21
Monday, June 13 Monday, June 13 Monday, June 13 Opening Plenary Session (Part 1 of 2) Opening Plenary Session (Part 2 of 2) Rotorcraft Icing (Part 1of 2) Session Code: Session Code: Session Code: ICE11 ICE11 ICE5 Room Empire Ballroom Room Empire Ballroom Room Salon 2 This session covers testing of rotorcraft subsystems as well as modeling and analysis in support of rotorcraft in-flight icing. This session also describes Computational Fluid Dynamics (CFD) codes that have been applied to rotary wing aircraft problems. The numerical simulation of icing on a helicopter fuselage as well as the ice accretion on a hovering rotor and ice accretion in unsteady conditions are the subject of the CFD. ICE6 also includes presentations related directly to rotorcraft. Richard Moser, Aerotex UK; Mark G. Potapczuk, NASA Glenn Research Center Richard Moser, Aerotex UK; Mark G. Potapczuk, NASA Glenn Research Center Moderators - Moderators - 9:15 a.m. 9:45 a.m. 10:15 a.m. 11:15 a.m. 11:45 a.m. 12:15 p.m. ORAL ONLY ORAL ONLY ORAL ONLY ORAL ONLY ORAL ONLY ORAL ONLY Icing: Accident Driven Actions and Inactions NASA's Research in Aviation Safety Icing Conditions: From Research to Operation - Observation and Predictability The Current State and Future Goals of Icing Analysis Tools and Their Impact on Aerodynamic Design Aircraft Development and Certification for Safe and Efficient Operation in Icing Conditions Managing Winter Challenges at Worlds Busiest Winter Airports Earl Weener, National Transportation Safety Board Douglas A. Rohn, NASA John Glenn Research Center Jean-Louis Brenguier, Meteo-France Bernard P. Paul, Cris Bosetti, Boeing Co. Richard Lewis, Airbus SAS Jack Lampe, United Air Lines Time Time Paper No. Paper No. Title Title SAE 2011 International Conference on Aircraft and Engine Icing and Ground Deicing Technical Session Schedule As of 06/19/2011 07:40 pm 9:15 a.m. 11:15 a.m. 2:30 p.m. Session Time: Session Time: Session Time:

SAE 2011 International Conference on Aircraft and Engine ... · helicopter fuselage as well as the ice accretion on a hovering rotor and ice accretion in unsteady ... Lakshmi N. Sankar,

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Page 1: SAE 2011 International Conference on Aircraft and Engine ... · helicopter fuselage as well as the ice accretion on a hovering rotor and ice accretion in unsteady ... Lakshmi N. Sankar,

Monday, June 13

Monday, June 13

Monday, June 13

Opening Plenary Session (Part 1 of 2)

Opening Plenary Session (Part 2 of 2)

Rotorcraft Icing (Part 1of 2)

Session Code:

Session Code:

Session Code:

ICE11

ICE11

ICE5

Room Empire Ballroom

Room Empire Ballroom

Room Salon 2

This session covers testing of rotorcraft subsystems as well as modeling and analysis in support of rotorcraft in-flight icing. This session alsodescribes Computational Fluid Dynamics (CFD) codes that have been applied to rotary wing aircraft problems. The numerical simulation of icing on ahelicopter fuselage as well as the ice accretion on a hovering rotor and ice accretion in unsteady conditions are the subject of the CFD. ICE6 alsoincludes presentations related directly to rotorcraft.

Richard Moser, Aerotex UK; Mark G. Potapczuk, NASA Glenn Research Center

Richard Moser, Aerotex UK; Mark G. Potapczuk, NASA Glenn Research Center

Moderators -

Moderators -

9:15 a.m.

9:45 a.m.

10:15 a.m.

11:15 a.m.

11:45 a.m.

12:15 p.m.

ORAL ONLY

ORAL ONLY

ORAL ONLY

ORAL ONLY

ORAL ONLY

ORAL ONLY

Icing: Accident Driven Actions and Inactions

NASA's Research in Aviation Safety

Icing Conditions: From Research to Operation - Observation andPredictability

The Current State and Future Goals of Icing Analysis Tools and TheirImpact on Aerodynamic Design

Aircraft Development and Certification for Safe and Efficient Operationin Icing Conditions

Managing Winter Challenges at Worlds Busiest Winter Airports

Earl Weener, National Transportation Safety Board

Douglas A. Rohn, NASA John Glenn Research Center

Jean-Louis Brenguier, Meteo-France

Bernard P. Paul, Cris Bosetti, Boeing Co.

Richard Lewis, Airbus SAS

Jack Lampe, United Air Lines

Time

Time

Paper No.

Paper No.

Title

Title

SAE 2011 International Conference onAircraft and Engine Icing and Ground

DeicingTechnical Session Schedule

As of 06/19/2011 07:40 pm

9:15 a.m.

11:15 a.m.

2:30 p.m.

Session Time:

Session Time:

Session Time:

Page 2: SAE 2011 International Conference on Aircraft and Engine ... · helicopter fuselage as well as the ice accretion on a hovering rotor and ice accretion in unsteady ... Lakshmi N. Sankar,

Monday, June 13

Monday, June 13

Rotorcraft Icing (Part 2 of 2)

Ice Phobic Materials (Part 1of 2)

Session Code:

Session Code:

ICE5

ICE9

Room Salon 2

Room Salon 3

This session covers testing of rotorcraft subsystems as well as modeling and analysis in support of rotorcraft in-flight icing. This session alsodescribes Computational Fluid Dynamics (CFD) codes that have been applied to rotary wing aircraft problems. The numerical simulation of icing on ahelicopter fuselage as well as the ice accretion on a hovering rotor and ice accretion in unsteady conditions are the subject of the CFD. ICE6 alsoincludes presentations related directly to rotorcraft.

This session presents both inflight and ground ice phobic ice protection research material. Included is information associated with concepts andmaterials that can prevent ice accretion or reduce the adhesion of ice.

Robert J. Flemming, Sikorsky Aircraft Corp.; Robert Leschi, Eurocopter; Richard Lewis, Airbus SAS

Philip J. Alldridge, Robert J. Flemming, Sikorsky Aircraft Corp.; Richard Lewis, Airbus SAS

Robert J. Flemming, Sikorsky Aircraft Corp.; Richard Lewis, Airbus SAS; Richard Moser, AerotexUK

Organizers -

Organizers -

Organizers -

Robert Leschi, Eurocopter

Philip J. Alldridge, Sikorsky Aircraft Corp.

Richard Moser, Aerotex UK

Chairpersons -

Chairpersons -

Chairpersons -

2:30 p.m.

3:00 p.m.

3:30 p.m.

4:30 p.m.

5:00 p.m.

2011-38-0006

2011-38-0014

2011-38-0008

2011-38-0015

2011-38-0016

Certification of the Sikorsky S-92A¿ Helicopter to the EASA LimitedIcing Special Condition

Extrapolation of Wind Tunnel Ice Shapes in the Evaluation of the Needfor Horizontal Tail Ice Protection on the BA609 Tiltrotor

The Certification of Externally-mounted Components on HelicoptersCertificated for Flight in Icing Conditions

Calculations of Ice Shapes on Oscillating Airfoils

Oscillating Airfoil Icing Tests in the NASA Glenn Research Center IcingResearch Tunnel

Robert J. Flemming, Sikorsky Aircraft Corp.; Philip Alldridge, SikorskyAircraft Corp

Jason Wright, Roger J. Aubert, Bell Helicopter Textron

Philip J. Alldridge, Robert J. Flemming, Sikorsky Aircraft Corp.

Robert Narducci, Tonja Reinert, The Boeing Company

Tonja Reinert, Boeing Co.; Robert J. Flemming, Sikorsky Aircraft Corp.;Robert Narducci, Boeing Co.; Roger J. Aubert, Bell Helicopter Textron

ORAL ONLY

Time

Time

Time

Paper No.

Paper No.

Paper No.

Title

Title

Title

4:30 p.m.

2:30 p.m.

Session Time:

Session Time:

Page 3: SAE 2011 International Conference on Aircraft and Engine ... · helicopter fuselage as well as the ice accretion on a hovering rotor and ice accretion in unsteady ... Lakshmi N. Sankar,

Monday, June 13

Monday, June 13

Ice Phobic Materials (Part 2 of 2)

CFD Icing Simulation Tools (Part 1of 6)

Session Code:

Session Code:

ICE9

ICE1

Room Salon 3

Room Salon 6

This session presents both inflight and ground ice phobic ice protection research material. Included is information associated with concepts andmaterials that can prevent ice accretion or reduce the adhesion of ice.

This session, comprised of six parts, provides information on developments in the use of CFD to simulate all facets of inflight icing, including droptrajectories, impingement, and accretion. Particular emphasis is on methods for physical modeling, for increased geometric complexity, for processintegration, and in the validation of the methodology.

Robert J. Flemming, Sikorsky Aircraft Corp.; Richard Lewis, Airbus SAS

Robert J. Flemming, Sikorsky Aircraft Corp.; Richard Lewis, Airbus SAS; Lakshmi N. Sankar,Georgia Institute of Technology

Organizers -

Organizers -

Richard Lewis, Airbus SAS

Lakshmi N. Sankar, Georgia Institute of Technology

Chairpersons -

Chairpersons -

2:30 p.m.

3:00 p.m.

3:30 p.m.

4:30 p.m.

5:00 p.m.

2:30 p.m.

2011-38-0001

2011-38-0002

2011-38-0003

2011-38-0009

2011-38-0010

2011-38-0106

In-Silico Environment for Designing Anti-icing Surfaces

Ice Phobic Coatings on Controlled and Covered Surfaces

Experimental Study of Hybrid Anti-Icing Systems CombiningThermoelectric and Hydrophobic Coatings

Surface Coating Effect on Protection of Icing for Axial Fan Blade

Hydrophobic Coating Study for Anti-icing Aircraft

Parallel Computing Applied to Three-Dimensional Droplet TrajectorySimulation in Lagrangian Approach

Jie Xiao, Katherine E. Mackie, Washington State Univ.; Joseph H. Osborne,Jill Seebergh, Boeing Research & Technology; Santanu Chaudhuri,Washington State Univ.

Brian Burkitt, Nathan Lipps, Nusil Technology

Guy Fortin, Maryelle Adomou, Jean Perron, Univ. du Quebec a Chicoutimi

Takeshi Murooka, Shinichirou Shishido, IHI Corp.; Riho Hiramoto, TakakazuMinoya, Hokkaido Institute of Technology

Katsuaki Morita, Koji Okamoto, Univ. of Tokyo; Akihito Aoki, Shigeo Kimura,Kanagawa Institute of Technology; Hirotaka Sakaue, Japan AerospaceExploration Agency

Ozgen Serkan, Middle East Technical University; Tarhan Erhan, CanibekMurat, Turkish Aerospace Industries Inc.

ORAL ONLY

Time

Time

Paper No.

Paper No.

Title

Title

4:30 p.m.

2:30 p.m.

Session Time:

Session Time:

Page 4: SAE 2011 International Conference on Aircraft and Engine ... · helicopter fuselage as well as the ice accretion on a hovering rotor and ice accretion in unsteady ... Lakshmi N. Sankar,

Monday, June 13

Tuesday, June 14

CFD Icing Simulation Tools (Part 2 of 6)

Appendix D: Ice Crystal Icing (Part 1of 4)

Session Code:

Session Code:

ICE1

ICE4

Room Salon 6

Room Salon 2

This session, comprised of six parts, provides information on developments in the use of CFD to simulate all facets of inflight icing, including droptrajectories, impingement, and accretion. Particular emphasis is on methods for physical modeling, for increased geometric complexity, for processintegration, and in the validation of the methodology.

This session deals with every aspect of flight in what is now known as Appendix D icing conditions, flight in clouds with ice crystal content. Thesession includes papers that present planning for future ice crystal research, the development of ice crystal test facilities, and wind tunnel and flighttests to gather ice crystal data and data on the effects of ice crystals. Since ice crystals generally affect only turbine engines, this session will have astrong emphasis on engine icing.

Robert J. Flemming, Sikorsky Aircraft Corp.; Daniel C. Knezevici, National Research CouncilCanada; Richard Lewis, Airbus SAS

Tom Currie, National Research Council Canada; Robert J. Flemming, Sikorsky Aircraft Corp.;Richard Lewis, Airbus SAS

Organizers -

Organizers -

Daniel C. Knezevici, National Research Council Canada

Tom Currie, National Research Council Canada

Chairpersons -

Chairpersons -

3:00 p.m.

3:30 p.m.

4:30 p.m.

5:00 p.m.

8:30 a.m.

9:00 a.m.

2011-38-0004

2011-38-0005

2011-38-0011

2011-38-0013

2011-38-0017

2011-38-0079

Improvements in Numerical Analysis of Droplet Impingement UsingLagrangian Approach

Lagrangian Parcel Volume Method for Unsteady Particle Concentration

Aircraft Icing and Anti-Icing Simulation Code CANICE3D: Panel Methodvs. CFD

Impingement of Supercooled Large Droplets via Reduced Order Models

An Overview of NASA Engine Ice-Crystal Icing Research

Development and Commissioning of a Linear Compressor Cascade Rigfor Ice Crystal Research

Peng Ke, Xinxin Wang, Beihang University

Jason Mickey, Eric Loth, Univ. of Virginia; Colin Bidwell, NASA

Jaideep Galhawat, Ion Paraschivoiu, Ecole Polytechnique Montreal; FarooqSaeed, King Fahd Univ. of Petroleum & Minerals

Marco Fossati, Wagdi G. Habashi, McGill University; Guido Baruzzi,Newmerical Technologies Inc.

Harold E. Addy, Jr., Joseph P. Veres, NASA Glenn Research Center

Daniel C. Knezevici, Dan Fuleki, James MacLeod, National ResearchCouncil Canada

ORAL ONLY

Time

Time

Paper No.

Paper No.

Title

Title

4:30 p.m.

8:30 a.m.

Session Time:

Session Time:

Page 5: SAE 2011 International Conference on Aircraft and Engine ... · helicopter fuselage as well as the ice accretion on a hovering rotor and ice accretion in unsteady ... Lakshmi N. Sankar,

Tuesday, June 14

Tuesday, June 14

Appendix D: Ice Crystal Icing (Part 2 of 4)

Appendix D: Ice Crystal Icing (Part 3 of 4)

Session Code:

Session Code:

ICE4

ICE4

Room Salon 2

Room Salon 2

This session deals with every aspect of flight in what is now known as Appendix D icing conditions, flight in clouds with ice crystal content. Thesession includes papers that present planning for future ice crystal research, the development of ice crystal test facilities, and wind tunnel and flighttests to gather ice crystal data and data on the effects of ice crystals. Since ice crystals generally affect only turbine engines, this session will have astrong emphasis on engine icing.

This session deals with every aspect of flight in what is now known as Appendix D icing conditions, flight in clouds with ice crystal content. Thesession includes papers that present planning for future ice crystal research, the development of ice crystal test facilities, and wind tunnel and flighttests to gather ice crystal data and data on the effects of ice crystals. Since ice crystals generally affect only turbine engines, this session will have astrong emphasis on engine icing.

Robert J. Flemming, Sikorsky Aircraft Corp.; Richard Lewis, Airbus SAS; Jen-Ching Tsao, OhioAerospace Institute

Philip Chow; Robert J. Flemming, Sikorsky Aircraft Corp.; Richard Lewis, Airbus SAS

Organizers -

Organizers -

Jen-Ching Tsao, Ohio Aerospace Institute

Philip Chow

Chairpersons -

Chairpersons -

9:30 a.m.

10:30 a.m.

11:00 a.m.

11:30 a.m.

2011-38-0018

2011-38-0025

2011-38-0026

2011-38-0027

Fundamental Ice Crystal Accretion Physics Studies

Engine Icing Modeling and Simulation (Part I): Ice Crystal Accretion onCompression System Components and Modeling its Effects on EnginePerformance

Engine Icing Modeling and Simulation (Part 2): Performance Simulationof Engine Rollback Phenomena

Atmosphere Sampling: Airbus A340 Flight Tests in Glaciated IcingConditions

Peter Struk, NASA John Glenn Research Center; Tom Currie, NationalResearch Council Canada; William Benjamin Wright, ASRC Aerospace;Daniel C. Knezevici, Dan Fuleki, National Research Council Canada; AndyBroeren, Mario Vargas, NASA; Jen-Ching Tsao, Ohio Aerospace Institute

Philip C. E. Jorgenson, NASA; Jospeh P. Veres, NASA John GlennResearch Center; William B. Wright, Ryan D. May, ASRC Aerospace

Ryan D. May, ASRC Aerospace; Ten-Huei Guo, Joseph P. Veres, Philip C.E. Jorgenson, NASA John Glenn Research Center

Alice Grandin, Airbus Operations S.A.S.ORAL ONLY

Time

Time

Paper No.

Paper No.

Title

Title

10:30 a.m.

1:30 p.m.

Session Time:

Session Time:

Page 6: SAE 2011 International Conference on Aircraft and Engine ... · helicopter fuselage as well as the ice accretion on a hovering rotor and ice accretion in unsteady ... Lakshmi N. Sankar,

Tuesday, June 14

Tuesday, June 14

Appendix D: Ice Crystal Icing (Part 4 of 4)

Meteorological Studies of Icing Conditions (Part 1 of 2)

Session Code:

Session Code:

ICE4

ICE17

Room Salon 2

Room Salon 3

Due to aircraft power budget limitations, there is a constant effort to minimize the energy requirements of ice protection systems. Numerical tools canbe used to optimize such systems but there is very little data available to validate the tools. This session will present details of ice protection systemsand their validation.

This session will focus on observational studies of in-flight icing events, the characterization of icing environments and ways to communicate that information to users.

Robert J. Flemming, Sikorsky Aircraft Corp.; Richard Lewis, Airbus SAS; Jeanne G. Mason, BoeingCommercial Airplanes

Ben C. Bernstein, Leading Edge Atmospherics; George A. Isaac, Environment Canada; ChristineLeBot, Meteo-France

Organizers -

Organizers -

Jeanne G. Mason, Boeing Commercial Airplanes

George A. Isaac, Environment Canada

Chairpersons -

Chairpersons -

1:30 p.m.

2:00 p.m.

2:30 p.m.

3:30 p.m.

4:00 p.m.

4:30 p.m.

2011-38-0036

2011-38-0037

2011-38-0038

2011-38-0048

2011-38-0049

2011-38-0050

Naturally Aspirating Isokinetic Total Water Content Probe: Wind TunnelTest Results and Design Modifications

Modifications at the Glenn Research Center's Propulsion SystemsLaboratory to Evaluate High Altitude Engine Icing Phenomena

Altitude Icing Testing of Jet Engines to begin at NASA Glenn ResearchCenter Propulsion Systems Laboratory

Particle Trajectory and Icing Analysis of the E<sup>3</sup> TurbofanEngine Using LEWICE3D Version 3

Critical Point Evaluation of Ice Crystals in Turbofan Engines

An Analysis of Turbofan Inlet Water and Ice Concentration Effects inIcing Conditions

Craig Davison, National Research Council Canada; Thomas Ratvasky,NASA John Glenn Research Center; Lyle Lilie, Science EngineeringAssociates

George Sydnor, NASA Langley Research Center; Jeffrey A. Chambers,NASA John Glenn Research Center

Thomas Hoffman, Paul Lizanich, Thomas Griffin, NASA John GlennResearch Center

Colin Bidwell, NASA

Robert S. Mazzawy, Trebor Systems Inc.

Shengfang Liao, Xuejun Liu, Matthew Feulner, United Technologies Prattand Whitney

ORAL ONLY

ORAL ONLY

Time

Time

Paper No.

Paper No.

Title

Title

3:30 p.m.

8:30 a.m.

Session Time:

Session Time:

Page 7: SAE 2011 International Conference on Aircraft and Engine ... · helicopter fuselage as well as the ice accretion on a hovering rotor and ice accretion in unsteady ... Lakshmi N. Sankar,

Tuesday, June 14

Tuesday, June 14

Remote Sensing of Atmospheric Icing Conditions (Part 1 of 2)

Remote Sensing of Atmospheric Icing Conditions (Part 2 of 2)

Session Code:

Session Code:

ICE18

ICE18

Room Salon 3

Room Salon 3

This session will focus on methods used to diagnose the presence of icing conditions using remote sensing using ground-based systems.

This session will focus on methods used to diagnose the presence of icing conditions using remote sensing using satellite-based and in-flightsystems.

Ben C. Bernstein, Leading Edge Atmospherics; Christine LeBot, Meteo-France; Cory Wolff,National Center for Atmospheric Research

Ben C. Bernstein, Leading Edge Atmospherics; Julie Haggerty, NCAR; Christine LeBot, Meteo-France

Organizers -

Organizers -

Cory Wolff, National Center for Atmospheric Research

Julie Haggerty, NCAR

Chairpersons -

Chairpersons -

8:30 a.m.

9:00 a.m.

9:30 a.m.

10:30 a.m.

11:00 a.m.

11:30 a.m.

2011-38-0019

2011-38-0020

2011-38-0021

2011-38-0028

2011-38-0029

2011-38-0030

Initial Steps Toward Inclusion of Icing-Relevant AtmosphericParameters in a Weather Forecast

An Examination of Aircraft Icing Conditions Associated with Cold Fronts

A Regional Comparison of Icing Conditions in Boundary Layer Clouds

A Freezing Fog/Drizzle Event during the FRAM-S Project

Decision Making Regarding Aircraft De-Icing and In-Flight Icing Usingthe Canadian Airport Nowcasting System (CAN-Now)

In-flight Icing Hazard Verification with NASA's Icing Remote SensingSystem for Development of a NEXRAD Icing Hazard Level Algorithm

Marcia K. Politovich, Daniel R. Adriaansen, Gregory Thompson, NationalCenter for Atmospheric Research

Cory Wolff, Frank Mcdonough, National Center for Atmospheric Research;Ben Bernstein, Leading Edge Atmospherics

Ben C. Bernstein, Leading Edge Atmospherics; Frank Mcdonough, CoryWolff, National Center for Atmospheric Research

Ismail Gultepe, Meteorological Service of Canada; George A. Isaac,Environment Canada; Roy Martin Rasmussen, National Center forAtmospheric Research; K. Ungar, Health Canada

George A. Isaac, Monika Bailey, Faisal Boudala, Stewart G. Cober, RobertCrawford, Norman Donaldson, Ismail Gultepe, Bjarne Hansen, IvanHeckman, Laura Huang, Alister Ling, Janti Reid, ARMP, EnvironmentCanada; Marc Fournier, CMAC-E, Environment Canada

David Serke, NCAR/RAL; John Hubbert, NCAR/EOL; Andrew Reehorst,NASA Glenn Research Center; Marcia Politovich, NCAR/RAL; PatrickKennedy, Colorado State University; Mike Dixon, Scott Ellis, NCAR/EOL;Chris Johnston, David Albo, Scott Landolt, NCAR/RAL

ORAL ONLY

Time Paper No. Title

10:30 a.m.

1:30 p.m.

Session Time:

Session Time:

Page 8: SAE 2011 International Conference on Aircraft and Engine ... · helicopter fuselage as well as the ice accretion on a hovering rotor and ice accretion in unsteady ... Lakshmi N. Sankar,

Tuesday, June 14

Tuesday, June 14

Meteorological Studies of Icing Conditions (Part 2 of 2)

CFD Icing Simulation Tools (Part 3 of 6)

Session Code:

Session Code:

ICE17

ICE1

Room Salon 3

Room Salon 6

This session will focus on observational studies of in-flight icing events, the characterization of icing environments and ways to communicate thatinformation to users. Mixed-phase icing environments are highlighted here.

This session, comprised of six parts, provides information on developments in the use of CFD to simulate all facets of inflight icing, including droptrajectories, impingement, and accretion. Particular emphasis is on methods for physical modeling, for increased geometric complexity, for processintegration, and in the validation of the methodology.

Ben C. Bernstein, Leading Edge Atmospherics; Christine LeBot, Meteo-France; Jakob Tendel,Leibniz University Hannover

Robert J. Flemming, Sikorsky Aircraft Corp.; Richard Lewis, Airbus SAS; William B. Wright, ASRCAerospace

Organizers -

Organizers -

Jakob Tendel, Leibniz University Hannover

William B. Wright, ASRC Aerospace

Chairpersons -

Chairpersons -

1:30 p.m.

2:00 p.m.

2:30 p.m.

3:30 p.m.

4:00 p.m.

4:30 p.m.

2011-38-0039

2011-38-0040

2011-38-0041

2011-38-0051

2011-38-0052

2011-38-0053

Characterization of Aircraft Icing Environment using Airborne Radarsand Radiometer

New Methods to Infer Aircraft Icing Conditions using Satellite Data

Nowcasting Aircraft Icing Conditions in the Presence of MultilayeredClouds Using Meteorological Satellite Data

Using the TAMDAR Sensor for In-flight Ice Detection and ImprovedSafety of Flight

The Large and Small-Scale Structure and Evolution of a Mixed-PhaseIcing Cloud

Aircraft Icing Under an Evolving Mixed Phase Environment

Mengistu Wolde, Institute for Aerospace Studies

William Smith, Patrick Minnis, NASA Langley Research Center; CeciliaFleeger, Douglas Spangenberg, Science Systems & Applications Inc.; DavidSerke, NCAR; Andrew Reehorst, NASA John Glenn Research Center

Douglas Spangenberg, Science Systems & Applications Inc.; Patrick Minnis,William Smith, NASA Langley Research Center; Fu-Lung Chang, ScienceSystems & Applications Inc

Jamie Braid, Patrick Van Wie, Jeffrey Rex, AirDat LLC

Frank Mcdonough, Cory Wolff, National Center for Atmospheric Research

John Hallett, Desert Research Institute

ORAL ONLY

ORAL ONLY

ORAL ONLY

Time

Time

Time

Paper No.

Paper No.

Paper No.

Title

Title

Title

3:30 p.m.

8:30 a.m.

Session Time:

Session Time:

Page 9: SAE 2011 International Conference on Aircraft and Engine ... · helicopter fuselage as well as the ice accretion on a hovering rotor and ice accretion in unsteady ... Lakshmi N. Sankar,

Tuesday, June 14

Tuesday, June 14

CFD Icing Simulation Tools (Part 4 of 6)

CFD Icing Simulation Tools (Part 5 of 6)

Session Code:

Session Code:

ICE1

ICE1

Room Salon 6

Room Salon 6

This session, comprised of six parts, provides information on developments in the use of CFD to simulate all facets of inflight icing, including droptrajectories, impingement, and accretion. Particular emphasis is on methods for physical modeling, for increased geometric complexity, for processintegration, and in the validation of the methodology.

This session, comprised of six parts, provides information on developments in the use of CFD to simulate all facets of inflight icing, including droptrajectories, impingement, and accretion. Particular emphasis is on methods for physical modeling, for increased geometric complexity, for processintegration, and in the validation of the methodology.

Robert J. Flemming, Sikorsky Aircraft Corp.; Richard Lewis, Airbus SAS; Robert Narducci, TheBoeing Company

Robert J. Flemming, Sikorsky Aircraft Corp.; Wagdi G. Habashi, McGill Univ.; Richard Lewis, AirbusSAS

Organizers -

Organizers -

Robert Narducci, Boeing Helicopters

Wagdi G. Habashi, McGill Univ.

Chairpersons -

Chairpersons -

8:30 a.m.

9:00 a.m.

9:30 a.m.

10:30 a.m.

11:00 a.m.

11:30 a.m.

2011-38-0022

2011-38-0023

2011-38-0024

2011-38-0031

2011-38-0032

2011-38-0033

Robust Moving Meshes for the Prediction of Aerodynamic Degradationduring In-Flight Icing

Proposed Wall Function Models for Heat Transfer around a Cylinder withRough Surface in Cross Flow

FENSAP-ICE: Numerical Prediction of Ice Roughness Evolution, and itsEffects on Ice Shapes

CFD-Icing: A Predictive Tool for In-Flight Icing Risk Management

Efficient Prediction of Ice Shapes in CFD Simulation of In-flight IcingUsing a POD-Based Reduced Order Model

FENSAP-ICE in Aid of Certification: From CFD to Flight Testing

Marco Fossati, Rooh-ul-Amin Khurram, Wagdi G. Habashi, McGill Univ.

Guilherme Araujo Lima da Silva, Marcos Noboru Arima, Aero-ThermalSolutions for Industry; Natashe Nicoli Branco, Marcos de Mattos Pimenta,University of São Paulo

Isik A. Ozcer, Guido S. Baruzzi, Thomas Reid, Newmerical TechnologiesInc.; Wagdi G. Habashi, Marco Fossati, McGill Univ.; Giulio Croce,Universita degli Studi di Udine

Danial Zeppetelli, Wagdi G. Habashi, McGill Univ.

Sung Ki Jung, Gyeongsang National Univ.; Rho Shin Myong, Tae HwanCho, GNU, Dept. of Aero. Sys. Eng. and ReCAPT

John P. Dow, Sr., DOW International, L.L.C.; Cristhian N. Aliaga, ShoaibShah, Jian Chen, Newmerical Technologies Inc.; Wagdi G. Habashi, McGillUniv.; John L. Siemens, JLS Eningeering Consultants Inc.

Time Paper No. Title

10:30 a.m.

1:30 p.m.

Session Time:

Session Time:

Page 10: SAE 2011 International Conference on Aircraft and Engine ... · helicopter fuselage as well as the ice accretion on a hovering rotor and ice accretion in unsteady ... Lakshmi N. Sankar,

Tuesday, June 14

Wednesday, June 15

CFD Icing Simulation Tools (Part 6 of 6)

The Effects of Icing (Part 1of 2)

Session Code:

Session Code:

ICE1

ICE2

Room Salon 6

Room Salon 2

This session, comprised of six parts, provides information on developments in the use of CFD to simulate all facets of inflight icing, including droptrajectories, impingement, and accretion. Particular emphasis is on methods for physical modeling, for increased geometric complexity, for processintegration, and in the validation of the methodology.

This session includes material on the effects of icing and ice accretion on the performance and flying characteristics of aircraft and on methods anddata used to support certification to 14 CFR 25 Part B (or the equivalent for other aircraft types and regulatory standards).

Michael B. Bragg, Univ. of Illinois at Urbana-Champaign; Robert J. Flemming, Sikorsky AircraftCorp.; Richard Lewis, Airbus SAS

Robert J. Flemming, Sikorsky Aircraft Corp.; Richard Lewis, Airbus SAS

Organizers -

Organizers -

Michael B. Bragg, Univ. of Illinois at Urbana-Champaign

Robert J. Flemming, Sikorsky Aircraft Corp.

Chairpersons -

Chairpersons -

1:30 p.m.

2:00 p.m.

2:30 p.m.

3:30 p.m.

4:00 p.m.

4:30 p.m.

2011-38-0054

2011-38-0043

2011-38-0044

2011-38-0055

2011-38-0056

ORAL ONLY

Improving Ice Accretion Simulation Through the use of CFD

Simulation of Ice Accretion on Three Dimensional Wing

A CFD Approach for Predicting 3D Ice Accretion on Aircraft

Analysis for the Design and Test of an Ice Protection System for aScoop Intake

Development of An Icing Tool For Aircraft Engines

Propulsion Icing Wind Tunnel Research Simulating Ice Pellet Conditions

Daniel Martins Silva, Instituto Tecnológico de Aeronaútica-ITA; LuisGustavo Trapp, Embraer Aircraft Corp.

Chao Wang, Shi-nan Chang, Beijing Univ. Aeronautics & Astronautics; Xin-ming Su, China Academy of Space Technology

Michael P. Kinzel, Ralph W. Noack, Christian M. Sarofeen, David Boger,Penn State Univ.-Applied Research Lab.; Richard Eric Kreeger, NASA JohnGlenn Research Center

Richard Moser, Roger Gent, Aerotex UK

Chiong S. Tan, GE Global Research Center; Byron Pritchard, Ron Plybon,Chuck Califf, Ray Holm, Sasikumar Muthusamy, Viilas Bokade, TS Niranjan,Balasubramaniam Mahadevan, General Electric Co

Marco Ruggi, APS Aviation Inc.

Time

Time

Time

Paper No.

Paper No.

Paper No.

Title

Title

Title

3:30 p.m.

8:30 a.m.

Session Time:

Session Time:

Page 11: SAE 2011 International Conference on Aircraft and Engine ... · helicopter fuselage as well as the ice accretion on a hovering rotor and ice accretion in unsteady ... Lakshmi N. Sankar,

Wednesday, June 15

Wednesday, June 15

The Effects of Icing (Part 2 of 2)

Ice Shedding and Ice Scaling (Part 1of 2)

Session Code:

Session Code:

ICE2

ICE6

Room Salon 2

Room Salon 2

This session includes material on the effects of icing and ice accretion on the performance and flying characteristics of aircraft and on methods anddata used to support certification to 14 CFR 25 Part B (or the equivalent for other aircraft types and regulatory standards).

This session includes papers dedicated to the shedding of ice from aircraft components as well as scaling relationships to allow the application tomodel-scale data to full-scale problems.

Robert J. Flemming, Sikorsky Aircraft Corp.; Richard Lewis, Airbus SAS; Tonja Reinert, Boeing Co.

Roger J. Aubert, Bell Helicopter Textron; Robert J. Flemming, Sikorsky Aircraft Corp.; RichardLewis, Airbus SAS

Organizers -

Organizers -

Tonja Reinert, Boeing Co.

Roger J. Aubert, Bell Helicopter Textron

Chairpersons -

Chairpersons -

8:30 a.m.

9:00 a.m.

9:30 a.m.

10:30 a.m.

11:00 a.m.

1:30 p.m.

2:00 p.m.

2011-38-0065

2011-38-0066

2011-38-0067

2011-38-0073

2011-38-0074

2011-38-0081

2011-38-0082

Aerodynamic Effects of Simulated Ice Accretion on a Generic TransportModel

Envelope Protection System for Iced Airfoils Using Flap Hinge Moment

Low Speed Aerodynamic Study of Full-Scale Figh-Fidelity Runback IceShapes

Aircraft Performance Degradation - the Effects of Inflight Icing upon Lift,Drag and Propulsive Efficiency

Flow Field Predictions of the NASA Glenn Icing Research Tunnel

Evaluation of Icing Scaling on Swept NACA 0012 Airfoil Models

Icing Scaling Laws Implemented in a Rotor Performance DegradationModel

Andy P. Broeren, NASA Glenn Research Center; Sam Lee, ASRCAerospace Corporation; Gautam H. Shah, Patrick C. Murphy, NASA LangleyResearch Center

Phillip J. Ansell, Michael B. Bragg, Univ. of Illinois at Urbana-Champaign;Michael F. Kerho, Rolling Hills Research Corp.

Nathalie Alegre, David Hammond, Cranfield Univ.

Anthony P. Brown, National Research Council Canada

Kevin M. Clark, Yong Han Yeong, Eric Loth, Univ. of Virginia; Judith FossVan Zante, David Sheldon, Robert Ide, NASA John Glenn Research Center

Jen-Ching Tsao, Ohio Aerospace Institute; Sam Lee, ASRC AerospaceCorp.

Stephane Catris, Eurocopter

Time

Time

Paper No.

Paper No.

Title

Title

ALL DAY

1:30 p.m.

Session Time:

Session Time:

Page 12: SAE 2011 International Conference on Aircraft and Engine ... · helicopter fuselage as well as the ice accretion on a hovering rotor and ice accretion in unsteady ... Lakshmi N. Sankar,

Wednesday, June 15

Wednesday, June 15

Wednesday, June 15

Ice Shedding and Ice Scaling (Part 2 of 2)

Applications of Weather Models for In-Flight Icing Diagnosis and Forecasting

Real-time Icing Products

Session Code:

Session Code:

Session Code:

ICE6

ICE23

ICE22

Room Salon 2

Room Salon 3

This session includes papers dedicated to the shedding of ice from aircraft components as well as scaling relationships to allow the application tomodel-scale data to full-scale problems.

This session will focus on the advancement of cloud microphysics schemes used to explicitly predict supercooled liquid water content and drop size,as well as their application in real-time icing systems.

Robert J. Flemming, Sikorsky Aircraft Corp.; Roger Gent, Aerotex UK; Richard Lewis, Airbus SAS

Ben C. Bernstein, Leading Edge Atmospherics; Gordon Brooks, Air Force Weather Agency;Christine LeBot, Meteo-France

Organizers -

Organizers -

Roger Gent, Aer

Gordon Brooks, Air Force Weather Agency

Chairpersons -

Chairpersons -

2:30 p.m.

3:30 p.m.

4:00 p.m.

8:30 a.m.

9:00 a.m.

2011-38-0083

2011-38-0089

2011-38-0090

2011-38-0060

2011-38-0062

Further Evaluation of Scaling Methods for Rotorcraft Icing

FENSAP-ICE: A CFD Monte Carlo Approach to Shed-Ice Trajectory andImpact

A Methodology for the Prediction of Rotor Blade Ice Formation andShedding

Applications of an Advanced Cloud and Precipitation Physics Packagein a Weather Forecast Model

Microphysics from High Resolution NWP Model in the IcingIdentification Tool Sigma

Jen-Ching Tsao, Ohio Aerospace Institute; Richard Kreeger, NASA JohnGlenn Research Center

Jean-Mathieu Deschenes, McGill Univ.; Guido S. Baruzzi, Patrick Lagace,Newmerical Technologies Inc.; Wagdi G. Habashi, McGill Univ.

Jeremy Bain, Lakshmi N. Sankar, Georgia Institute of Technology; Roger J.Aubert, Bell Helicopter Textron; Robert J. Flemming, Sikorsky Aircraft Corp.

Gregory Thompson, Changhai Liu, Marcia Politovich, National Center forAtmospheric Research

Christine LeBot, Meteo-France

ORAL ONLY

ORAL ONLY

Time

Time

Paper No.

Paper No.

Title

Title

3:30 p.m.

8:30 a.m.

Session Time:

Session Time:

Page 13: SAE 2011 International Conference on Aircraft and Engine ... · helicopter fuselage as well as the ice accretion on a hovering rotor and ice accretion in unsteady ... Lakshmi N. Sankar,

Wednesday, June 15

Wednesday, June 15

High Ice-water Content and Jet Engine Icing

Aircraft Anti-icing and Deicing Operations (Part 1of 4)

Session Code:

Session Code:

ICE21

ICE10

Room Salon 3

Room Salon 3

Room Salon 3

This session will focus on real-time icing products that merge information from a variety of sources, with emphasis on their performance, strengthsand weaknesses and their adaptation to new environments.

This session will focus on the phenomenon of jet engine icing associated with the presence of large concentrations of ice crystals. Examinations ofrecent events, planned field program work and new techniques to detect these events will be discussed.

Ben C. Bernstein, Leading Edge Atmospherics; Christine LeBot, Meteo-France

Ben C. Bernstein, Leading Edge Atmospherics; Jonathan Gould, Pratt & Whitney; Christine LeBot,Meteo-France

Organizers -

Organizers -

Ben C. Bernstein, Leading Edge Atmospherics; Christine LeBot, Meteo-France

Jonathan Gould, Pratt & Whitney

Chairpersons -

Chairpersons -

10:30 a.m.

11:00 a.m.

11:30 a.m.

1:30 p.m.

2:00 p.m.

2:30 p.m.

2011-38-0068

2011-38-0069

2011-38-0070

ORAL ONLY

2011-38-0094

2011-38-0095

Verification of ADWICE In-Flight Icing Forecasts: Performance vsPIREPS Compared to FIP

Exercising CIP Severity: An Investigation of Methodologies within theCIP Severity Algorithm

LOWICE: An Example of the Adaption of In-flight Icing DiagnosisConcepts to the Structural Icing Environment

High Ice Water Content Cloud Characterization Flight Campaign Update

The Challenges Identifying Weather Associated With Jet Engine IceCrystal Icing

Preliminary Algorithm for High Ice Water Content Detection

Jakob Tendel, Leibniz Universität Hannover; Cory Wolff, National Center forAtmospheric Research

Daniel R. Adriaansen, Cory Wolff, Frank Mcdonough, National Center forAtmospheric Research

Ben C. Bernstein, Leading Edge Atmospherics; Erik Gregow, FinnishMeteorological Institute; Ian Wittmeyer, Leading Edge Atmospherics; JarkkoHirvonen, Finnish Meteorological Institute

Thomas Ratvasky, NASA John Glenn Research Center; J. Walter Strapp,Environment Canada

Jeanne G. Mason, Matthew Grzych, Boeing Commercial Airplanes

Jennifer Black, Julie Haggerty, NCAR; Frank Mcdonough, Marcia K.Politovich, National Center for Atmospheric Research

ORAL ONLY

Time

Time

Paper No.

Paper No.

Title

Title

10:30 a.m.

1:30 p.m.

3:30 p.m.

Session Time:

Session Time:

Session Time:

Page 14: SAE 2011 International Conference on Aircraft and Engine ... · helicopter fuselage as well as the ice accretion on a hovering rotor and ice accretion in unsteady ... Lakshmi N. Sankar,

Wednesday, June 15

Wednesday, June 15

Appendix O: SLD Icing (Part 1 of 4)

Appendix O: SLD Icing (Part 2 of 4)

Session Code:

Session Code:

ICE3

ICE3

Room Salon 6

Room Salon 6

This session addresses a wide variety of research topics related to aircraft ground deicing operations including active frost detection systems, liquidwater equivalent based systems to determine and update anti-icing fluid holdover times. Aircraft flight testing and wind tunnel testing with anti-icingfluids, along with fluid failure modeling, runway deicing fluid development and environmental regulations will also be discussed.

This session presents the latest developments and applications for certification to 14 CFR 25 Appendix O supercooled large drop (SLD) icingconditions. Included are topics of droplet splashing, rebound and re-impingement, and the effect they have on the resultant ice shapes.

Oliver M. Arzt, N ICE Aircraft Services & Support GmbH; Warren M. Underwood, Federal AviationAdministration

Robert J. Flemming, Sikorsky Aircraft Corp.; Eugene G. Hill; Richard Lewis, Airbus SAS

Organizers -

Organizers -

Oliver M. Arzt, N ICE Aircraft Services & Support GmbH; Warren M. Underwood, Federal AviationAdministration

Eugene G. Hill

Chairpersons -

Chairpersons -

3:30 p.m.

4:00 p.m.

4:30 p.m.

8:30 a.m.

9:00 a.m.

9:30 a.m.

2011-38-0045

2011-38-0046

2011-38-0047

ORAL ONLY

2011-38-0063

2011-38-0064

Experimental Study of Snow Precipitation Over a Generic Deicing Fluidwithout Fluid Flow

Using Manual Snow Pan Measurements to Verify a Liquid EquivalentWater-based System for Ground De-icing Operations

A New Technique for Automated Frost Detection

Aerodynamics Degradations and Control Anomalies during a Departurefrom Controlled Flight of a Turboprop Airplane in an SLD Environment

EXTICE: EXTreme Icing Environement

Experimental Investigation of Thin Water Film Stability and ItsCharacteristics in SLD Icing Problem

Guy Fortin, Ilham Enneji, Arlene Beisswenger, Jean Perron, Univ. duQuebec a Chicoutimi

Jennifer Black, Scott Landolt, Roy Martin Rasmussen, National Center forAtmospheric Research

Scott Landolt, Roy Martin Rasmussen, Chris Johnston, National Center forAtmospheric Research

Daniel R. Bower, Ph.D., Dennis A. Crider, National Transportation SafetyBoard

Giuseppe Mingione, Emiliano Iuliano, CIRA; Didier Guffond, ONERA;Cameron Tropea, Technical Univ. of Darmstadt

Jafar Alzaili, David Hammond, Cranfield University

ORAL ONLY

ORAL ONLY

Time

Time

Paper No.

Paper No.

Title

Title

8:30 a.m.

10:30 a.m.

Session Time:

Session Time:

Page 15: SAE 2011 International Conference on Aircraft and Engine ... · helicopter fuselage as well as the ice accretion on a hovering rotor and ice accretion in unsteady ... Lakshmi N. Sankar,

Wednesday, June 15

Wednesday, June 15

Appendix O: SLD Icing (Part 3 of 4)

Appendix O: SLD Icing (Part 4 of 4)

Session Code:

Session Code:

ICE3

ICE3

Room Salon 6

Room Salon 6

This session presents the latest developments and applications for certification to 14 CFR 25 Appendix O supercooled large drop (SLD) icingconditions. Included are topics of droplet splashing, rebound and re-impingement, and the effect they have on the resultant ice shapes.

This session presents the latest developments and applications for certification to 14 CFR 25 Appendix O supercooled large drop (SLD) icingconditions. Included are topics of droplet splashing, rebound and re-impingement, and the effect they have on the resultant ice shapes.

This session presents the latest developments and applications for certification to 14 CFR 25 Appendix O supercooled large drop (SLD) icingconditions. Included are topics of droplet splashing, rebound and re-impingement, and the effect they have on the resultant ice shapes.

Robert J. Flemming, Sikorsky Aircraft Corp.; Dan Fuleki, National Research Council Canada;Richard Lewis, Airbus SAS

Robert J. Flemming, Sikorsky Aircraft Corp.; Jim R. Hoppins, Cessna Aircraft Co.; Richard Lewis,Airbus SAS

Biagio Esposito, CIRA; Robert J. Flemming, Sikorsky Aircraft Corp.; Richard Lewis, Airbus SAS

Organizers -

Organizers -

Organizers -

Dan Fuleki, National Research Council Canada

Jim R. Hoppins, Cessna Aircraft Co.

Biagio Esposito, CIRA

Chairpersons -

Chairpersons -

Chairpersons -

10:30 a.m.

11:00 a.m.

11:30 a.m.

1:30 p.m.

2:00 p.m.

2:30 p.m.

ORAL ONLY

2011-38-0071

2011-38-0072

ORAL ONLY

2011-38-0080

2011-38-0086

Practical Scaling of Available IWT Conditions to the Appendix O Spectra

Numerical Simulation of SLD Ice Accretions

Wind Tunnel Investigation on the Response Characteristics of ParticleSpectrometers to SLD Cloud Conditions

Determining the Suitability of IWT Test Facilities for DemonstratingCompliance with Certification Requirements in Appendix O Conditions

CFD Analysis of Supercooled Large Droplets in Turbofan Engines

New SLD Icing Capabilities at DGA Aero-engine Testing

David C. Parkins, American Kestrel Company

Jacco Hospers, H. W. M. Hoeijmakers, Univ. of Twente

Biagio Esposito, CIRA; J. Walter Strapp, Environment Canada; William D.Bachalo, Artium Technologies Inc.; Myron Oleskiw, National ResearchCouncil Canada

Kamel Al-Khalil, Joseph Vogel, Cox & Company Inc.; David C. Parkins,American Kestrel Company

Chuck Califf, Anabel Rodriguez, Eduardo Lemini, GE Aviation; Chiong Tan,GE Global Research Center

Franck Hervy, DGA Essais Propulseurs

ORAL ONLY

Time

Time

Paper No.

Paper No.

Title

Title

1:30 p.m.

3:30 p.m.

Session Time:

Session Time:

Page 16: SAE 2011 International Conference on Aircraft and Engine ... · helicopter fuselage as well as the ice accretion on a hovering rotor and ice accretion in unsteady ... Lakshmi N. Sankar,

Thursday, June 16

Thursday, June 16

Icing Certification Plenary Session

Ice Protection Systems (Part 1 of 3)

Session Code:

Session Code:

ICE12

ICE8

Room Empire Ballroom

Room Salon 2

Due to aircraft power budget limitations, there is a constant effort to minimize the energy requirements of ice protection systems. Numerical tools canbe used to optimize such systems but there is little data available to validate the tools. This session will present details of ice protection systems andtheir validation.

Stephane Catris, Eurocopter; Robert J. Flemming, Sikorsky Aircraft Corp.; Richard Lewis, AirbusSAS

Organizers -

Stephane Catris, EurocopterChairpersons -

Thomas H. Bond, Federal Aviation AdminstrationModerators -

3:30 p.m.

4:00 p.m.

3:30 p.m.

8:30 a.m.

9:00 a.m.

9:30 a.m.

2011-38-0087

2011-38-0088

ORAL ONLY

ORAL ONLY

2011-38-0035

2011-38-0034

Rotating Rig Development for Droplet Deformation/Breakup and ImpactInduced by Aerodynamic Surfaces

ONICE2D and DROP3D SLD Capability Assessment

Aircraft Turbine Engine Icing: Current Issues and Future Vision

Clean Sky European JTI, Systems for Green Operations - Electrical IceProtection Systems

The Building Blocks for a Hybrid ElectroThermal-ElectroMechanicalSimulation Tool

Experimental and Computer Model Results for a Bleed Air Ice ProtectionSystem

Alejandro Feo, Instituto Nacional de Técnica Aeroespacial (INTA); MarioVargas, NASA Glenn Research Center; Suthyvann Sor, Instituto Nacional deTécnica Aeroespacial (INTA)

Fabien Dezitter, Airbus

John Fisher, Federal Aviation Administration

Francois LaRue, Zodiac Aerospace

Colin Hatch, Richard Moser, Roger Gent, Aerotex UK; Peter Hicks,University College London UK

Michael Papadakis, Alonso O. Zamora Rodriguez, Rodrigo HoffmannDomingos, Wichita State Univ.

Time

Time

Time

Paper No.

Paper No.

Paper No.

Title

Title

Title

3:30 p.m.

8:30 a.m.

Session Time:

Session Time:

Page 17: SAE 2011 International Conference on Aircraft and Engine ... · helicopter fuselage as well as the ice accretion on a hovering rotor and ice accretion in unsteady ... Lakshmi N. Sankar,

Thursday, June 16

Thursday, June 16

Ice Protection Systems (Part 2 of 3)

Ice Protection Systems (Part 3 of 3)

Session Code:

Session Code:

ICE8

ICE8

Room Salon 2

Room Salon 2

Due to aircraft power budget limitations, there is a constant effort to minimize the energy requirements of ice protection systems. Numerical tools canbe used to optimize such systems but there is little data available to validate the tools. This session will present details of ice protection systems andtheir validation.

Due to aircraft power budget limitations, there is a constant effort to minimize the energy requirements of ice protection systems. Numerical tools canbe used to optimize such systems but there is little data available to validate the tools. This session will present details of ice protection systems andtheir validation.

Thomas H. Bond, Federal Aviation Adminstration; Robert J. Flemming, Sikorsky Aircraft Corp.;Richard Lewis, Airbus SAS

Gene Addy, NASA John Glenn Research Center; Robert J. Flemming, Sikorsky Aircraft Corp.;Richard Lewis, Airbus SAS

Organizers -

Organizers -

Thomas H. Bond, Federal Aviation Adminstration

Gene Addy, NASA John Glenn Research Center

Chairpersons -

Chairpersons -

10:30 a.m.

11:00 a.m.

11:30 a.m.

1:30 p.m.

2:00 p.m.

2:30 p.m.

2011-38-0096

2011-38-0097

2011-38-0098

2011-38-0102

2011-38-0103

2011-38-0104

Numerical Simulation of Electro-thermal Deicing Process and theEffects of Icing Conditions

Challenges in Predicting Rotor Blade Ice Protection Coverage Extentusing Alternate Flow Solver and Lewice3D

Rotating Testing of a Low-Power, Non-Thermal Ultrasonic De-icingSystem for Helicopter Rotor Blades

FENSAP-ICE: 3D Simulation, and Validation, of De-icing with Inter-cycle Ice Accretion

Optimized Hot-Air Ice Protection Systems via FENSAP-ICE

Flight Tests in Natural Icing of the PZL Mielec M28 Commuter TurbopropAirplane

Shinan Chang, Beijing Univ. Aeronautics & Astronautics

Roger J. Aubert, Jason Wright, Bell Helicopter Textron

Austin Overmeyer, Jose Luis Palacios, Edward C. Smith, Penn State Univ.;Roger Royer, FBS Inc.

Thomas Reid, Guido S. Baruzzi, Isik A. Ozcer, Newmerical TechnologiesInc.; Wagdi G. Habashi, McGill Univ.

Mathieu Pellissier, Wagdi G. Habashi, McGill Univ.; Alberto Pueyo,Bombardier Aerospace

Mariusz Kubryn, Polskie Zaklady Lotnicze Sp. z o.o.; Robert Flemming,Sikorsky Aircraft Corp.; Ben Bernstein, Leading Edge Atmospherics; JanuszPietruszka, Polskie Zak¿ady Lotnicze Sp. z o.o.

ORAL ONLY

Time

Time

Paper No.

Paper No.

Title

Title

10:30 a.m.

1:30 p.m.

Session Time:

Session Time:

Page 18: SAE 2011 International Conference on Aircraft and Engine ... · helicopter fuselage as well as the ice accretion on a hovering rotor and ice accretion in unsteady ... Lakshmi N. Sankar,

Thursday, June 16

Thursday, June 16

Aircraft Anti-icing and Deicing Operations (Part 2 of 4)

Aircraft Anti-icing and Deicing Operations (Part 3 of 4)

Session Code:

Session Code:

ICE10

ICE10

Room Salon 3

Room Salon 3

This session addresses a wide variety of research topics related to aircraft ground deicing operations including active frost detection systems, liquidwater equivalent based systems to determine and update anti-icing fluid holdover times. Aircraft flight testing and wind tunnel testing with anti-icingfluids, along with fluid modeling, runway deicing fluid development and environmental regulations will also be discussed.

This session addresses a wide variety of research topics related to aircraft ground deicing operations including active frost detection systems, liquidwater equivalent based systems to determine and update anti-icing fluid holdover times. Aircraft flight testing and wind tunnel testing with anti-icingfluids, along with fluid modeling, runway deicing fluid development and environmental regulations will also be discussed.

Oliver M. Arzt, N ICE Aircraft Services & Support GmbH; Warren M. Underwood, Federal AviationAdministration

Oliver M. Arzt, N ICE Aircraft Services & Support GmbH; Warren M. Underwood, Federal AviationAdministration

Organizers -

Organizers -

Oliver M. Arzt, N ICE Aircraft Services & Support GmbH; Warren M. Underwood, Federal AviationAdministration

Oliver M. Arzt, N ICE Aircraft Services & Support GmbH; Warren M. Underwood, Federal AviationAdministration

Chairpersons -

Chairpersons -

8:30 a.m.

9:00 a.m.

9:30 a.m.

10:30 a.m.

11:00 a.m.

2011-38-0057

2011-38-0058

2011-38-0059

2011-38-0076

2011-38-0078

Transport Canada Guidelines for Aeroplane Testing FollowingDeicing/Anti-icing Fluid Application

Issues and Testing of Non-Glycol Aircraft Ground Deicing Fluids

A Comparison of an Automated Holdover Time Determination Algorithm(Checktime) to Outdoor Aircraft Anti-icing Fluid Testing

Cloud Phase Discrimination Using the Optical Icing Conditions Detector:Wind Tunnel and Flight Test Results

Wind Tunnel Experiments with Anti-Icing Fluids

James Martin, Transport Canada

Arlene Beisswenger, Caroline Laforte, Jean Perron, Anti-Icing Materials Intl.Laboratory

Scott Landolt, National Center for Atmospheric Research; Jennifer Black,NCAR; Roy Martin Rasmussen, National Center for Atmospheric Research

Kaare J. Anderson, Goodrich Advanced Sensors Technical Center; Gary E.Halama, Mark D. Ray, Goodrich Sensors & Integrated Systems; Michael P.Nesnidal, Goodrich Advanced Sensors Technical Center; Robert Ide, SierraLobo Inc. - NASA Glenn Research Center; Michael Poellot, David Delene,University of North Dakota

Michael Papadakis, Paul Strong, See-Cheuk Wong, Wichita State Univ.

ORAL ONLY

ORAL ONLY

Time

Time

Paper No.

Paper No.

Title

Title

8:30 a.m.

10:30 a.m.

Session Time:

Session Time:

Page 19: SAE 2011 International Conference on Aircraft and Engine ... · helicopter fuselage as well as the ice accretion on a hovering rotor and ice accretion in unsteady ... Lakshmi N. Sankar,

Thursday, June 16

Thursday, June 16

Aircraft Anti-icing and Deicing Operations (Part 4 of 4)

Test and Correlation (Part 1of 2)

Session Code:

Session Code:

ICE10

ICE7

Room Salon 3

Room Salon 6

This session addresses a wide variety of research topics related to aircraft ground deicing operations including active frost detection systems, liquidwater equivalent based systems to determine and update anti-icing fluid holdover times. Aircraft flight testing and wind tunnel testing with anti-icingfluids, along with fluid modeling, runway deicing fluid development and environmental regulations will also be discussed.

The test facilities session includes papers that describe ground icing test facilities (outdoor facilities, wind tunnels, and indoor cold chambers), detailmethods for the calibration of these facilites, present new ways to use these facilities, and that present data acquired in these facilities. Ice crystal andsupercooled large drop papers are in dedicated Appendix D and Appendix O sessions.

Oliver M. Arzt, N ICE Aircraft Services & Support GmbH; Warren M. Underwood, Federal AviationAdministration

Robert J. Flemming, Sikorsky Aircraft Corp.; Richard Lewis, Airbus SAS; James MacLeod, NationalResearch Council Canada

Organizers -

Organizers -

Oliver M. Arzt, N ICE Aircraft Services & Support GmbH; Warren M. Underwood, Federal AviationAdministration

James MacLeod, National Research Council Canada

Chairpersons -

Chairpersons -

11:30 a.m.

1:30 p.m.

2:00 p.m.

2:30 p.m.

8:30 a.m.

2011-38-0077

2011-38-0085

2011-38-0084

ORAL ONLY

ORAL ONLY

An Update on the Development of an Liquid Water Equivalent-basedSystem for Determining Precipitation Intensity

Laboratory Testing and Field Demonstration of an EnvironmentallyBenign and Reduced Corrosion Runway Deicing Fluid

Airport Deicing - Changing Environmental Regulations and AirportStrategies to Respond

Study of Ground Deicing Activities in European Airports

Ice Testing on Aerodynamic Surfaces

Roy Martin Rasmussen, Scott Landolt, National Center for AtmosphericResearch; Jennifer Black, NCAR; Andrew Gaydos, National Center forAtmospheric Research

Satya P. Chauhan, Melissa Roshon, W. D. Samuels, H. Nick Conkle,Battelle Memorial Institute; Elizabeth Berman, Mary Wyderski, US Air Force

Devon Seal, John Lengel, Timothy Arendt, Gresham Smith and Partners

Alberto Lopez, European Aviation Safety Agency

Stefan Jung, Domink Raps, Vuong Doan, Tobias Strobel, EADS GermanyGmbH

ORAL ONLY

Time

Time

Paper No.

Paper No.

Title

Title

1:30 p.m.

8:30 a.m.

Session Time:

Session Time:

Page 20: SAE 2011 International Conference on Aircraft and Engine ... · helicopter fuselage as well as the ice accretion on a hovering rotor and ice accretion in unsteady ... Lakshmi N. Sankar,

Thursday, June 16

Friday, June 17

Test and Correlation (Part 2 of 2)

Closing Plenary Session (Part 1 of 2)

Session Code:

Session Code:

ICE7

ICE13

Room Salon 6

Room Empire Ballroom

The test facilities session includes papers that describe ground icing test facilities (outdoor facilities, wind tunnels, and indoor cold chambers), detailmethods for the calibration of these facilites, present new ways to use these facilities, and that present data acquired in these facilities. Ice crystal andsupercooled large drop papers are in dedicated Appendix D and Appendix O sessions.

Robert J. Flemming, Sikorsky Aircraft Corp.; Richard Lewis, Airbus SAS; Mark G. Potapczuk, NASAGlenn Research Center

Organizers -

Mark G. Potapczuk, NASA Glenn Research CenterChairpersons -

Richard Moser, Aerotex UK; Mark G. Potapczuk, NASA Glenn Research CenterModerators -

9:00 a.m.

9:30 a.m.

10:30 a.m.

11:00 a.m.

11:30 a.m.

8:30 a.m.

9:00 a.m.

9:30 a.m.

2011-38-0092

2011-38-0093

2011-38-0099

2011-38-0100

2011-38-0101

ORAL ONLY

ORAL ONLY

ORAL ONLY

An Experimental Correlation between Rotor Test and Wind Tunnel IceShapes on NACA 0012 Airfoils

Comparison of Experimental and Computational Ice Shapes for a SweptWing Model

Development of a Unique Icing Spray System for a New Facility forCertification of Large Turbofan Engines

Low Weight, Low Power, Electric Pulsed Deicer

S-76D¿ Tail Rotor Ice Impact Test

Inflight Icing Track Update

Icing Meteorology Track Update

Aircraft De/Anti-icing during Ground Operations Track Update

Yiqiang Han, Jose Luis Palacios, Edward C. Smith, Penn State Univ-University Park

See-Cheuk Wong, Michael Papadakis, Hsiung-Wei Yeong, See Ho Wong,Wichita State Univ.

James MacLeod, National Research Council Canada; John Jastremski,MDS Aero Support Corp.

Joseph J. Gerardi, Innovative Dynamics Inc.

Regina Kuznetsova, Sikorsky Aircraft Corp.

Robert J. Flemming, Sikorsky Aircraft Corp.

Ben C. Bernstein, Leading Edge Atmospherics

Warren Underwood, Federal Aviation Administration

ORAL ONLY

Time

Time

Paper No.

Paper No.

Title

Title

10:30 a.m.

8:30 a.m.

Session Time:

Session Time:

Page 21: SAE 2011 International Conference on Aircraft and Engine ... · helicopter fuselage as well as the ice accretion on a hovering rotor and ice accretion in unsteady ... Lakshmi N. Sankar,

Friday, June 17

Closing Plenary Session (Part 2 of 2)Session Code: ICE13

Room Empire Ballroom

Richard Moser, Aerotex UK; Mark G. Potapczuk, NASA Glenn Research CenterModerators -

10:30 a.m. ORAL ONLY An FAA Update on Aircraft Icing

Thomas H. Bond, Federal Aviation Adminstration

Time Paper No. Title

10:30 a.m.Session Time: