENT OF SMALL UAS OPERATING AT VERY LOW LEVEL T. dubot, ONERA, France

17:00 (1.8.3) FEASIBILITY ANALYSIS OF SPAN EXTENSION OF MORPHING HALE UAV WING Tanvi Prakash, India

17:30 (1.8.4) CONCEPTUAL AND AERODYNAMIC DESIGN OF A UAV FOR SUPERFICIAL VOLCANO MONITORING. P. D. Bravo Mosquera, University of Sao Paulo, Brazil

2.8 16:00 - 18:00 Hypersonic Aerodynamics Chair: Hong Kim, K., Sec. Chair: Dala, L.


Validation

16:00 (2.8.1) NUMERICAL SIMULATION OF MIXING IN AN INLET-FUELED HYPERSONIC AIR-BREATHING PROPULSION J.W. Kim, Korea Advanced Institute of Science and Technology, South Korea

16:30 (2.8.2) AEROTHERMODYNAMICS CHARACTERISTICS OF A SPACE PROBE IN THE MARTIAN ATMOSPHERE I. Egorov, TsAGI, Russia

17:00 (2.8.3) A MESHLESS METHOD FOR SIMULATION OF HYPERSONIC VISCOUS FLOWS J.Y. HUH, Seoul National University, South Korea

17:30 (2.8.4) ON THE AERODYNAMIC ANALYSIS OF ORION SPACECRAFT T. Wan, Tamkang Univ., Taiwan

3.8 16:00 - 18:00 Flow Visualisation 2 Chair: Goraj, Z.


16:00 (3.8.1) PRESSURE ANALYSIS BASED ON PIV MEASUREMENT IN AIRPLANE WAKES K. Matsushima, Univ. of Toyama, Japan; H. Kato, JAXA, Japan

16:30 (3.8.2) AIRFLOW VISUALISATION DURING RESEARCH OF LARGE SCALE VORTEX FLOWS A. Zamyatin¹, M. Grigorev¹, V. Rogozin¹; ¹Gromov Flight Research Institute, Russia

17:00 (3.8.3) DIAGNOSTICS OF BOUNDARY LAYER TRANSITION BY SHEAR STRESS SENSITIVE LIQUID CRYSTALS E.S. Shapoval, FSUE TsAGI, Russia

17:30 (3.8.4) TSP MEASUREMENT ON INFLATABLE AERODYNAMIC DECELERATOR AT HYPERSONIC SPEED M. Taguchi, Nagoya University, Japan

4.8 16:00 - 18:00 (Aerodynamic) Control Methods Chair: ,


16:00 (4.8.1) MODELING OF A COANDA FLAP SYSTEM FOR FLAPLESS FLIGHT CONTROL K. Stadlberger, TUM, Institute of Aircraft Design, Germany

16:30 (4.8.2) STABILITY AND CONTROL ANALYSIS AND DESIGN OF TAILLESS AIRCRAFT USING VARIABLE-FIDELITY AERODYNAMIC ANALYSIS JH Park, Virginia Polytechnic Institute and State University, United States

17:00 (4.8.3) IMPORTANCE OF TRANSIENT AERODYNAMIC DERIVATIVES FOR V-TAIL AIRCRAFT FLIGHT DYNAMIC DESIGN N.-A Musa, Aeronautical Laboratory,, Malaysia

17:30 (4.8.4) NUMERICAL INVESTIGATION OF DIELECTRIC BARRIER DISCHARGE PLASMA ACTUATORS FOR DELTA-WING UAV APPLICATIONS R.W.L Ling, RMIT University, Australia

5.8 16:00 - 18:00 Damage Tolerance Chair: Kim, J., Sec. Chair: Bayandor, J.


Tolerance

16:00 (5.8.1) DAMAGE TOLERANCE AND REPAIR OF UD-RIBS OF LATTICE COMPOSITE FUSELAGE STRUCTURES E.A. Dubovikov, Central Aerohydrodynamic Institute (TsAGI), Russia

16:30 (5.8.2) NUMERICAL ASSESSSMENT OF DAMAGE TOLERANCE ALLOWABLES FOR NEW DESIGN CONCEPTS OF STIFFENED COMPOSITE PANELS T. Bach, German Aerospace Center (DLR), Germany

17:00 (5.8.3) XFEM-BASED FRACTURE MECHANICS ANALYSIS OF AERONAUTICAL STRUCTURES AFFECTED BY RESIDUAL STRESSES I. Rivero Arevalo, Airbus Defence and Space, Spain

17:30 (5.8.4) INVESTIGATION OF DEFORMATION FIELDS IN AIRCRAFT PANELS BY NON-CONTACT VIDEOGRAMMETRY METHOD K.A. Kopoteva, Central Aerohydrodynamic Institute (TsAGI), Russia

6.8 16:00 - 18:00 Structural Design 4 Chair: Kuzmins, S., Sec. Chair: Shin, E.



16:00 (6.8.1) NUMERICAL AND EXPERIMENTAL STRENGTH ANALYSIS OF LATTICE COMPOSITE FUSELAGE STRUCTURES I.O. Ivan, 140180, Russia

16:30 (6.8.2) EXPERIENCE AND PERSPECTIVES OF USING NONLINEAR

NUMERICAL ANALYSIS TO ESTIMATE AIRCRAFT STRUCTURE LOAD-BEARING CAPACITY E.A. Levchenko, Central Aerohydrodynamic Institute n.a. prof. N.E. Zhukovsky, Russia

17:00 (6.8.3) APPLICATION OF BUCKLING/POST-BUCKLING ANALYSIS FOR COMPOSITE STIFFENED PANELS L.J. Dong, Chinese Aeronautical Establishment, China

17:30 (6.8.4) OPTIMIZATION OF COMPOSITE PATCHREPAIR FOR ANGLED CRACK ON ALUMINUM PLATE USING GENETIC ALGORITHM A. Abedian, Sharif University of Technology, Iran

7.8 16:00 - 18:00 System of Systems Design & Operation Chair: Holmberg, G., Sec. Chair: Andersson, K.


Supply Chain

16:00 (7.8.1) AN EXPLORATION OF CONTROL SCHEMES AND ARCHITECTURES FOR UNMANNED SWARMS IN MARITIME OPERATIONS D.N. Mavris, Georgia Tech, United States

16:30 (7.8.2) THE DESIGN OF OPERATIONAL CONCEPT FOR DRONE DELIVERY SYSTEM H.-S. Kim, Republic of Korea Air Force Academy, South Korea

17:00 (7.8.3) EVOLUTIONARY GAME BASED MULTI OBJECTIVE OPTIMIZATION H Shin, United Kingdom

17:30 (7.8.4) MODEL BASED DESIGN FOR AUTOMATED SYSTEM ARCHITECTURE GENERATION I. Staack, Linköping University, Sweden

8.8 16:00 - 18:00 Flight Trajectory Design Chair: Tsuchiya, T., Sec. Chair: Miyazawa, Y.

Track 8 05.1 - Flight Dynamics and Control (Control

& Modelling)

16:00 (8.8.1) SHORTEST PAST OPTIMIZATION FOR ATM BASED ON APPROXIMATED OPTIMAL PATH H Shin, United Kingdom

16:30 (8.8.2) BENEFITS ASSESSMENT ON TIME-BASED OCEANIC ARRIVALS TO THE TOKYO METROPOLITAN AREA N.K. Wickramasinghe, Electronic Navigation Research Institute, Japan

17:00 (8.8.3) TRAJECTORY DESIGN WITH PATH PREDICTION FOR TERRAIN FOLLOWING MK KIM, KAIST, South Korea

17:30 (8.8.4) MINIMUM-TIME FORMATION USING OPTIMAL SOLUTIONS OF SINGLE FIXED-WING AIRCRAFT H. Fukumoto, Yokohama National University, Japan

9.8 16:00 - 18:00 Modeling and Tests of Systems & Subsystems 2 Chair: Stoufflet, B.


Equipment 16:00 (9.8.1) COMPARISON OF FUNCTIONAL ANALYSES FOR THE FLIGHT TEST

DRIVEN DEVELOPMENT OF HLFC SYSTEMS FOR HTP AND VTP O. Seibel¹, G. Kalarikovilagam Sri¹, O. Bertram¹, H. Spangenberg¹; ¹DLR, Germany

16:30 (9.8.2) REAL-TIME CREDIBILITY ASSESSMENT OF AIRCRAFT SYSTEM SIMULATORS M. Eek, Saab Aeronautics, Sweden

17:00 (9.8.3) SYSTEMS DRIVEN AIRCRAFT CONFIGURATION OPTIMIZATION USING INSIDE OUT APPROACH P S Shiva Prakasha, German Aerospace Center , DLR , Germany

17:30 (9.8.4) HIL TEST BENCH FOR ENGINE\'S FUEL CONTROL SYSTEMS INVESTIGATION S.A. Gafurov, Samara State Aerospace University (National Research University), Russia

10.8 16:00 - 18:00 Shock Waves and Control Chair: Sznajder, J., Sec. Chair: Goraj, Z.


Control

16:00 (10.8.1) INVESTIGATION ON OBLIQUE SHOCK WAVE CONTROL BY SURFACE ARC DISCHARGE PLASMA F.-L. LIU, Northwestern Polytechnical University, China

16:30 (10.8.2) OPTIMISATION OF NS-DBD PLASMA ACTUATORS FOR SUPERSONIC FLOW CONTROL A Russell, United Kingdom

17:00 (10.8.3) THE DEVELOPMENT OF A SIMPLE METHOD FOR DRAG ESTIMATION FOR WEDGE-LIKE FAIRINGS IN HYPERSONIC FLOW S. A. Prince, Cranfield University, United Kingdom

17:30 (10.8.4) OSCILLATION CHARACTERISTICS OF THE SHOCK WAVES AROUND A SUPERSONIC DECELERATION-DEVICE-MODEL WITH AEROSPIKE T. Mizukaki, Tokai University, Japan

11.8 16:00 - 18:00 Separation Management Chair: Graham, R., Sec. Chair: Conway, S.


16:00 (11.8.1) OPTIMAL SEQUENCING IN ATM COMBINING GENETIC ALGORITHMS AND GRADIENT BASED METHODS TO A BILEVEL APPROACH B. Grüter¹, M. Bittner¹, M. Rieck¹, J. Diepolder¹, F. Holzapfel¹; ¹Institute of Flight System Dynamics, TU München, Germany

16:30 (11.8.2) WAKE TURBULENCE RE-CATEGORISATION ON APPROACH AND DEPARTURE FOR SAFE AND MORE EFFICIENT AIR TRAFFIC MANAGEMENT F. Rooseleer, EUROCONTROL, Belgium

17:00 (11.8.3) AIRBORNE COLLISION AVOIDANCE CONSIDERATIONS FOR INDEPENDENT AND DEPENDENT CLOSELY-SPACED PARALLEL APPROACHES C. Hanses, German Aerospace Center (DLR), Germany

17:30 (11.8.4) NONLINEAR OPTIMAL CONFLICT RESOLUTION SOLVED WITH PARTICLE SWARM OPTIMIZATION Y. Hong, Seoul National University, South

20

Korea 12.8 16:00 - 18:00 Humans in the Loop

Chair: Lafoutan, R. Track 12

09 - Safety and Security 16:00 (12.8.1) CAN 3D-AUDIO IMPROVE STATE-OF-THE-ART PILOT-ASSISTANCE

SYSTEMS? C. A. Niermann, German Aerospace Center (DLR), Germany 16:30 (12.8.2) OBJECTIVE EVALUATION OF HUMAN PILOT OPERATIONS IN

WIND SHEAR USING PSYCHOPHYSIOLOGICAL MEASUREMENTS J.O. Entzinger, The University of Tokyo, Japan

17:00 (12.8.3) EVALUATION METHODS OF AIRCRAFT FLIGHT SAFETY J Zurek, Air Force Institute of Technology, Poland

0.11 08:00 - 09:30 GENERAL LECTURE 5 Chair:

08:00 IFAR Plenary Lecture tbd

09:30 - 10:00 Break

1.9 10:00 - 12:30 Environmentally Responsible

Aviation Chair: Mavris, D., Sec. Chair: Collier, F.


Integration 2.9 10:00 - 12:30 Turbulence Modeling

and Transition Chair: Mor_Yossef, Y., Sec. Chair: Bigarella, E.

Track 2 02.1 - Aerodynamics - CFD Methods

and Validation

10:00 (2.9.1) ENGINEERING APPLICATION OF GAO-YONG RATIONAL TURBULENCE MODEL TO AN INTERCOOLED DUCT Xiaotang Li¹, Wentao Zheng¹; ¹AVIC, China

10:30 (2.9.2) NUMERICAL SIMULATIONS OF TURBULENT FLOWS OVER THE ONERA-M6 AND DLR-F6 CONFIGURATIONS J. L. Azevedo, Instituto de Aeronautica e Espaco, Brazil

11:00 (2.9.3) SUPERSONIC/HYPERSONIC LAMINAR BOUNDARY LAYER OVER A SINGLE DISCRETE ROUGHNESS ELEMENT D. de Rosa, CIRA Italian Aerospace Research Centre, Italy

11:30 (2.9.4) NUMERICAL ANALYSIS OF LOW-REYNOLDS-NUMBER AIRFOIL AERODYNAMIC CHARACTERISTICS S.L. Zhang, Northwestern Polytechnical University, China

3.9 10:00 - 12:30 Student Final Chair: , Track 3

4.9 10:00 - 12:30 Design Optimization 2 Chair: ,


10:00 (4.9.1) COLLABORATIVE MULTI-LEVEL MDO PROCESS DEVELOPMENT AND APPLICATION TO LONG-RANGE TRANSPORT AIRCRAFT S. Goertz, DLR, Germany

10:30 (4.9.2) ON MORE EFFECTIVE AERODYNAMIC DATA GENERATION FOR SIMULATION BASED AIRCRAFT CONCEPTUAL DESIGN P. Raj, Virginia Tech/ AOE, United States

11:00 (4.9.3) MULTILEVEL COLLABORATIVE AERODYNAMIC DESIGN OPTIMIZATION BASED ON SOBOL’ GLOBAL SENSITIVITY ANALYSIS C.-W Wang, Northwestern Polytechnical University, China

11:30 (4.9.4) SURROOPT: A GENERIC SURROGATE-BASED OPTIMIZATION CODE FOIRAERODYNAMIC AND MULTIDISCIPLINARY DESIGN Z.-H. Han, NorthwesternPolytechnicalUniversity, China

12:00 (4.9.5) DEVELOPMENT OF VARIABLE-FIDELITY DESIGN FRAMEWORK WITH A COUPLED 3-D PANEL/NAVIER-STOKES SOLVER UNCER UNCERTAINTY Y. M. Jo, Korea Advanced Institute of Science and Technology, South Korea

5.9 10:00 - 12:30 Fatigue and Corrosion Chair: Nutt, S., Sec. Chair: Rand, O.


Tolerance

10:00 (5.9.1) DETERMINATION OF FRACTURE MECHANICS PARAMETERS FOR FATIGUE CRACKS EMANATING FROM INITIAL AND COLD-EXPANDED HOLES V.S. Pisarev, Central Aero-Hydrodynamics Institute (TsAGI), Russia

10:30 (5.9.2) VERIFICATION OF CFRP COMPONENTS FATIGUE EVALUATION PROCEDURE UNDER IRREGULAR CYCLING LOADING Pankov A.V. Pankov, TsAGI, Russia

11:00 (5.9.3) PREDICTION OF WFD OCCURRENCE IN LONGITUDINAL JOINTS OF A FUSELAGE FOR COMMERCIAL AIRPLANE A.A. Sviridov, TsAGI, Russia

11:30 (5.9.4) LIFE PREDICTION MODEL OF AIRCRAFT STRUCTURE UNDER ALTERNATE ACTION OF CORROSION AND FATIGUE YTH He, Air Force Engineering University, China

12:00 (5.9.5) DETECTION OF HIDDEN FATIGUE CRACKS IN RIVETED LAP JOINTS USING WAVELET TRANSFORM AND NEURAL NETWORKS A. ABEDIAN, sharif university of technology, Iran

6.9 10:00 - 12:30 Aeroelasticity 2


Chair: Tichy, L., Sec. Chair: Shin, S.


10:00 (6.9.1) ELASTO-STATIC AND MODAL MODELLING OF FLEXIBLE WINGS CARRYING MULTIPLE EXTERNAL STORES E. M. Amato¹, C. Polsinelli¹, E. Cestino², G. Frulla², P. Marzocca¹; ¹RMIT University, Australia ;²Politecnico di Torino, Italy

10:30 (6.9.2) INVESTIGATION OF AN INFLUENCE OF TRANSONIC FLOW VISCOSITY ON STATIC AND DYNAMIC AEROELASTICITY OF AIRCRAFT I Kuzmina, TsAGI, Russia

11:00 (6.9.3) THE EFFECT OF LOOSENED ROOT CONNECTIONS ON NONLINEAR AEROELASTIC BEHAVIOR VIA HIGHER-ORDER SPECTRA M. J. Candon, RMIT University, Australia

11:30 (6.9.4) UNSTEADY AERODYNAMIC COMPUTATIONS ACROSS MACH REGIMES BASED ON NONLINEAR SYSTEM IDENTIFICATION THEORY M. Winter, Technische Universität München, Germany

12:00 (6.9.5) NUMERICAL SIMULATION OF A TRANSONIC WIND TUNNEL TEST Q. Y. Chen, COMAC, China

7.9 10:00 - 12:30 Systems Engineering & Integration Chair: Fredriksson, B., Sec. Chair: de Boer, A.


Supply Chain

10:00 (7.9.1) REPORT FROM ICAS WORKSHOP ON SYSTEM INTEGRATION S. Ying, China

10:30 (7.9.2) SYSTEMS OF SYSTEMS ENGINEERING AND VISUAL ANALYTICS D.N. Mavris, Georgia Tech, United States

8.9 10:00 - 12:30 Hybrid-Electric and Distributed Propulsion Aircraft 2 Chair: Isikveren, A., Sec. Chair: Singh, R.

Track 8 01 - Aircraft and Systems

Integration 10:00 (8.9.1) EFFICIENCY ANALYSIS OF DISTRIBUTED PROPULSION SYSTEMS

FOR HYBRID WING BODY CONCEPT IN FP7 PROJECT DISPURSAL A. A. Mirzoyan, Central Institute of Aviation Motors (CIAM), Russia

10:30 (8.9.2) AEROPROPULSIVE PERFORMANCE ANALYSIS OF THE NOVA CONFIGURATIONS L. Wiart, ONERA, France

11:00 (8.9.3) HYBRID-ELECTRIC MOTIVE POWER SYSTEMS FOR COMMUTER TRANSPORT AIRCRAFT T. Isikveren, none, Germany

11:30 (8.9.4) ELECTRIC DISTRIBUTED PROPULSION FOR SMALL BUSINESS AIRCRAFT A CONCEPT-PLANE FOR KEY-TECHNOLOGIES INVESTIGATIONS J. Hermetz, ONERA The French Aerospatial Lab, France

9.9 10:00 - 12:30 UAV Collaborative Operations Chair: Posse, C., Sec. Chair: Belo, E.


related) 10:00 (9.9.1) VECTOR FIELD GUIDANCE LAW FOR MULTI UNMANNED AGENT

COOPERATION WY Jung, KAIST, South Korea 10:30 (9.9.2) DESIGN THE GUIDANCE LAW FOR AUTONOMOUS FORMATION

FLIGHT OF UAVS USING VIRTUAL PURSUIT POINT H.M. Shin, KAIST, South Korea

11:00 (9.9.3) NON-COOPERATIVE GROUND VEHICLE TRACKING AND INTERCEPTION BY MULTI-RPA COLLABORATION Y. Watanabe, ONERA, France

11:30 (9.9.4) SAMPLING-BASED MOTION PLANNING FOR COOPERATIVE AERIAL MANIPULATION H.I Kim, Seoul National Univ., South Korea

12:00 (9.9.5) A NOVEL NONLINEAR FLIGHTH CONTROL ALGORITHM FOR MULTICOPTERS O. Tekinalp, Middle East Technical University, Turkey

10.9 10:00 - 12:30 Transsonic Buffet Control Chair: Wood, N., Sec. Chair: Wegner, W.


Control

10:00 (10.9.1) NEW METHOD OF TRANSONIC BUFFET DECREASING ON SUPERCRITICAL AIRFOIL M.A. Brutyan, TsAGI, Russia

10:30 (10.9.2) INVESTIGATION OF FLOW CONTROL OVER THE SUPERCRITICAL AIRFOIL BY TANGENTIAL JET BLOWING AT TRANSONIC SPEEDS A.V. Albert, TsAGI, Russia

11:00 (10.9.3) NUMERICAL STUDY ON TRANSONIC BUFFET ACTIVE CONTROL BY OPEN AND CLOSED LOOP METHODS C.-Q. Gao, China

11:30 (10.9.4) EFFECTS OF LAMINAR-TURBULENT TRANSITION ON BUFFET ONSET AND TRANSONIC CHARACTERISTICS OF LAMINAR AIRFOIL W. STALEWSKI¹, K. SURMACZ¹, J. SZNAJDER¹; ¹INSTITUTE of AVIATION, Poland

12:00 (10.9.5) PLASMA CONTROL OF TRANSONIC SHOCK WAVE A. Sidorenko, ITAM, Russia

11.9 10:00 - 12:30 Trajectories Chair: Kügler, D., Sec. Chair: Lamiscarre, B.

Track 11 08 - Air Transport System

Efficiency 10:00 (11.9.1) ADVANCED RNP TO ILS AUTOLAND APPROACHES FOR OPTIMAL

BENEFITS FROM PBN: FLIGHT TESTING PROCEDURES WITH AN A320 T. Dautermann, DLR German Aerospace Center, Germany

10:30 (11.9.2) IMPACT OF WEATHER UNCERTAINTIES ON NOISE CONTOURS AND NOISE ABATEMENT DESCENT TRAJECTORIES A. Andreeva-Mori, Japan Aerospace Exploration Agency, Japan

21

11:00 (11.9.3) OPTIMAL APPROACH TRAJECTORIES FOR MULTIPLE AIRCRAFT CONSIDERING DISTURBANCES AND CONFIGURATION CHANGES M. Bittner¹, M. Rieck¹, B. Grüter¹, F. Holzapfel¹; ¹Institute of Flight System Dynamics, TUM, Germany

11:30 (11.9.4) AIR TRAFFIC EFFICIENCY EVALUATION BY TRAJECTORY OPTIMIZATION AND ADS-B DATA A. Harada, Kyushu University, Japan

12:00 (11.9.5) EFFICIENT CONTROL OF ARRIVAL TIME TO A CONGESTED AIRPORT\'S TERMINAL AREA Y. Miyazawa, Kyushu University, Japan

12.9 10:00 - 12:30 Safety & Operations of Unmanned Aircraft Systems Chair: Beccaro, A.

Track 12 09 - Safety and

Security 10:00 (12.9.1) FORMAL VERIFICATION OF AUTOPILOTS IN UMANNED AIRCRAFT

SYSTEMS B. J. Yang, Optimal Syntheis Inc., United States 10:30 (12.9.2) DETECT AND AVOID FOR REMOTELY PILOTED AIRCRAFT IN AIR

TRAFFIC CONTROL SIMULATIONS * Alfredson, Saab, Sweden 11:00 (12.9.3) THE DRONE AVIATION NAVIGATION SYSTEMS M.T TANAKA,

NAGOYA UNIV, Japan 11:30 (12.9.4) SECURE ESTIMATION FOR UNMANNED AERIAL VEHICLES

AGAINST ADVERSARIAL ATTACKS Q Hu, University of California Berkeley, United States

12:00 (12.9.5) VERTICAL POSITION ERROR BOUNDING FOR INTEGRATED GPS/BAROMETER SENSORS TO SUPPORT UNMANNED AERIAL VEHICLE (UAV) J. Lee, KAIST, South Korea

12:30 - 14:00 Lunch

1.10 14:00 - 15:30 High Speed and Access to

Space Chair: Lezoud, P., Sec. Chair: Kimmel, W.


Integration 14:00 (1.10.1) STUDY ON CONFIGURATION OF A MODULAR AIRPLANE SYSTEM

A.K. Kwiek, Warsaw University of Technology, Poland 14:30 (1.10.2) EOLE, AN INNOVATIVE FLYING SCALE DEMONSTRATOR FOR

AIR-LAUNCH-TO-ORBIT AUTOMATIC SYSTEMS J. GAUVRIT-LEDOGAR, ONERA, France

15:00 (1.10.3) CABIN ESCAPE SYSTEM: A WAY TO ENSURE CREW SAFETY DURING SUBORBITAL FLIGHTS R. Fusaro, Politecnico di Torino, Italy

2.10 14:00 - 15:30 Space Vehicle Configurations Chair: Eggers, T., Sec. Chair: Voevodenko, N.


Validation

14:00 (2.10.1) NUMERICAL SIMULATION OF AEROTHERMODYNAMIC CHARACTERISTICS OF FLOW OVER SPACE VEHICLE MODEL N. Palchekovskaya, TsAGI, Russia

14:30 (2.10.2) AERODYNAMIC ANALYSIS WITH SEPARATION DYNAMICS OF A LAUNCHER AT STAGING CONDITIONS A. Viviani, Second University of Naples, Italy

15:00 (2.10.3) NUMERICAL SIMULATION OF HYDRODYNAMIC LOADINGS ON REENTRY VEHICLE DURING SPLASHDOWN A.A. Aksenov, TESIS/CAPVIDIA, Russia

3.10 14:00 - 15:30 Scale Model Flight Testing Chair: ,


14:00 (3.10.1) SUBSCALE FLIGHT TESTING OF A GENERIC FIGHTER AIRCRAFT D. Lundstrom, Linkoping University, Sweden

4.10 14:00 - 15:30 HEXAFLY-INT Project Chair: ,


14:00 (4.10.1) NUMERICAL AND EXPERIMENTAL RESEARCH ON AERODYNAMICS OF HIGH-SPEED PASSENGER VEHICLE WITHIN THE HEXAFLY-INT PROJECT M. Marini, CIRA, Italy

14:30 (4.10.2) BOUNDARY LAYER STATE INFLUENCE ON START OF THE INWARD-TURNING INTAKE N.V. Voevodenko, TsAGI, Russia

15:00 (4.10.3) NUMERICAL AND EXPERIMENTAL INVESTIGATION OF DIFFERENT INTAKE CONFIGURATIONS OF HEXAFLY-INT FACILITY MODULE N.V. Kukshinov, CIAM, Russia

5.10 14:00 - 15:30 ISABE 2 Chair: , Track 5

14:00 (5.10.1) THE FUTURE JOURNEY OF CIVIL AEROSPACE: WEATHER, ENVIRONMENT AND CLIMATE R Singh, Emeritus Cranfield University, United Kingdom

6.10 14:00 - 15:30 Structural Dynamics Chair: Wiedemann, M., Sec. Chair: Park, C.



14:00 (6.10.1) THE SUPPORT PROCESS, SIMULATION RESEARCH DESIGN AND STRUCTURE OF THE NEW HELICOPTER’S CONSTRUCTION SCHEMATICS WITH SPECI G. Kowaleczko, Poland

14:30 (6.10.2) A STUDY OF THE ACCURACY OF GROUND VIBRATION TEST

DATA USING A REPLICA OF THE GARTEUR SM-AG19 TESTBED STRUCTURE P.G Gustafsson, SAAB AB, Sweden

15:00 (6.10.3) NOSE LANDING GEAR SHIMMY ANALYSIS AND FULL-SCALE TEST VALIDATION B. Feng, Shanghai Aircraft Design and Research Institute of COMAC, China

7.10 14:00 - 15:30 Combustion and High Speed Chair: Majjigi, M., Sec. Chair: Yan, H.


14:00 (7.10.1) HIGH SPEED OH-PLIF AND PIV MEASUREMENT IN A SNG PARTIALLY PREMIXED FLAME AT A MODEL GAS TURBINE S. P. JOO, South Korea

14:30 (7.10.2) INVESTIGATION OF THE HYDROGEN COMBUSTION CHAMBER PERFORMANCE WITHIN THE HEXAFLY-INT PROJECT V. Talyzin, TsAGI, Russia

15:00 (7.10.3) CFD MODELING TO OPTIMIZE THE MAXIMUM THRUST IN SCRAMJET ENGINE M.P. `Pires, IME, Brazil

8.10 14:00 - 15:30 Flight Modeling & Simulation Chair: Doll, C., Sec. Chair: Kim, S.

Track 8 05.1 - Flight Dynamics and Control (Control

& Modelling) 14:00 (8.10.1) FLIGHT MECHANICAL ANALYSIS OF THE ATMOSPHERIC FLIGHT

OF THE HYPERSONIC EXPERIMENT SHEFEX II A. Bierig, DLR, Germany 14:30 (8.10.2) FLIGHT DYNAMIC STABILITY ANALYSIS OF A FLEXIBLE FLYING

WING L.B. Wang, The First Aircraft Institute of AVIC, China 15:00 (8.10.3) BIFURCATION ANALYSIS OF A GENERIC PUSHER TYPE

TRANSPORT AIRCRAFT CONFIGURATION IN NEAR-STALL FLIGHT Amit Kumar Khatri, CSIR-National Aerospace Laboratories, India

9.10 14:00 - 15:30 UAV Flight Dynamics Chair: Larsson, R., Sec. Chair: Krus, P.


related)

14:00 (9.10.1) THE EFFECTS OF BODY AERODYNAMICS ON THE DYNAMIC STABILITY OF INSECT FLIGHT A.-T. Nguyen, Korea Advanced Institute of Science and Technology, South Korea

14:30 (9.10.2) FLIGHT DYNAMIC RESPONSE ANALYSIS OF THE FLEXIBLE AIRCRAFT FLYING THROUGH THE WIND FIELD OVER COMPLEX TERRAINS C. Tang, China

15:00 (9.10.3) MOBILE LAUNCHING TREBUCHET FOR UAVS B. Gati, Budapest University of Technology and Economics, Hungary

10.10 14:00 - 15:30 Hypersonic/Transitional Boundary Layers Chair: Lipatov, I., Sec. Chair: Prince, S.

Track 10 02.3 - Basic Fluid Dynamics

and Flow Control 14:00 (10.10.1) DNS OF THE DEVELOPMENT OF RANDOM DISTURBANCES IN A

HYPERSONIC BOUNDARY LAYER V. Chuvakhov, Central Aerodynamic Institute, Russia

14:30 (10.10.2) DIRECT NUMERICAL SIMULATION OF DISTURBANCES IN A 3D HYPERSONIC NEAR-WALL FLOW OVER FLAT PLATE AND COMPRESSION CORNER A.V. Novikov, TsAGI, Russia

15:00 (10.10.3) STUDY OF THE UNSTEADY STRUCTURES EVOLUTION IN SHOCK WAVE / BOUNDARY LAYER INTERACTION FOR VARIOUS UPSTREAM CONDITIONS P.A. Polivanov, ITAM SB RAS, Russia

15:30 - 16:00 Break

0.12 16:00 - 17:00 VON KARMAN LECTURE Chair: Susan Ying Chair ICAS Programme Committee

16:00 The Airbus 350 XWB Programme Gordon McConnel, Didier Evard

0.13 17:00 - 17:30 CLOSING CEREMONY Chair:

17:00

22

ACCEPTED PAPERS - CATEGORY B – STANDBY / POSTER

These papers are standby for oral presentations in case papers are withdrawn from an appropriate session. Full papers will appear in the congress CD-Rom Proceedings.

Authors are encouraged to also present their papers as posters in the Poster area.

1 - AIRCRAFT AND SYSTEMS INTEGRATION ICAS2016-1.3ST: C. Jouannet, SAAB Aeronautics, Sweden MODEL-BASED INTEGRATION OF CONCEPTUAL DESIGN AND OPERATIONAL ANALYSIS ICAS2016-1.8ST: M. I. Alam, IIT Bombay, India MULTIDISCIPLINARY DESIGN OPTIMIZATION OF STRATOSPHERIC AIRSHIP ICAS2016-1.1ST: A. Zyluk, Air Force Academy, Poland; K.-S. Sibilski, Air Force Institute of Technology, Poland; K. Falkowski, Military University of Technology, Poland SPECIFICATION, DEVELOPMENT, SIMULATION, AND EXPERIMENTAL STUDY THE SMALL-SCALED MODEL OF MAGLEV SYSTEM ASSISTED AIRCRAFT ICAS2016-1.8ST: - Pellebergs, SAAB, Sweden DETECT AND AVOID - FINDINGS AND CONCLUSIONS FROM MIDCAS ICAS2016-1.7ST: Wu Wu, NPU, China STOCHASTIC TRANSONIC AERODYNAMICS ANALYSIS ICAS2016-ST: S. Tsach, Advanced Programs Group (APG), Israel UNMANNED AUTONOMOUS AVIATION DEVELOPMENT TRENDS ICAS2016-1.6ST: L. G. GONZALEZ, EMBRY RIDDLE AERONAUTICAL UNIVERSITY, United States DETAILED AERO-STRUCTURAL DESIGN OF WINGLET FOR BUSINESS JET ICAS2016-1.2ST: K Lee, Pusan National University, South Korea MODEL ORDER REDUCTION OF INCOMPLETE SIMULATION DATA WITH PROBABILISTIC PRINCIPAL COMPONENT ANALYSIS AND KRIGING ICAS2016-1.1ST: P. Krus, Linköping university, Sweden FEASIBILITY STUDY FOR A TAILLESS AIRCRAFT WITH POST STALL MANOUVERING CAPABILITY ICAS2016-1.10ST: L. G. GONZALEZ, EMBRY RIDDLE AERONAUTICAL UNIVERSITY, United States SUPERSONIC BUSINESS JET TECHNOLOGY & MISSION TRADE STUDIES ICAS2016-1.4ST: R Vos, TU Delft, Netherlands ARE BLENDED-WING-BODY AIRCRAFT BETTER THAN TUBE-AND-WING AIRCRAFT? ICAS2016-1.3ST: Mh Zhang, School of Aeronautics, Northwestern Polytechnical University, China A CONCEPTUAL DESIGN PLATFORM FOR BLENDED-WING-BODY TRANSPORTS ICAS2016-1.6ST: I. Berlowitz, Israel Aerospace Industries, Israel DEVELOPMENT OF TYPE CERTIFICATION FOR MILITARY COMMERCIAL DERIVATIVE AIRCRAFT & TURBINE ENGINE

2.1 - AERODYNAMICS - CFD METHODS AND VALIDATION ICAS2016-2.6ST: Y.J. Choi, KAIST, South Korea NUMERICAL INVESTIGATION OF SUBSONIC RAREFIED FLOWS USING DSMC-IP METHODS ICAS2016-2.6ST: A. Jahangirian, Amirkabir University, Iran A MESHLESS METHOD FOR COMPRESSIBLE FLOW CALCULATIONS AT ALL SPEED CONDITIONS ICAS2016-2.9ST: F.J Wang, China RESEARCH ON MASSIVELY SEPARATED FLOWS AND STABILITY ANALYSIS OF AIRCRAFT ON DES MODEL ICAS2016-2.10ST: S. Mikhalyov, TsAGI, Russia OPTIMIZATION OF AEROSPACE SYSTEM PARAMETERS IN TERMS OF COMPUTATIONAL FLUID DYNAMICS SIMULATIONS ICAS2016-2.1ST: Y.-G Bai, Dalian University of Technology, China INFLUENCE OF THE RHOMBOID ZONE ON AEROELASTIC EXPERIMENTS OF SUPERSONIC AIRCRAFT ICAS2016-2.3ST: T. Iwao, Graduate School of Tokai University, Japan NUMERICAL ANALYSIS OF FOCUS BOOM AT TRANSITION FLIGHT OF SUPERSONIC TRANSPORT ICAS2016-12.3ST: S. N. Skinner, University of Glasgow, United Kingdom AEROSTRUCTURAL AND PITCH STABILITY OPTIMISATION OF NONPLANAR LIFTING SURFACES ICAS2016-2.7ST: Z.-P Li, Shenyang Engine Design and Research Institute, AVIC, China APPLICATION OF CFD TECHNOLOGY ON COMPRESSOR TEST RIG INTAKE ROOM DESIGN ICAS2016-2.9ST: Z. Li, Tsinghua University, China

23

A COMPARATIVE STUDY OF TURBULENCE MODELS IN SIMULATING A WINGTIP VORTEX ICAS2016-2.2ST: M.E. Arkhipov, Moscow Institute of Physics and Techtology, Russia PROPELLER SLIPSTREAM INTERFERENCE EFFECTS ON AIRCRAFT AERODYNAMICS ICAS2016-2.4ST: zq ZHANG, School of Aeronautics, Northwestern Polytechnincal Univ, China COMPUTATIONAL INVESTIGATION FOR FREE-FLIGHT AERODYNAMICS AND FLIGHT DYNAMICS OF SUBSONIC AND SUPERSONIC PROJECTILES ICAS2016-2.8ST: J. G. Kim, Sejong University, South Korea THERMOCHEMICAL NONEQUILIBRIUM STUDY OF O2+AR

2.2 - EXPERIMENTAL AERODYNAMICS ICAS2016-3.3ST: R. Placek, Institute of Aviation, Poland THE ROUGHNESS POSITION INFLUENCE ON LAMINAR AEROFOIL AERODYNAMIC CHARACTERISTICS IN TRANSONIC FLOW REGIME ICAS2016-3.4ST: Jia-Jian Zhou, China Academy of Aerospace Aerodynamics, China AIRFRAME NOISE RESEARCH BY MICROPHONE ARRAY TECHNIQUE IN A CLOSED WIND TUNNEL ICAS2016-3.5ST: A.-C Avelar, Instituto de Aeronautica e Espaco, Brazil EXPERIMENTAL INVESTIGATION OF UNSTEADY FLOW PHENOMENA ON AN AIRFOIL IN THE TRANSONIC REGIME ICAS2016-3.8ST: H.W Wang, China Academy of Aerospace Aerodynamics, China THE RESEARCH AND VALIDATION OF GLOBAL SKIN FRICTION FIELD MEASUREMENT BASED ON FLUORESCENT OIL FILM ICAS2016-3.4ST: L. Deng, Northwestern Ploytechnical University, China DEVELOPMENT OF HALF-MODEL TEST CAPABILITY AT THE NF-3 WIND TUNNEL ICAS2016-3.3ST: K. A. Kasim, Universiti Teknologi Malaysia, Malaysia EFFECTS OF PROPELLER LOCATIONS ON THE VORTEX SYSTEM ABOVE DELTA-SHAPED UAV MODEL

2.3 - BASIC FLUID DYNAMICS AND FLOW CONTROL ICAS2016-9.9ST: J.-L. Li, National Key Laboratory of Science and Technology on Aerodynamic, China RESEARCH ON THE IMPACT OF SHOCK WAVE TO EXTENSIONALITY OF POD METHOD ICAS2016-10.1ST: Y Yi, Beihang University, China COROTATING EQUAL STRENGTH VORTEX PAIR MERGING IN ADVERSE PRESSURE GRADIENT ENVIRONMENT ICAS2016-10.7ST: M. P. Brandao, ITA - DCTA, Brazil AERODYNAMICS VIA AEROACOUSTICS – THE CASE FOR CIRCULATION CAPTURE ICAS2016-9.10ST: RO Bura, Faculty of Mechanical and Aerospace Engineering, ITB, Indonesia TIME-DEPENDENT SIMULATION OF TRANSITIONAL SWBLI IN HYPERSONIC FLOWS WITH EFFECTS TO HEATING RATES ICAS2016-10.5ST: H. Xu, Department of Mathematics, Imperial College London, United Kingdom EFFECT OF 3D SURFACE DEPRESSION ON BOUNDARY LAYER TRANSITION ICAS2016-10.8ST: J B Samuel, Indian Institute of Technology Madras, India HIGH TEMPERATURE EFFECTS ON DNS OF SHOCK/TURBULENCE INTERACTION ICAS2016-10.3ST: S. A. Prince, Cranfield University, United Kingdom A STUDY OF THE AERODYNAMNIC CHARACTERISTICS OF AN OSCILLATORY PITCHING NACA0012 AEROFOIL ICAS2016-11.5ST: V.I. Shalaev, Moscow Institute of Physics and Technology, Russia SINGULARITIES OF LAMINAR BOUNDARY LAYER EQUATIONS AND FLOW STRUCTURE IN LEEWARD PLANE ON CONICAL BODIES ICAS2016-10.2ST: A.-J. Jahangirian, Amirkabir University of Technology, Iran NUMERICAL SIMULATION OF FLOW SEPARATION CONTROL OVER A HUMP USING DBD PLASMA ACTUATOR ICAS2016-10.4ST: Y.-F. Liu, CAAA, China NUMERICAL INVESTIGATION OF SUPERSONIC JET IN SUBSOINC/TRANSONIC COMPRESSIBLE FLOW ON AN OGIVE-CYLINDER CONFIGURATION

2.4 - APPLIED AERODYNAMICS ICAS2016-4.7ST: W. Yang, Northwestern Polytechnical University, China DEFORMATION EFFECTS ON THE PROPULSIVE EFFICIENCY OF FLEXIBLE FLAPPING-WING ICAS2016-4.3ST: Chen Lan, CAAA, China COMPUTATIONAL AND EXPERIMENTAL INVESTIGATION OF UNSTEADY CHARACTERISTICS OF VORTEX BREAKDOWN ICAS2016-4.8ST: Y Liu, AVIC Aircraft Co,. Ltd, China THE RESEARCH ON THE EFFECT OF A LARGE SWEPTBACK DORSAL FIN ON THE EFFICIENCY OF

24

VERTICAL TAIL OF A TRANSPORT AIRCRAFT ICAS2016-4.5ST: S. ZIETARSKI, MILITARY UNIVERSITY OF TECHNOLOGY, Poland OPTIMIZED AIRFOILS AND QUADRICS AS ESSENTIAL ELEMENTS FOR AN ACCURATE GEOMETRIC MODELING AND CNC MACHINING IN AIRCR ICAS2016-3.6ST: I.A. Gubanova, TsAGI, Russia RESIDUAL CORRECTION METHOD FOR MULTIELEMENT WING DESIGN ON THE BASIS OF NAVIER-STOKES EQUATIONS SOLUTION ICAS2016-4.2ST: A JAHANGIRIAN, Amirkabir University of Technology, Iran NUMERICAL STUDY OF ACTIVE SHOCK WAVE-TURBULENT BOUNDARY LAYER INTERACTION CONTROL FOR TRANSONIC AERODYNAMICS ICAS2016-3.6ST: Y. Inada, Tokai University, Japan ANALYSIS OF FLIGHT PERFORMANCE OF STREAKED SHEARWATER

3.1 - MATERIALS ISSUES, FATIGUE AND DAMAGE TOLERANCE ICAS2016-5.8ST: A. ABEDIAN, sharif university of technology, Iran INSTANTANEOUS BASELINE MULTIPLE DAMAGE DETECTION AND LOCALIZATION IN AN ALUMINIUM PLATE USING LAMB WAVES ICAS2016-12.4ST: Q. Weiqi, China Aerodynamics Research and Development Center, China ESTIMATION OF TEMPERATURE-DEPENDANT THERMAL CONDUCTIVITY OF MATERIAL WITH GENETIC ALGORITHM ICAS2016-4.9ST: V.A. Glushchenkov, SSAU, Russia DEVELOPMENT OF CRACKS IN THE SAMPLES EXPOSED TO THE PULSE MAGNETIC FIELD ACTION. ICAS2016-4.9ST: M.K. Lee, Agency for Defense Development, South Korea PREDICTION OF FRACTURE STRENGTH FOR NOTCHED LAMINATE SUBJECTED TO TENSION LOADING ICAS2016-5.6ST: Z.L. Hong, China MICROSTRUCTURES AND OXIDATION BEHAVIOURS OF PARTICLES MODIFIED PTAL BOND COATS ON NI SUPERALLOYS

3.2 - STRUCTURAL ANALYSIS AND DESIGN, STRUCTURAL DYNAMICS, AEROELASTICITY ICAS2016-6.8ST: I.V. Mareskin¹, Yu.A. Dynnikov¹; ¹DAFE MIPT, Russia MULTIDISCIPLINARY OPTIMIZATION OF PRO-COMPOSITE STRUCTURAL LAYOUTS OF HIGH LOADED AIRCRAFT CONSTRUCTIONS ICAS2016-6.5ST: H. Dastoom-L, Sharif University of Technology, Iran NONLINEAR STABILITY ANALYSIS OF CARBON NANOTUBES BASED ON TIMOSHENKO BEAM THEORY AND MODIFIED COUPLE STRESS THEORY ICAS2016-5.9ST: J.-B. Duan, Ordnance Engineering College, China A METHOD FOR THE AIRCRAFT WING FLUTTER BASED ON THE NUMERICAL DISTRIBUTED TRANSFER FUNCTION ICAS2016-5.10ST: Q.-J JIE, AVIC, China RESEARCH ON VIBRATION CHARACTERISTIC FOR VARIABLE ROTATING VELOCITY BLADES ICAS2016-12.2ST: J.-M. Yun, KAIST, South Korea SELECTION OF PARAMETERS IN SPR CAMERA SYSTEM FOR STRUCTURAL HEALTH MONITORING OF UAV MAIN WING ICAS2016-6.4ST: K.-H. Nguyen, Gyeongsang National University, South Korea A STUDY ON FAILURE BEHAVIORS OF REPAIRED COMPOSITE STRUCTURES WITH SCARF BONDED PATCH ICAS2016-6.6ST: K.-Y Ye, School of Aeronautics, Northwestern Polytechnical University, China UNCERTAINTY AND GLOBAL SENSITIVITY ANALYSIS FOR HYPERSONIC CONTROL SURFACE AEROTHERMOELASTIC ICAS2016-ST: Yang Fei, Shanghai Aircraft Design and Research Institute of COMAC, China AEROELASTIC RESPONSE SIMULATION IN AEROSERVOELASTIC(ASE) FLIGHT TEST ICAS2016-6.1ST: S. Y. Sang-Young, Konkuk University, South Korea THE SIMULTANEOUS STRUCTURAL DESIGN AND ANALYSIS OF HIGH SUPERSONAIC VEHICLE ENGINE IINLET ICAS2016-6.5ST: W Li, NASA Armstrong Flight Research Center, United States AEROELASTIC OPTIMIZATION OF A HYBRID WING BODY AIRCRAFT USING CURVILINEAR SPARS AND RIBS ICAS2016-5.9ST: A. Hermanutz, TU Muenchen, Germany PROGRESS TOWARDS THE DEVELOPMENT OF A FLUTTER DEMONSTRATOR WITH VERY FLEXIBLE HIGH ASPECT RATIO WINGS

25

ICAS2016-6.7ST: M.M. Ramos Teixeira, ITA, Brazil STRUCTURES TOPOLOGIC OPTIMIZATION BASED ON DARWIN’S EVOLUTIONARY THEORY ICAS2016-12.2ST: ZHAO XJ Zhao, China Academy of Aerospace Aerodynamics, China PANEL VIBRO-ACOUSTIC RESPONSE PREDICTION BASED ON TURBULENT BOUNDARY LAYER MEASUREMENT ICAS2016-6.6ST: W. H. Hu, Northwestern Polytechnical University, China THE INFLUENCE OF MORPHING PROCESS ON THE AEROELASTIC CHARACTERISTICS OF A FOLDING WING ICAS2016-6.3ST: A. abedian, Sharif University of Technology, Iran USING AXIOMATIC DESIGN APPROACH TO REDESIGN TILE THERMAL PROTECTION SYSTEM ICAS2016-6.2ST: R.V. Leonteva, PSC Tupolev, Russia COMPARATIVE ANALYSIS OF STATIC AEROELASTICAND DYNAMIC LOADS ON THE AIRPLANE CALCULATED BY VARIOUS AERODYNAMIC METHODS

4 - PROPULSION ICAS2016-6.10ST: J.S. Shin, Korea Aerospace University, South Korea IDDES OF A MODEL SCRAMJET ENGINE WITH A CAVITY FLAME-HOLDER ICAS2016-6.10ST: T. Yatsufusa, Hiroshima Institute of Technology, Japan APPLICATION OF FLAME MEASUREMENT TECHNIC BY DENSELY INSTALLED ION-PROBES ON 2-STROKE GASOLINE ENGINE

5.1 - FLIGHT DYNAMICS AND CONTROL (CONTROL & MODELLING) ICAS2016-8.3ST: S.Y. Oh, Korea Aerospace Industries, LTD., South Korea AN INVESTIGATION OF EFFECTS OF FLIGHT MANEUVERS ON A SUPERSONIC AIRCRAFT WITH ACTUATOR FAILURE ICAS2016-7.10ST: P. V. Kuzmin, TsAGI, Russia HEURISTIC MODEL OF NON-STEADY LONGITUDINAL AERODYNAMIC CARACTERISTICS AT HIGH ANGLES OF ATTACK

5.2 - FLIGHT DYNAMICS AND CONTROL (UAV RELATED) ICAS2016-9.3ST: T. Fricke¹, F. Holzapfel¹; ¹Technische Universität München, Germany STRATEGIES FOR MANUAL LANDING OF REMOTELY PILOTED AIRPLANES WITH LARGE TIME DELAY ICAS2016-9.1ST: K Fujita, ISAS/JAXA, Japan EFFECT OF YAW-TILTED HINGE AXIS ON DEPLOYMENT ROBUSTNESS OF MARS AIRPLANE ICAS2016-8.10ST: Y.J. Kang, Seoul National University, South Korea A NEW SOLUTION METHOD FOR SIX DEGREE OF FREEDOM FLIGHT DYNAMICS SIMULATION OF A HIGH ASPECT RATIO WING VEHICLE ICAS2016-9.2ST: S. Lee, Seoul National University, South Korea CAPTURE REGION ANALYSIS FOR FIELD-OF-VIEW CONSTRAINT MISSILE GUIDANCE LAW AGAINST MOVING TARGET ICAS2016-9.6ST: B.Y. Lee, Korea Advanced Institute of Science and Technology, South Korea ONE-VERSUS-ONE AIR-TO-AIR COMBAT MANEUVER GENERATION BASED ON THE DIFFERENTIAL GAME THEORY ICAS2016-9.6ST: T.M. Shim, KAIST, South Korea OPERATION SCENARIOS OF UNMANNED AIRCRAFT SYSTEMS INTEGRATED INTO THE KOREAN NATIONAL AIRSPACE SYSTEM ICAS2016-9.7ST: J Narkiewicz, Warsaw University of Technology, Poland OPTIMIZATION OF UAV FLEET MISSION - SIMULATION AND IN-FLIGHT DEMONSTRATION ICAS2016-9.4ST: Lei, Z. Lei, Tokyo University of Science, Suwa, Japan PERFORMANCE ANALYSIS OF SOLAR-POWERED UNMANNED AERIAL VEHICLE FOR HIGH ALTITUDE AND LONG ENDURANCE ICAS2016-8.9ST: H. Hamada, Graduate School of Tokai University, Japan FORMATION FLIGHT OF MULTIPLE QUADCOPTERS USING BLE-BASED INTER-VEHICLE DISTANCE CONTROL

6 - SYSTEMS, SUBSYSTEMS AND EQUIPMENT ICAS2016-5.5ST: H. LIU, China STRATEGIES TO ENHANCE A CONFIGURATION FOR HIGH-PRECISION MULTI DISCIPLINARY OPTIMIZATION

8 - AIR TRANSPORT SYSTEM EFFICIENCY ICAS2016-11.1ST: N. Masotti¹, C.-A. Persiani , ENAV S.p.A, Italy; O. Barrowclough, SINTEF ICT, Norway; S. Bagassi¹; ¹University of Bologna, Italy TOWARDS THE DEVELOPMENT OF AN AIRPORT SURFACE MOVEMENT GUIDANCE AND CONTROL

26

SYSTEM BASED ON REMOTE TOWERS SENSING TECHNO ICAS2016-11.2ST: F. Morscheck, DLR, Germany ANALYSES ON FORMATION FLIGHT IN A CIVIL AIR TRAFFIC SYSTEM ICAS2016-11.6ST: C.P. Posse, Boeing, United States AN IN-FLIGHT AID TO NEGOTIATE A MORE EFFICIENT FLIGHT PATH ICAS2016-10.9ST: S.R. Ramasamy, RMIT University, Australia CNS+A CRITERIA DETERMINATION AND EVALUATION FOR PERFORMANCE BASED OPERATIONS ICAS2016-11.8ST: A. Gardi, RMIT University, Australia PLANNING AND NEGOTIATION OF OPTIMIZED 4D-TRAJECTORY INTENTS IN STRATEGIC AND TACTICAL RE-ROUTING OPERATIONS ICAS2016-11.3ST: S Frank, TU Braunschweig/ Institute of Flight Guidance, Germany SENSOR CONCEPT OF HIGHLY-AUTOMATED AIRPORT TUGS FOR ENGINE-OUT TAXI OPERATION ICAS2016-10.9ST: J.A. PÉREZ CASTÁN, UPM, Spain IMPACT ON MANEUVER TERMINAL AREA CAPACITY BY INTEGRATING CONTINUOUS CLIMB OPERATIONS

9 - SAFETY AND SECURITY ICAS2016-11.9ST: W-L-L lili, Civil Aviation University of China, China STUDY ON THE SAFETY RISK AND CAPACITY OF THE ONE-WAY CIRCULATION AIR ROUTE IN CHINA ICAS2016-12.6ST: J.Z. Zhang, Beihang University, China RESEARCH ON LOAD SPECTRUM OF AERO HYDRAULIC PUMP BASED ON ACCELERATED DEGRADATION TESTING ICAS2016-12.7ST: Y. -J. Cheng, Beihang University, China FAULT DIAGNOSIS FOR ROTATING MACHINERY: AN IMAGE PROCESSING METHOD ICAS2016-12.6ST: Wang Zhenyu, NEIAS-AVIC, China DISATCH RELIABILITY ORIENED MMEL FORMULATION TECHNOLOGY RESEARCH

10 - CHALLENGE OF THE ENVIRONMENT ICAS2016-11.7ST: M Kowalski, Air Force Institute of Technology, Poland EMULSION FROM POINT OF VIEW REDUCTION OF EMISSIONS ICAS2016-11.4ST: J.-H. Seok, Korea Advanced Institute of Science and Technology, South Korea AN AVIATION EMISSION ESTIMATION ALGORITHM WITH STANDARD PROFILES AND TRACKS FOR SHORT AIR ROUTES ICAS2016-11.7ST: V. Vid¹, V. Dedesh¹, A. Lanshin, Central Institute of Aviation Motors, Russia; ¹Gromov Flight Research Institute, Russia COMPLEX OF QUANTITATIVE METRICS OF GREENHOUSE EFFECT CHANGE DUE TO CONTRAIL CIRRUS CLOUDS

11 - OPERATIONS AND SUSTAINMENT ICAS2016-9.5ST: E. Fouladi, Iran AIRLINES MAINTENACE COST ANALYSIS USING SYSTEM DYNAMICS MODELING ICAS2016-5.7ST: A.M. Gareyev¹, Y.P. Zlobina¹, I.A. Popelniuk¹; ¹SSAU, Russia IMPROVING THE EFFICIENCY AND RELIABILITY ASSESSMENT TECHNICAL STATE LIQUID SYSTEMS AIRCRAFT DURING ACCEPTANCE TESTS ICAS2016-5.3ST: E. Fouladi, Iran RELIABILITY ANALYSIS OF AGING AIRCRAFT

12 - HOST NATION ICAS2016-ST: R. Gorbushin, Central Aerohydrodynamic Institute, Russia THE ORIGIN OF WIND TUNNELS IN RUSSIA

27

ACCEPTED PAPERS - CATEGORY C - POSTERS

These papers will be presented in the Poster area Most papers will also appear in the Congress CD Proceedings

1 - AIRCRAFT AND SYSTEMS INTEGRATION ICAS2016-P1.1: Yu haisheng, hanghai Aircraft Design and Research Institute, China AN ACOUSTIC EMISSION BEAMFORMING METHOD FOR LOCALIZING RUB FAULT OF ROTOR-STATOR ICAS2016-P1.2: W.T.Gu Gu, Northwestern Polytechnical University, China PHYSICALLY-BASED MULTIDISCIPLINARY DESIGN OPTIMIZATION FRAMEWORK COUPLING AIRFRAME AND PROPULSION ICAS2016-P1.3: M.-C MA, COMAC, China A CONCEPTUAL ANALYSIS OF A CIVIL AIRCRAFT WITH REAR-MOUNTED OPEN ROTOR ENGINES ICAS2016-P1.4: Y.L.-L Li, First Aircraft Institute, China VTOL FANWING CONCEPT AND TEST ICAS2016-P1.5: K-C-J Kim, Korea Aerospace Industries, Ltd, South Korea FLIGHT TEST FOR TYPE CERTIFICATION ACQUISITION OF SMALL CIVIL AIRPLANE KC-100 ICAS2016-P1.6: M.-C MA, COMAC, China SYNTHESIZED ANALYSIS FROM DESIGN RANGE TO THE CONCEPTUAL DESIGN OF WIDE-BODY AIRLINER ICAS2016-P1.7: C.S. Song, Northwestern Polytechnical University, China EFFICIENT AERODYNAMIC OPTIMIZATION WITH HIERARCHICAL KRIGING MODEL COMBINED WITH GRADIENT ICAS2016-P1.8: N. Kuprikov, Moscow aviation institute, Russia ANALYSIS OF DESIGN AND TECHNICAL CHARACTERISRIC OF AIRPLANES OPERATION IN ARTIC REGION OF RUSSIAN FEDERATION ICAS2016-P1.9: A.G. Garstka, Warsaw University of Technology, Poland IS TO BE THE MICRODRONE

2.1 - AERODYNAMICS - CFD METHODS AND VALIDATION ICAS2016-P2.1.1: X.-RR RongRong, Northwestern Polytechnical University, China AERODYNAMIC CHARACTERISTIC COMPARISON OF THE FORWARD-& BACKWARD-SWEPT WINGS ICAS2016-P2.1.2: H. - P. Hospodar, VZLU a.s., Czech Republic METAMODEL ASSISTED GENETIC ALGORITHM FOR SHAPE OPTIMIZATION OF TRANSONIC AIRFOIL ICAS2016-P2.1.3: H,-C Chun, Konkuk University, South Korea HEAT LOAD ANALYSIS OF AIR INTAKE STRUCTURE OF HIGH SPEED VEHICLE ICAS2016-P2.1.4: Lu-Meng: L.-P. meng, tsinghua university, China NUMERICAL SIMULATION OF RICHTMYER-MESHKOV INSTABILITY WITH COMPACT-WENO SCHEME ICAS2016-P2.1.5: R. Szczepaniak, Air Force Academy, Poland COMPARATIVE ANALYSIS OF AIR FLOW IN THE COMPRESSOR OF THE GTD-350 ENGINE ICAS2016-P2.1.6: J.S Rhee, Seoul National Universtiy, South Korea A METHOD FOR A REFINEMENT OF THE MESHLESS POINT SYSTEM ICAS2016-P2.1.7: Y-F Fang, China AERODYNAMIC ANALYSIS OF FLUSH-MOUNTED STATIC PORTS PLACEMENT ON THE COMMERCIAL TRANSPORT AIRCRAFT ICAS2016-P2.1.8: K.-J. Lee, KAI, South Korea FIGHTER AIRCRAFT HIGH AOA DIRECTIONAL STABILITY IMPROVEMENT DESIGN ICAS2016-P2.1.9: Ed.-F. Falkov, State Research Institute of Aviation Systems, Russia VORTEX VISION. SIMULATION OF TRAILING VORTICES ICAS2016-P2.1.10: Q.-GP Qian, COMAC, China NUMERICAL STUDY OF FIXED TRANSITION LOCATION EFFECT ON SUPERCRITICAL WING AERODYNAMIC CHARACTERISTICS

2.2 - EXPERIMENTAL AERODYNAMICS ICAS2016-P2.2.1: K. A. Surmacz, Institute of Aviation, Poland AN AERODYNAMIC ANALYSIS OF THE 3D FLOW AROUND THE SSC-A09 AIRFOIL ICAS2016-P2.2.2: CHAO-W WANG, Chinese Aerodynamic Research and Development Center, China THE PERFORMANCE STUDY OF 0.55M×0.4M ACOUSTIC WIND TUNNEL ICAS2016-P2.2.3: W.S. Stryczniewicz, Institute of Aviation, Poland

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INVESTIGATION OF UNSTEADY TRANSONIC FLOW FIELD ABOVE AN AIRFOIL BY PIV METHOD ICAS2016-P2.2.4: Ivan Alexeevich Amelyushkin, TsAGI, Russia MATHEMATICAL MODELS AND OPTICAL INVESTIGATION OF TWO PHASE FLOWS IN WIND TUNNELS ICAS2016-P2.2.5: Dj. Vukovic, Vojnotehnicki institut, Serbia A GENERALISATION OF THE MATHEMATICAL MODEL OF INTERNAL WIND TUNNEL BALANCES ICAS2016-P2.2.6: Z. Patek, VZLU Aerospace Research and Test Establishment, Czech Republic EXPERIMENATAL AND COMPUTATIONAL STUDY OF GROUND EFFECT ON AIRFOIL SECTION ICAS2016-P2.2.7: D. Park, KARI, South Korea AN EXPERIMENTAL STUDY ON THE LOW REYNOLDS NUMBER AERODYNAMICS OF AN AIRFOIL ICAS2016-P2.2.8: S YUAN, AVIC Shenyang Engine Design & Research Institute, China TOTAL TEMPERATURE RECOVERY CHARACTERISTICS TEST TECHNIQUE BASED ON TOTAL PRESSURE CALIBRATION WIND TUNNEL ICAS2016-P2.2.9: Z.-B. Yan, Dalian University of Technology, China THE MANUFACTURE AND APPLICATION FOR COMPOSITES AEROELASTIC MODEL OF CIVIL AIRLINER WING IN FL-26 TRANSONIC WIND-TUNNEL ICAS2016-P2.2.10: F.M. Catalano, Sao Carlos School of Engineering/University of Sao Paulo, Brazil THE EFFECTS OF AN OVER-THE-WING NACELLE IN THE AERODYNAMIC CHARACTERISTICS OF A CONVENTIONAL AIRCRAFT ICAS2016-P2.2.11: V.I. Zapryagaev, ITAM SB RAS, Russia INVESTIGATION OF BRAKING SUPERSONIC PLUMES OF RE-ENTRY VEHICLE IMPINGING WITH LANDING SURFACE ICAS2016-P2.2.12: J. Cervinka, Aerospace Research and Test Establishment, Czech Republic SIMULATION OF PROPELLER EFFECT IN WIND TUNNEL ICAS2016-P2.2.13: K.-Z. Li, Dalian University of Technology, China EFFECT OF BEARING CLEARANCE ON FLUTTER CHARACTERISTICS FOR AIRCRAFT ALL-MOVABLE HORIZONTAL TAIL FLUTTER MODEL WITH ELAST ICAS2016-P2.2.14: H. D Ceron-Muñoz, School of engineering of São Carlos/ USP, Brazil EXPERIMENTAL ANALYSES OF DROOP´, WINGTIP DEVICES ON A BWB MODEL ICAS2016-P2.2.15: D. Damljanovic, Military Technical Institute (VTI), Serbia A STUDY OF WALL-INTERFERENCE EFECTS IN WIND-TUNNEL TESTING OF A STANDARD MODEL AT TRANSONIC SPEEDS

2.3 - BASIC FLUID DYNAMICS AND FLOW CONTROL ICAS2016-P2.3.1: X.-L Xie, The AVIC First Aircraft Institute, China SIMULATION OF PERFORATED PLATE SPOILER FOR CAVITY ACOUSTICS SUPPRESSION

2.4 - APPLIED AERODYNAMICS ICAS2016-P2.4.1: Zdenek Patek¹, Petr Vrchota¹, Jan Cervinka¹; ¹VZLU, Czech Republic EXPERIMENTAL AND COMPUTATIONAL STUDY OF GROUND EFFECT ON AIRFOIL SECTION ICAS2016-P2.4.2: Zhong Y Yuan, COMAC, China INVESTIGATION ON FLOW SEPARATION EFFECTS ON AIRCRAFT LONGITUDINAL MOMENT CHARACTERISTICS FOR FUSELAGE-MOUNTED AIRCRAFT

3.1 - MATERIALS ISSUES, FATIGUE AND DAMAGE TOLERANCE ICAS2016-P3.1.1: S. Langlo, Brazil DAMAGE AND FAILURE PREDICTION OF COMPOSITE ROTORCRAFT BLADES UNDER COMBINED BENDING-TORSION LOADING ICAS2016-P3.1.2: J. Y. Cho, Inha University, South Korea PREDICTION OF RESIDUAL STRESS IN FORGED AIRCRAFT LANDING GEAR COMPONENT MADE OF AL-ZN-MG-CU ALLOY DURING HEAT TREATMENT ICAS2016-P3.1.3: Y,-M Liang, China RESEARCH ON TWO WELDING METHODS FOR AN ALUMINUM ALLOY GUIDE BLADE ICAS2016-P3.1.4: WR Kang, KAIST, South Korea PERIODICALLY OSCILLATING TWO TRAILING EDGE FLAPS ACTUATED BY SHAPE MEMORY ALLOY WIRES ICAS2016-P3.1.5: H.-S. Lee, Korea Aerospace Research Institute, South Korea A STUDY ON MICROSTRUCTURE OF FRICTION STIR WELDED AA2195 SHEETS

3.2 - STRUCTURAL ANALYSIS AND DESIGN, STRUCTURAL DYNAMICS, AEROELASTICITY ICAS2016-P3.2.1: M.A. Pronin, TsAGI, Russia EXPERIMENTAL COMPARISON OF LIMIT CYCLE METHOD WITH PHASE RESONANCE AND PHASE SEPARATION METHODS

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ICAS2016-P3.2.2: Z.H. Wu, Nanjing University of Science and Technology, China A FOLDABLE FLAPPING WING DESIGN INSPIRED BY THE WRIST-ELBOW ANATOMY OF BATS ICAS2016-P3.2.3: hou yingyu, China Academy o f Aerospace Aerodynamics, China SOLAR UAV GUST LOAD AMENDMENT ICAS2016-P3.2.4: L. F. Ferreira, UFMG, Brazil GROUND VIBRATION TEST USING ACOUSTIC EXCITATION - APPLICATION ON A COMPOSITE WING ICAS2016-P3.2.5: G.C. Fonseca, ITA - Instituto Tecnologico de Aeronautica, Brazil NUMERICAL SIMULATION IN FINITE ELEMENT METHOD AND MANUFACTURING OF LUG MATERIAL COMPOSITE BY RTM PROCESS ICAS2016-P3.2.6: C Ji, CAAA, China RESEARCH ON FLUTTER TEST TECHNIQUE IN HYPERSONIC WIND TUNNEL ICAS2016-P3.2.7: E.S. Dias, Brazil BEARING STRENGTH ASSESSMENT OF COMPOSITE MATERIAL THROUGH NUMERICAL MODELS ICAS2016-P3.2.8: B. Rasuo, University of Belgrade/Faculty of Mechanical Engineering, Serbia THE EFFECT OF LAMINATE LAY-UP ON THE FLUTTER SPEED OF COMPOSITE STABILIZERS ICAS2016-P3.2.9: P. C. Cheng, Shanghai Aircraft Design & Research Institute, China LOAD TRANSFER IN AEROELASTICITY BASED ON RADIAL BASIS FUNCTION ICAS2016-P3.2.10: L.M.F. Barbosa, Demec UFMG, Brazil STUDY OF THE COMPROMISE OF AERODYNAMIC AND STRUCTURE STANDPOINTS IN A HIGH-ASPECT RATIO WING DESIGN

4 - PROPULSION ICAS2016-P4.1: A. C. Marta A. C. Marta, IST, Portugal ON ACOUSTIC-VORTICAL-ENTROPY WAVES IN PROPULSION SYSTEMS ICAS2016-P4.2: A.E. Kishalov¹, K.V. Markina¹, D.A. Akhmedzyanov¹, V.D. Lipatov¹; ¹USATU, Russia KEY FEATURES FORECAST OF BYPASS TURBOJET ENGINE WITH MIXING FOR PERSPECTIVE AVIATION COMPLEXES ICAS2016-P4.3: N. Valery Grigorievich , Moscow Aviation Institute, Russia IMPROVEMENT OF THE DESIGN AND METHODS OF DESIGNING TUBULER AIR-TO-AIR HEAT EXHANGERS COOLING SYSTEMS OF GAS TURBINES ICAS2016-P4.4: S.Q.-C Shengqi, 38th Research Institute of China Electronic Technology Group Cor, China PERFORMANCE TEST FOR HIGH ALTITUDE AIRSHIP'S PROPULSION SYSTEM BASED ON PROPELLER SIMULATOR ICAS2016-P4.5: Ma Wensheng, AVIC Shenyang Aeroengine Research Institute, China LABYRINTH SEALS DYNAMIC COEFFICIENTS AND CRITICAL SPEED RESEARCH BASE OF CHILD’ MODEL ICAS2016-P4.6: cjh cui, AVIC Shenyang Engine Design and Research Institute, China NUMERICAL SIMULATION OF RCS FOR A SPHERICAL CONVERGENT FLAP NOZZLE WITH A NON-RECTANGULAR DIVERGENT DUCT ICAS2016-P4.7: N Liu Liu, Shanghai Aircraft Design and Research Institute, China LINEAR MODELING BASED ON INSTRUMENTAL MODEL ESTIMATION AND PID PARAMETERS TUNING IN FREQUENCY-DOMAIN OF AIRCRAFT ENGINE ICAS2016-P4.8: V. Baklanov, Tupolev Design Bureau, Russia DYNAMICS AND VIBRATION OF NEW GENERATION AVIATION ENGINES ICAS2016-P4.9: Z-H-Y HaiYang, China Aerodynamics Research and Development Centre, China NUMERICAL INVESTIGATION OF FLOW STRUCTURE OF DIFFERENTIAL EJECTORS ICAS2016-P4.10: J.G. BAK, Hanyang Univeristy, South Korea FEASIBILITY STUDY OF HYBRID ELECTRIC PROPULSION SYSTEM FOR FIXED-WING VSTOL UAV ICAS2016-P4.11: Liu Xiao wen, China NUMERICAL INVESTIGATION OF INLET STARTING CHARACTERISTICS ICAS2016-P4.12: V. Levin, Institute of Mechanics, Moscow State University, Moscow, Russia RESEARCH OF PRESSURE PULSATIONS OF ON THE ANNULAR NOZZLE THRUST WALL ICAS2016-P4.13: A. Kartashev, South Ural State University, Russia RESEARCH OF FLOW IN STAGE OF TURBINE AND OPTIMAL MODES OF MICRO GAS TURBINE POWER PLANT ICAS2016-P4.14: L.S. Yanovskiy, CIAM, Russia THE FOAMING PROPERTIES OF LUBRICATING OILS FOR AIRCRAFT GAS TURBINE ENGINES

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5.1 - FLIGHT DYNAMICS AND CONTROL (CONTROL & MODELLING) ICAS2016-P5.1.1: B. Rasuo, University of Belgrade/Faculty of Mechanical Engineering, Serbia GENERAL APPROACH TO THE ANALYSIS OF THE ASYMMETRICALLY LOADED AIRPLANE FLIGHT LIMITATIONS ICAS2016-P5.1.2: L Jia, PLA Naval Aeronautical and Astronautical University, China HANDLING QUALITIES PREDICTION BASED ON ADAPTIVE OPTIMAL CONTROL PILOT MODEL ICAS2016-P5.1.3: O.D. Kreerenko, Beriev Aircraft Company, Russia SYNTHESIS OF CONTROL LAWS OF AEROSPACE SYSTEM BASED ON A SYNERGISTIC APPROACH ICAS2016-P5.1.4: J.G Park, KoreanAir, South Korea MODEL FOLLOWING CONTROL FOR MD500 HELICOPTER ICAS2016-P5.1.5: F Cappello, Royal Melbourne Institute of Technology, Australia AUGMENTATION OF AIRBORNE SURVEILLANCE INFORMATION WITH 6-DOF AIRCRAFT DYNAMICS MODEL ICAS2016-P5.1.6: Yi Wang Wang, College of Aerospace Science and Engineering, National Universit, China THE EFFECT OF SATELLITE FORMATION FLYING ON AUTONOMOUS NAVOGATION ICAS2016-P5.1.7: D Lee, KAIST, South Korea OPTIMAL GUIDANCE LAW FOR COOPERATIVE ATTACK OF TWO MISSILES WITH COUPLED TERMINAL VELOCITY CONSTRAINT

5.2 - FLIGHT DYNAMICS AND CONTROL (UAV RELATED) ICAS2016-P5.2.1: M. Ariola, Università di Napoli Parthenope, Italy MODEL PREDICTIVE CONTROL FOR A SWARM OF UAVS ICAS2016-P5.2.2: S. Serokhvostov, MIPT DAFE, Russia OPTIMIZATION OF THE TRAJECTORY AND ACCUMULATOR MASS FOR THE SOLAR-POWERED AIRPLANE ICAS2016-P5.2.3: F. Schettini, University of Pisa, Italy NONLINEAR MODEL IDENTIFICATION OF A SMALL-SCALE UNMANNED ROTORCRAFT ICAS2016-P5.2.4: Ki-Duck. K.D. KIM, Korea Advanced Institute of Science and Technology, South Korea OPTIMAL ASCENDING TRAJECTORY DESIGN OF HIGH ALTITUDE LONG ENDURANCE UAVS USING THE JET STREAM MODEL

6 - SYSTEMS, SUBSYSTEMS AND EQUIPMENT ICAS2016-P6.1: CY Cheng, Chengdu Aircraft Design and research Institute, China A TEST METHOD BASED ON AIRCRAFT PLATFORM FOR ATMOSPHERIC LASER VISIBILITY ICAS2016-P6.2: HONGWEI ZHAO¹, SHIHUI DUAN¹, JIANMIN FENG¹; ¹Aircraft Strength Research Institute of China, China STUDY OF PID TUNING METHOD FOR MULTIPLE-CHANNEL STRUCTURAL FATIGUE TESTING SYSTEM ICAS2016-P6.3: B. Li, COMAC, China AUXILIARY POWER UNIT (APU) PERFORMANCE EVALUATION AND INTER-SYSTEM PERFORMANCE MATCHING ANALYSIS FOR CIVIL AIRCRAFT ICAS2016-P6.4: H. LIU, China GLOBAL OPTIMIZATION ON SENSORS INTEGRATED TO ACHIEVE HIGH-LEVEL ACCURACY ICAS2016-P6.5: J.W. Bae, Korea Aerospace Research Institute, South Korea DEVELOPMENT OF GBAS INDEPENDENT PERFORMANCE MONITORING SYSTEM ICAS2016-P6.6: J Zang, AVIC Development Research Center, China COMBAT EFFECTIVENESS EVALUATION-ORIENTED AVIONICS SYSTEM MODELING ICAS2016-P6.7: D. Wang, COMAC, China ESTIMATION OF APU COMPARTMENT DRAINAGE CAPABILITY

8 - AIR TRANSPORT SYSTEM EFFICIENCY ICAS2016-P8.1: D. Steiner, Johannes Kepler University Linz, Austria IN-FLIGHT PROVISIONING AND DISTRIBUTION OF ATM INFORMATION ICAS2016-P8.2: F. Lucchi¹, S. Bagassi¹, F. De Crescenzio¹, F. Persiani¹; ¹University of Bologna, Italy HUMAN MACHINE INTERFACE DESIGN FOR SINGLE PILOT OPERATIONS ICAS2016-P8.3: A. Kan, FSUE GosNIIAS, Russia INTEGRATED RESEARCH SIMULATION STAND ADVANCED AIR TRAFFIC CONTROL SYSTEMS

9 - SAFETY AND SECURITY ICAS2016-P9.1: H. Yuan¹, C. Lu¹, Z.-Y Wang¹, F.-M. Li, Chinese Flight Test Establishment, China; ¹Beihang University, China MAKING HEALTH MANAGEMENT MORE CONCISE AND EFFICIENT: AIRCRAFT CONDITION MONITORING BASED ON COMPRESSED SENSING

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11 - OPERATIONS AND SUSTAINMENT ICAS2016-P11.1: D. Kiselev, Samara State Aerospace Univers, Russia CONTROL OF CONDITION OF GAS TURBINE ENGINE ROTOR BEARINGS IN DIAGNOSTIC PARAMETERS IN A DIFFERENT PHYSICAL NATURE

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Technical Tours The Congress participants are invited to visit a number of research centers and enterprises of the aeronautical engineering industry which are located in Korea. They will see the manufacturing and experimental capabilities, research and training laboratories, and have meetings with the leading scientists and professionals.

[TT01] Technical Tour 01: KARI

Korea Aerospace Research Institute (KARI) KARI is contributing to the sound development of the national economy improving the quality of people’s lives through the development of aerospace technology, and realizing the dream of sky and space of the Republic of Korea. Address 169-84, Gwahak-ro, Yuseong-gu, Daejeon 305-806, Korea Course Satellite Integration & Test Center → Aircraft Structures and Flight Control Laboratory → Satellite Application Cooperation Center

[TT 02] Technical Tour 02: KAI

Korea Aerospace Industries, Ltd. (KAI) Korea Aerospace Industries, Ltd. (KAI) has been orienting towards the world’s first-class aerospace company and leading the development of Korea’s aerospace industry with an indomitable challenging spirit, laying a groundwork for leading to the global aerospace company. Address HQ78, Gongdanro 1-ro, Sanam-Myeon, Sacheon, Gyeongsangnam-do, Korea

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[TT 03] Technical Tour 03: Aerospace Systems T&E Centerin Agency for Defense Development

Agency for Defense Development (ADD) Aerospace Systems Test and Evaluation Center (ASTEC) in ADD has the capability of integrated test & evaluation for EMC, Environmental and Flight tests. EMC and Environmental tests can be done for air/ground/naval/missile weapon systems including commercial items. Three 950Hp Turboprop aircrafts are operated for captive flight tests to validate performance of electronic equipment and commercial equipment and development flight test for airborne weapon system. There are the fixed and the mobile telemetry systems which have the capacity of data acquisition from more than 200km distance. Address Headquarters- 34188, P.O. Box 25, Yuseong-gu, Daejeon , Korea Haemi Flight Test Field- 32035, P.O. Box 1, Haemi-myeon, Chungcheongnam-do, Korea

* For further information, please contact ICAS 2016 Local Secretariat on [email protected]

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Social Programme Lunch & Coffee Break (Morning/Afternoon)

Date 26 September 2016 – 29 September 2016 Morning and Afternoon Teas will be served on the 1st and 2nd lobby of DCC to enable delegates to view the displays and network with colleagues. Lunches will be served at Room 112 on the 1st floor of DCC.

Welcome Reception

Date 25 September 2016 Place Terrace, 2F, DCC

Attendees Included for fulltime delegates and accompanying persons

After registering, join fellow delegates for a warm Daejeon welcome to the Congress. Night view of Daejeon and finger food with beverages will be prepared.

Congress Reception

Date 26 September 2016 Place Cheong Nam Dae (Presidential Villa)

Attendees Included for fulltime delegates and accompanying persons

It will be held at unique scenery around lake Daecheong-Ho and special dinner as well as night view will be prepared.

Student Party

Date 27 September 2016 Place Auditorium (#E15), KAIST

Attendees Included for fulltime student registrants It will be a great opportunity for students to get together, and more importantly, to become acquainted with new peers in fields of aeronautical sciences.

Congress Banquet

Date 29 September 2016 Place Grand Ballroom, 2F, DCC

Attendees The Congress Banquet is not included in the registration, and tickets must be purchased in advance.

Enjoy a delicious dinner and entertaining performance, and mingle with colleagues from all over world.

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General Information

LOCATION AND DATES

The 30th ICAS Congress will be held at the Daejeon Convention Center (DCC), Daejeon, Republic of Korea from Sunday, 25 September to Friday, 30 September, 2016

CONFERENCE LANGUAGE

Official Language is English.

REGISTRATION

Registration Fees: The ICAS Executive Committee fixed the fees as follows:

Category 2016 Registration (EUR, €)

Early; (by 30 June)

Normal; (1 July – 31 August)

Late; (from 1 September)

Member (Any ICAS Member Society or ICAS Associate Member organization)

610 730 800

Non-Member 740 900 970

Student (Undergraduate or graduate full time students, who will not have completed doctorate studies by the date of the congress)

106 106 106

Retired Person (Above 65 years of age)

410 410 410

Accompanying Person (All accompanying person must be registered)

0 0 0

Registration Inclusions

Member - Congress sessions - Morning and Afternoon Coffee & Tea, lunches on Sep. 26–29 - Welcome Reception - Congress Reception - Student Party (Only included in Student Registration) - Congress Bag: - Name Badge, Final Programme, Proceedings

Non-Member

Student

Retired Person

Accompanying Person - Welcome Reception - Congress Reception

- The student verification section of the registration MUST be completed and signed.

- Student registrations without this section completed will be returned to the applicant.

- Participants can complete the registration online at www.icas2016.com.

- All attendees must complete the online registration form indicating all the meetings and events they would like to attend.

- Please register no later than 23 September 2016 through the ICAS 2016 website and online registration system.

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REGISTRATION & INFORMATION DESK

The registration desk, located on the 1st floor of Daejeon Convention Center (DCC) will be open during the following hours:

Sunday 25 September 16:00–19:00 Monday 26 September–Thursday 29 September 08:00–17:00

REGISTRATION POLICY

Cancellations must be notified in writing to ICAS Local Secretariat. If received before or on 25 August 2016, registration fees will be refunded less 20% to cover administration costs. After 25 August 2016, no refunds will be given. This also includes the costs of the congress banquet. As an alternative to cancellation, your registration may be transferred to another person without penalty, provided a registration form with new details is submitted.

METHODS OF PAYMENT

Please choose and indicate on your registration form; one of the three methods of payment noted below. All prices are in Euro and are inclusive of GST.

i) Credit Card

- Visa, Master Card and American Express are accepted. Please note that debits to your credit card will appear as KSAS (The Korean Society for Aeronautical & Space Sciences) on your credit card statement.

- Payment through credit card at venue is available. Please check your credit card prior to this congress whether it can be used at international area or not.

ii) Cash

- Payment through cash is available at registration desk only during Congress and should be made in Euro or KRW (Korean Won).

iii) Bank Transfer

Please contact the ICAS 2016 Local Secretariat ([email protected]) for Bank transfer details.

Bank Transfer Account Holder The Korea Society for Aeronautical and Space Sciences (KSAS)

Account Number 186-04051-244-01

Bank Name CITIBANK KOREA

Swift Code CITIKRSX Bank Address 39, Da-Dong, Jung-Gu, Seoul, KOREA

- Please make the bank transfer to account specified. (Sender's name MUST BE identical with registrant's name)

- All bank remittance charges are to be paid by registrants.

- In order to confirm your payment, please send the remittance slip via e-mail ([email protected]) or fax (+82-42-472-7459).

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Upon receiving your registration form and payment, ICAS 2016 Local Secretariat will send you a confirmation by email.

For further information concerning registration and payment, please contact:

Genicom Co., Ltd. (ICAS 2016 Local Secretariat)

2F, 927 Tamnip-dong, Yuseong-gu, Daejeon, Korea 34036

Fax: +82-42-472-7459

Email: [email protected]

CONGRESS PROCEEDINGS

The ICAS 2016 Congress proceedings will be available at the Congress. The proceedings are included in the registration fee where indicated. Additional Congress Proceedings can be ordered on the registration form at a cost of 100 EUR.

OFFICIAL INVITATION LETTER

Official invitation letter will be issued upon requests of those who complete the registration including payment. The letter will be sent from KSAS (The Korean Society for Aeronautical & Space Sciences).

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APPLICATION FOR VISA

1 Visitors who plan to stay in Korea for longer than 90 days must obtain a visa before entering Korea.

2. Nationals of those countries or regions with which Korea has signed a visa waiver agreement can enter without a visa, on the condition that they do not engage in remunerative activities during their stay.

[Nationals of countries or regions allowed for visa-free entry (up to 30 days unless noticed otherwise)]

Continents Countries or Regions

Asia or regions (6) Brunei (30 days), Hong Kong (90 days), Indonesia (diplomatic and official, 30 days), Japan (90 days), Macau (90 days), Taiwan (90 days)

America (8) Argentina (30 days), Brazil (90 days), Canada (6 months), Ecuador (90days), Guyana (30 days), Honduras (30 days), Paraguay (30 days), United States (90 days)

Europe (11) Albania (30 days), Andorra (30 days), Bosnia-Herzegovina (30 days), Croatia (90 days), Cyprus (30 days), Monaco (30 days), Montenegro (30 days), San Marino (30 days), Serbia (90 days), Slovenia (90 days), Vatican (30 days)

Oceania or regions (13)

Australia (90 days), Fiji (30 days), Guam (30 days), Kiribati (30 days), Marshall Islands (30 days), Micronesia (30 days), Nauru (30 days), New Caledonia (30 days), Palau (30 days), Samoa (30 days), Solomon Islands (30 days), Tonga (30 days), Tuvalu (30 days)

Mid- East and Africa (12)

Bahrain (30 days), Egypt (30 days), Kuwait (30 days), Lebanon (diplomatic and official 30 days), Mauritius (30 days), Oman (30 days), Qatar (30 days), Saudi Arabia (30 days), Seychelles (30 days), South Africa (30 days), Swaziland (30 days), United Arab Emirates (30 days)

3. Visa application should be made at Korean embassies or consulates abroad.

4. Visa applicants are required to submit passport, application forms, a recent passport-size color photograph, and other relevant documents as determined by their status of stay.

5. For more detailed information about VISA issuance, please visit the Ministry of Affairs of Republic of Korea website (http://www.mofa.go.kr/ENG).

• Please kindly note that ICAS 2016 Local Organizing Committee cannot directly intervene on visa matters.

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Accommodation

ICAS 2016 Local Organizing Committee is pleased to offer a wide selection of hotels with discounted rates near the venue (DCC). As rooms will be reserved on a first-come, first served basis, once room blocks at these hotels have been filled, we may not be able to secure further rooms with the hotels at the special rates quoted.

ICAS 2016 DAEJEON Hotel Contract

No Hotel Type Contract Room No.

Room Rate (KRW)

Breakfast (KRW)

Distance from Venue

1 Lotte City Hotel Double 50 140,000

18,400 3 min. on foot Twin 100 150,000

2 Hotel ICC Single 25 60,000 Incl. 1 Person

5 min. on foot Twin 25 80,000 Incl. 2 Persons

3 Hotel Riviera Standard 60 121,000

18,000 18 min. by car Deluxe 20 121,000

4 Yousung Hotel Standard 100 110,000 16,000 18 min. by car

5 Hotel Interciti Double 50 150,000

20,000 16 min. by car Twin 50 150,000 Deluxe 20 170,000

6 Toyoko Inn Standard - 60,500

Incl. 1 Person

10min. by car 7 Nuvotsar Standard 25 88,000 10min. by car

8 Graytone Hotel Single 10 54,000

12min. by car Double 10 66,000 Twin 10 74,000

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[H1] Lotte City Hotel

Manager Mr. Woo-chul Park

Contact +82-42-333-1000

Website http://www.lottehotel.com/city/daejeon/en/Default.asp

Address 4-30, Doryong-dong, Yuseong-gu, Daejeon, Korea

Distance from Venue 3 min. on foot

[H2] Hotel ICC

Manager Ms. Ju-young Lee

Contact +82-42-866-5050~5052

Website http://hotelicc.com/eng/index.do

Address 4-29, Doryong-dong, Yuseong-gu, Daejeon, Korea

Distance from Venue 5 min. on foot

[H3] Hotel Riviera Manager Mr. Young-woo Lee

Contact +82-42-823-2111

Website http://www.shinan.co.kr/yusong/eng/index_yuseong.asp

Address 7 Oncheonseo-ro Yuseong-gu, Daejeon, Korea

Distance from Venue 18 min. by car

[H4] Yousung Hotel Manager Mr. Hae-sik Chung

Contact +82-42-820-0100

Website http://www.yousunghotel.com/eng/index.do

Address 9 Oncheon-ro, Yuseong-gu, Daejeon, Korea


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[H5] Hotel Intercity

Manager Mr. Dong-won Seo

Contact +82-42-600-6000

Website http://www.hotelinterciti.com/

Address 92 Oncheon-ro, Yuseong-gu, Daejeon, Korea


[H6] Toyoko Inn

Contact +82-42-545-1045

Website http://www.toyoko-inn.com/eng/index.html

Address 13, Dunsanjung-ro 134beon-gil, Seo-gu, Daejeon, Korea


[H7] Nuvotsar

Manager Mr. Hyung-Man Choi

Contact +82-42-488-2900

Website 922 Dunsan-Dong, Seo-gu, Daejeon, Korea

Address http://www.nuvostar.net/eng/index.asp


[H8] Graytone Hotel

Contact +82-42-482-1000

Website http://www.graytone.co.kr/

Address 922 Dunsan-Dong, Seo-gu, Daejeon, Korea


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Tour Information

Healing Courses in Daejeon

Red Clay Road in Mt. Gyejok Forest Lodge of Mt. Jangtae Mt. Gyeryong National Park

Along with the Mt. Gyejok Premium 100-ri Forest Trail, this beautiful trail is found in Jang-dong Recreational Forest. Visitors can take a pleasant barefoot walk along this 13km-long loess trail from spring to fall.

Mt. Jangte Forest (300,000 pyeong) is the first recreation forest built by the private fund in South Korea. It has accommodation facilities, fish farm, deer farms, and a children’s playground.

Mt. Gyeryong is 845.1m above sea level and was made a national park in 1968. The origin of the word Gyeryong comes from the fact that the ridgeline looks like a dragon wearing a chicken's crest on its head.

Unique Courses in Daejeon

Hanbat Arboretum EXPO Science Park Yuseong Hot Spring

This arboretum is located in the center part of the Daejeon Government Complex and the Expo Science Park. This is the hub of culture and art that embraces the Daejeon Art Center, Pyeongsong Youth Cultural Center, City Art Musuem, and the Lee Eungno Gallery.

The Expo Science Park was established to commemorate the Daejeon Expo held in 1993, to encourage the development of cutting edge industry, to raise awareness of science and technology. Through the Expo Re-creation Project, the Expo Science Park was designated as `City Restoration Priority Area` (September, 2008) as a long term development strategy.

The Yuseong Hot Spring is located in Bongmyeong-dong, Yuseong-gu of Daejeon City. Yuseong is famous for hot springs. Yuseong improves every day. Many education institutions including Chungnam National University and Daeduck Research Complex known as the science center of Korea are located in Yuseong.

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Night of Daejeon City

Dunsan Area (Dunsan-dong) Ui-neung-jeong-i Cultural Street Expo Bridge

Dunsan-dong is one of the most-visited places in Daejeon to have shopping together with the Ui-neung-jeong-i Cultural Street. There are many shops and restaurants. It takes 15 minutes from venue(DCC). Also there is the Galleria Department Store which is high-class department store with quality customer service.

Ui-neung-jeong-i Cultural Street was the center of the government administration, business and traditional culture in the central region from the 1960s to the 1980s. Now, it is emerging as an art and cultural street. About 150 art and culture-related shops and facilities are clustered along this street.

Expo Bridge is the one of the special site in Daejeon. Many people visit the Expo Bridge to ride a bycicle or to exersice with their family at night. Walking the bridge as well as riding a bycircle is good way to enjoy the Expo bridge. (It is car-free bridge.) A musical fountain show often takes place around this bridge.

Sightseeing around Daejeon

Sejeong City Gongju City

Sejong City is located in the central inner area of Chungcheongnam-do, and stretches south-north. Consequently, from ancient times, the current city areas were divided by the Mt. Charyeong and the Geum River into parts of Jeoneui, Yeongi, and Geumnam. But, with the development of streets in recent decades, those areas were combined into one.

Gongju is located in the center of South Korea and of South Chungcheong Province. Two major mountains are located near Gongju (Mt. Charyong and Mt. Gyeryong), and Geum River runs through the city from east to west. Several tributary rivers such as Yugu-cheon, Jeongan-cheon, Daekyocheon, Jemin-cheon, and Hyoljeo-cheon meet here.

• For further information, please contact ICAS 2016 Local Secretariat on [email protected].

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PRE & POST CONGRESS TOURS

Course 1. Jeonju Traditional Areas

Itinerary Gyeonggi-Jeon (Royal Palace) → Lunch → Jeonju Hanok Village → Wanju Healjo Town

Gyeonggijeon Shrine was erected in 1410 and holds the portrait of King Tae-jo, the founder of the Joseon Dynasty. The King and his wife’s mortuary tablets are enshrined here at Jogyeong Shrine. Gyeonggijeon is located around Hanok Village. There are over 800 traditional Korean 'hanok' houses at the village. Gyeonggi-Jeon and Jeonju Hanok Village are currently the newest hot spot for foriegners. It is a great place to experience wearing traditional clothes called Hanbok while touring the city. It will be a great opportunity to enjoy the Korean food, clothing, and shelter. Finally, light festival held in Wanju Healjo Town helps restoring the soul and gives visitors unique experiences.

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Course 2. Korea Tradition and Modernity [Seoul]

Itinerary Samsung Innovation Museum → Lunch → Gyeong-bok-gung (Royal Palace) → Insa-dong

The capital city of Korea, Seoul, is the biggest city which has special culture including past and present Korea. Samsung Innovation Museum is a business hall as well as the largest sized industrial electronics museum in Korea, displaying the growing steps of Samsung Electronics Corporation at a glance. Gyeongbokgung was constructed in 1395 as the first royal palace of the Joseon Dynasty, and it has been the main royal palace among the five grand palaces during the Joseon Dynasty. Many buildings including the Throne Hall Geunjeongjeon, Gyeonghoe-ru Pavilion and Hwangwonjeong Pond are very well preserved. The Changing of Guards ceremony performed in front of the palace gate is a must-see when visiting the area. Insa-dong Street is one of the most memorable attractions in Seoul and represents the focal point of Korean traditional culture and crafts. The street offers rich opportunities for visitors to experience Korean traditional culture and arts.

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Course 3. Baekje Historic Areas [UNESCO World Heritage Site]

Itinerary Busosanseong Fortress of Buyeo → Lunch → Jeongnimsa Temple Site → Neungsan-ri Ancient Tombs

Located in the mountainous mid-western region of the Republic of Korea, this historic area comprises eight archaeological sites dating from 475 to 660 AD, including the Gongsanseong fortress and royal tombs at Songsan-ri related to the capital, Ungjin (present day Gongju), the Busosanseong Fortress, the Jeongnimsa Temple, and the Neungsan-ri Ancient Tombs related to the capital, Sabi (now Buyeo), the royal palace at Wanggung-ri and the Mireuksa Temple in Iksan related to the secondary Sabi capital. Together, these sites represent the later period of the Baekje Kingdom during which time they were at the crossroads of considerable technological, religious (Buddhist), cultural and artistic exchanges between the ancient East Asian kingdoms in Korea, China and Japan. These places will be the where you want to refresh your mind and soul with nature.

* For further information, please contact ICAS 2016 Local Secretariat on [email protected].

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Travel TRANSPORTATION

i) Limousine Bus

Step 1) Buy an Airport Limousine Bus ticket at the International Airport

The bus stop which is located at platform 9D in 1st floor. It will take 2 hours and 40 minutes (160 minutes) by bus. (Gimpo: Bus Stop #1 around Gate 1 in 2nd floor)

* Incheon International Airport

* Gimpo International Airport

Route Normal Late-night Incheon Int’l Airport - Daejeon KRW 23,100 KRW 25,400 Gimpo Int’l Airport - Daejeon KRW 14,300 -

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Step 2) Take an Airport Limousine Bus at bus stop.

You can purchase the ticket near the platform 9D (Gimpo: Bus Stop #1 around Gate 1 in 2nd floor) or at the ticket booth inside the terminal building near the 1st floor gate 5 or 8 and this bus will not go through the rest area normally. Therefore, please drop by toilets in the terminal building before getting on the bus.

Step 3) Get off at the Daejeon Government Complex Stop and travel to Congress venue or your hotel.

It will stop at 4 locations in Daejeon. And the third stop (Daejeon Chungsa or Daejeon Government Complex Station) is the best stop for you to get off. When you get off in Daejeon, it is highly recommended to take a taxi to go to your destination.

ii) KTX Train (Korean Train eXpress)

There are two ways from Incheon International Airport to Daejeon Station. One is to take KTX express trains that directly link to and from Incheon International Airport to Daejeon Station without transit. However, KTX between Incheon International Airport and Daejeon Station runs only five or six times a day and approximately the cost is KRW 37,000. Another one is to take AREX Express from Incheon International Airport to Seoul Station, and take KTX express trains departing from Seoul Station to Daejeon Station. KTX between Seoul and Daejeon runs at 15-minute intervals from about 05:20 to 23:20. It will cost KRW 24,000 approximately.

Step 1) Move to transportation center on the first basement level.

KTX between Incheon International Airport and Daejeon Station runs only five or six times a day. For the booking the KTX ticket in advance, please refer to the KTX website: http://www.letskorail.com/ebizbf/EbizBfIndex.do

Step 2) Walk to Station and buy a ticket at ticket office.

Time Approx. 2 hours (120 minutes) Fee Approx. KRW 37,000

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Step 3) Get off at Daejeon station.

When you get off the Daejeon, it is highly recommended to take a taxi to go to your destination. It will take about 30 min. from Daejeon station to Venue and will cost KRW 8,000 approximately

EMERGENCY PHONE NUMBER

According to a survey conducted 2015, South Korea was chosen as the world’s safest nation among 120 countries. South Korea has never been under attack from terrorist group. Possession of guns as well as drugs are prohibited and penalized by law. Also Perfect order reigned throughout the country.

129 Medical Emergency, First Aid Services 119 Emergencies for Fire, Rescue & Hospital Services 112 Police

CLIMATE

Korea’s climate is regarded as a continental climate from a temperate standpoint and a monsoon climate from a precipitation standpoint. The climate of Korea is characterized by four distinct seasons. Spring and Autumn are rather short, Summer is hot and humid, and Winter is cold and dry with abundant snowfall. Temperatures differ widely from region to region within Korea, with the average being between 6 °C (43°F) and 16 °C (61°F).

CURRENCY & BANK

1) Currency

Korea’s currency is the won. There are 1,000, 5,000, 10,000, and 50,000 won bills. Coins come in 10, 50, 100, and 500 won. (10 and 50 won coins are not widely in circulation)

2) Bank

Banks can offer some of the best exchange rates to travelers. Banking hours can vary, but most business hours are from 09:00 to 16:00. ATMs typically operate until 23:00, but many are open 24 hours. ATMs can also be found at convenient stores, but generally charge a higher transaction fee. ATMs that accept international cards are common, especially in areas frequented by foreigners; look for ATMs with a “Global” sign or the logo of your bank. Global ATMs offer multi-languages.

Element Jan. Feb. Mar. Apr. May Jun. Jul. Aug. Sep. Oct. Nov. Dec.

Minimum temperature(℃)

-6.1 -4.1 1.1 7.3 12.6 17.8 21.8 22.1 16.7 9.8 2.9 -3.4

Maximum temperature(℃)

1.6 4.1 10.2 17.6 22.8 26.9 28.8 29.5 25.6 19.7 11.5 4.2

Rainfall(mm) 21.6 23.6 45.8 77.0 102.2 133.3 327.9 348.0 137.6 49.3 53.0 24.9

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ELECTRICTY & VOLTAGE

The electricity supply commonly used in Korea is the 200-volt 60Hz system. Because most newly built hotels and houses have the 220-volt wiring installed, you are advised to check your electronic equipment beforehand.

<Korean Electrical Sockets and Plug>

BUSINESS HOURS

Government office hours are usually from 9:00 to 18:00 on weekdays. Banks are open from 9:00 to 16:00 on weekdays. Most stores are open every day from 10:30 to 20:00, including Sundays.

TAX

Value-added tax (VAT) is levied on most goods and services at a standard rate of 10% and is included in the retail price. In tourist hotels, this 10% tax applies to meals and other services and is added into the bill.

TIPPING

Tipping is not a traditional custom in Korea. A 10% service charge will be added to your bill at all tourist restaurants and hotels. It is also not necessary to tip a taxi driver unless he assists you with luggage or provides an extra service.

CREDIT CARDS

American Express, Master Card, Discover, and Visa are accepted in most hotels, restaurants, and shops.

Documents

List of Contents - ICAS 2016 · 1 List of Contents Welcome from ICAS and KSAS Presidents 2 ICAS Organization and Committees 4 ICAS 2016 Local Organizing Committee 6 ICAS Member Societies