Hamid Reza Ovesy - Amirkabir University of Technologyaerospace.aut.ac.ir/autcms/res/upload/aerospace-engineering/ovesy... · Calculation of Initial Post-Buckling Stiffness of Shear-Deformable

Last Updated June 2014

Hamid Reza OvesyProfessor

OFFICE:Aerospace Engineering Department, Amirkabir University of Technology, Hafez Ave.,#424, Tehran, Iran.Tel: +98-21-64543215Fax: +98-21-66959020E-mail: [email protected] site: www.aut.ac.ir/departments/aero

EDUCATION:1998 - Cranfield University, England – PhD, Aerospace Structural Engineering.1994 - Cranfield University, England - M.Sc. Aerospace Vehicle Design (AVD).1988 - Tehran University, Tehran, Iran - B.Sc., Mechanical Engineering.

PROFESSIONAL EXPERIENCE:1998, Assistant Professor, Dept. of Aerospace Eng., Amirkabir Univ. of Technology;2005, Associate Professor, Dept. of Aerospace Eng., Amirkabir Univ. of Technology;2009, Professor, Dept. of Aerospace Eng., Amirkabir Univ. of Technology;

2001-2003, Vice-Head of Aerospace Eng. Dept. in Educational Affairs, Amirkabir Univ. ofTechnology;2003-2004, Vice-Head of Aerospace Eng. Dept. in Research Affairs, Amirkabir Univ. ofTechnology;2004-2005, Head of Dept. of Aerospace Eng., Amirkabir Univ. of Technology;2008-2010, Head of Structural & Flight Mechanics Group, Dept. of Aerospace Eng., AmirkabirUniv. of Technology;2009-2012 Head of Center of Excellence in Computational Aerospace Engineering;2009-2013, Editorial Board Member, Journal of Composite Structures (Elsevier-ISSN:0263-8223).

Since 1999, Member of Structural & Flight Mechanics Group, Dept. of Aerospace Eng.,Amirkabir Univ. of Technology;Since 2000, Member of IAS (Iranian Aerospace Society);Since 2006, Establishing and Heading the Composite Material Lab, Dept. of Aerospace Eng.,Amirkabir Univ. of Technology;Since 2007, Board Member, Center of Excellence in Computational Aerospace Engineering;Since 2009, Editorial Board Member, Journal of Thin-walled Structures (Elsevier-ISSN:0263-8231);

Since 2010, Member of Composite Group, Dept. of Mechanical Eng., Amirkabir Univ. ofTechnology;Since 2010, Vice-Head of Aerospace Eng. Dept. in Educational Affairs, Amirkabir Univ. ofTechnology;Since 2014, Editorial Board Member, Amirkabir Journal of Science and Technology;


TAUGHT COURSES:

Undergraduate: Strength of Materials; Mechanical Vibrations; Dynamics I;Dynamics II;

Post-graduate: Structural Stability; Finite Element Analysis; Advanced AerospaceStructural Design; Mechanics of Composite Materials;

RESEARCH INTERESTS:

Analysis and Design of Aircraft Structures;Linear and Non-linear Finite Strip Methods;Delamination Buckling, Post-buckling and Growth Analysis;Non-local Elasticity Analysis;Parametric & Dynamic Instability Analysis of Composite Structures;Instability and Large Deformation Analysis of Intelligent Structures;Thermo-mechanical Analysis of FGM;Fluid-Structure Interaction Analysis.

KEYNOTE LECTURING:

Title: Large Deflection Behaviour of Functionally Graded Plates under Pressure Loads,

Using Finite Strip Method

The Third European Conference on Computational Mechanics Solids, Structures and

Coupled Problems in Engineering (ECCM 2006), Lisbon, Portugal, 5–8 June 2006.


PEER-REVIEWED JOURNAL PAPERS:

64) P. Khaneh Masjedi, H. R. Ovesy, ”Aeroelastic Instability of Composite Wings by theConsideration of Different Structural Constitutive Assumptions”, Journal of Fluids andStructures., (In Press - Available online 28 May 2014).

63) H. R. Ovesy, P. Khaneh Masjedi, ”Investigation of the Effects of ConstitutiveEquations on the Free Vibration Behavior of Single-Celled Thin-Walled CompositeBeams”, Mechanics of Advanced Materials and Structures., 2014, Vol. 21, pp 842-858.

62) M. Hajikazemi, H. R. Ovesy, H. Assaee, M. H. Sadr, ”Post-Buckling Finite StripAnalysis of Thick Functionally Graded Plates”, Structural Engineering and Mechanics.,2014, Vol. 49, No. 5, pp 569-595.

61) S. A. M. Ghannadpour, H. R. Ovesy, E. Zia-Dehkordi, ”An Exact Finite Strip for theCalculation of Initial Post-Buckling Stiffness of Shear-Deformable Composite LaminatedPlates”, Composite Structures., 2014, Vol. 108, Issue 1, pp 504-513.

60) H. R. Ovesy, J. Fazilati, ”Parametric Instability Analysis of Laminated CompositeCurved Shells Subjected to Non-Uniform In-Plane Load”, Composite Structures., 2014,Vol. 108, Issue 1, pp 449-455.

59) M. Kharazi, H. R. Ovesy, M. Asghari Mooneghi, ”Buckling Analysis of DelaminatedComposite Plates Using a Novel Layerwise Theory”, Thin-Walled Structures., 2014, Vol.74, No. 1, pp 246-254.

58) M. H. Sherafat, H. R. Ovesy, S. A. M. Ghannadpour, “Buckling Analysis ofFunctionally Graded Plates under Mechanical Loading Using Higher OrderFunctionally Graded Strip”, International Journal of Structural Stability and Dynamics.,2013, Vol. 13, No. 6.

57) M. H. Sherafat, S. A. M. Ghannadpour, H. R. Ovesy, ”Pressure Loading, End-Shortening and Through-Thickness Shearing Effects on Geometrically NonlinearResponse of Composite Laminated Plates Using Higher Order Finite Strip Method”,Structural Engineering and Mechanics., 2013, Vol. 45, No. 5, pp 677-691.

56) A. Koochi, M. Abadyan, H. Hosseini-Toudeshky, H. R. Ovesy, “Modeling TheInfluence of Surface Effect on Instability of Nano-CantileveriIn Presence of Van DerWaals Force”, International Journal of Structural Stability and Dynamics., 2013, Vol. 13,No. 4.


55) H. R. Ovesy, S. A. M. Ghannadpour, E. Zia-Dehkordi, ”Buckling Analysis ofModerately Thick Composite Plates and Plate Structures Using an Exact Finite Strip”,Composite Structures., 2013, Vol. 95, Issue 1, pp 697-704.

54) J. Fazilati, H. R. Ovesy, ”Parametric Instability of Laminated LongitudinallyStiffened Curved Panels with Cutout Using Higher Order FSM”, Composite Structures.,2013, Vol. 95, Issue 1, pp 691-696.

53) H. R. Ovesy, A. Nikou, H. Shahverdi, ”Flutter Analysis of High-Aspect-Ratio WingsBased on a Third-Order Nonlinear Beam Model”, Proc IMechE Part G: J AerospaceEngineering., 2012, Vol. 227, Issue 7, pp 1090-110

52) S. A. M. Ghannadpour, H. R. Ovesy, M. Nassirnia, “An Investigation on BucklingBehaviour of Functionally Graded Plates Using Finite Strip Method”, AppliedMechanics and Materials, 2012, Vols. 152-154, pp 1470-1476.

51) H. Assaee, H. R. Ovesy, M. Hajikazemi, ”A Semi-Energy Finite Strip Non-LinearAnalysis of Imperfect Composite Laminates Subjected to End-Shortening”, Thin-WalledStructures., 2012, Vol. 60, pp 46-53.

50) S. A. M. Ghannadpour, H. R. Ovesy, M. Nassirnia, ”Buckling Analysis ofFunctionally Graded Plates Under Thermal Loadings Using The Finite Strip Method”,Computers & Structures., 2012, Vols. 108-109, pp 93-99.

49) H. R. Ovesy, M. Taghizadeh, M. Kharazi, ”Post-Buckling Analysis of CompositePlates Containing Embedded Delaminations with Arbitrary Shape by Using HigherOrder Shear Deformation Theory”, Composite Structures., 2012, Vol. 94, Issue 3, pp1243-1249.

48) H. R. Ovesy, J. Fazilati, “Lay-up Effects on the Dynamic Instability of ModeratelyThick Stiffened Curved Panels”, Applied Mechanics and Materials, 2012, Vols. 152-154,pp 1477-1482.

47) H. Assaee, M. Hajikazemi, H. R. Ovesy, ”The Effect of Anisotropy on Post-BucklingBehavior of Laminated Plates Using Semi-Energy Finite Strip Method”, CompositeStructures., 2012, Vol. 94, Issue 5, pp 1880-1885.

46) H. R. Ovesy, J. Fazilati, ”Parametric Instability Analysis of Moderately Thick FGMCylindrical Panels Using FSM”, Computers & Structures., 2012, Vols. 108-109, pp 135-143.

45) S. A. M. Ghannadpour, H. R. Ovesy, ”High Accuracy Postbuckling Analysis ofChannel Section Struts”, Non-Linear Mechanics., 2012, Vol. 47, pp 968-974.


44) H. R. Ovesy, J. Fazilati, ”Buckling and Free Vibration Finite Strip Analysis ofComposite Plates with Cutout Based on Two Different Modeling Approaches”,Composite Structures., 2012, Vol. 94, Issue 3, pp 1250-1258.

43) H. R. Ovesy, M. Hajikazemi, H. Assaee, ”A Novel Semi Energy Finite Strip Methodfor Post-Buckling Analysis of Relatively Thick Anti-Symmetric Laminated Plates”,Advances in Engineering Software., 2012, Vol. 48, Issue 1, pp 32-39.

42) J. Fazilati, H. R. Ovesy, ”Finite Strip Dynamic Instability Analysis of PerforatedCylindrical Shell Panels”, Composite Structures., 2012, Vol. 94, Issue 3, pp 1259-1264.

41) S. A. M. Ghannadpour, H. R. Ovesy, M. Nassirnia, ”High Accuracy PostbucklingAnalysis of Box Section Struts”, Applied Mathematics and Mechanics (ZAMM)., 2012,Vol. 92, No. 8, pp 668-680.

40) H. R. Ovesy, M. Kharazi, ”Stability Analysis of Composite Plates with Through-the-Width Delamination”, Engineering Mechanics (ASCE)., 2011, Vol. 137, No. 2, pp 87-100.

39) H. R. Ovesy, M. H. Sadr, M. Hajikazemi, H. Assaee, ”Large Deflection Behavior ofComposite Laminated Plates Under End-Shortening and Normal Pressure LoadingUsing a Semi-Energy Finite Strip Method”, Key Engineering Materials., 2011, Vols. 471-472, pp 423-437.

38) S. A. M. Ghannadpour, H. R. Ovesy, M. Nassirnia, “Nonlinear Post BucklingAnalysis of Isotropic Plates Using Finite Strip Methods”, Journal of Aerospace Scienceand Technology (JAST), 2011, Vol. 8, No. 1, pp 11-19.

37) M. Nassirnia, H. R. Ovesy, S. A. M. Ghannadpour, ”Thermal Buckling Analysis ofModerately Thick Plates Using Functionally Graded Strips”, Key Engineering Materials.,2011, Vols. 471-472, pp 757-762.

36) H. R. Ovesy, H. Assaee, M. Hajikazemi, ”Post-Buckling of Thick SymmetricLaminated Plates Under End-Shortening and Normal Pressure Using Semi-Energy FiniteStrip Method”, Computers & Structures., 2011, Vol. 89, Issue 9-10, pp 724-732.

35) S. A. M. Ghannadpour, H. R. Ovesy, M. Hajikazemi, ”An Investigation on RelativePost-Buckling Stiffness Variations of Symmetrically Cross-Ply Laminates”, KeyEngineering Materials., 2011, Vols. 471-472, pp 1022-1027.

34) H. R. Ovesy, S. A. M. Ghannadpour, ”An Exact Finite Strip For The InitialPostbuckling Analysis of Channel Section Struts”, Computers & Structures., 2011, Vol.89, Issue 19-20, pp 1785-1796.


33) J. Fazilati, H. R. Ovesy, ”Boundary Condition Effects on the Parametric Stability ofModerately Thick Laminated Cylindrical Panels”, Key Engineering Materials., 2011,Vols. 471-472, pp 466-471.

32) H. R. Ovesy, M. Kharazi, ”Compressional Stability Behavior of Composite Plateswith Through-the-Width and Embedded Delaminations by Using First Order ShearDeformation Theory”, Computers & Structures., 2011, Vol. 89, Issue 19-20, pp 1829-1139.

31) M. Hajikazemi, H. R. Ovesy, M. H. Sadr, ”A Semi- Energy Finite Strip Method forPost-Buckling Analysis of Relatively Thick Anti-Symmetric Cross-Ply Laminates”, KeyEngineering Materials., 2011, Vols. 471-472, pp 426-431.

30) S. A. M. Ghannadpour, H. R. Ovesy, ”Relative Post-buckling Stiffness Calculation ofSymmetrically Laminated Composite Plates Using An Exact Finite Strip”, AdvancedMaterials Research., 2010, Vols. 123-125, pp 201-204.

29) H. R. Ovesy, M. Kharazi, M. Taghizadeh, ”Semi-Analytical Buckling Analysis ofClamped Composite Plates Containing Embedded Rectangular And CircularDelaminations”, Mechanics of Advanced Materials and Structures., 2010, Vol. 17, Issue5, pp 343-352.

28) M. Kharazi, H. R. Ovesy, ”Large Deflection Compressional Analysis ofUnsymmetric Delaminated Composite Plates with Consideration of ContactPhenomenon”, Applied Composite Materials., 2010, Vol. 17, Issue 5, pp 515-528.

27) J. Fazilati, H. R. Ovesy, ”Dynamic Instability Analysis of Composite LaminatedThin-Walled Structures Using Two Versions of FSM”, Composite Structures., 2010, Vol.92, Issue 9, pp 2060-2065.

26) H. R. Ovesy, S. A. M. Ghannadpour, M. H. Sherafat, ”Buckling Analysis ofLaminated Composite Plates Using Higher-order Semi–analytical Finite Strip Method”,Applied Composite Materials., 2010, Vol. 17, Issue 2, pp 69-80.

25) M. Kharazi, H. R. Ovesy, M. Taghizadeh, ”Buckling of The Composite LaminatesContaining Through-The-Width Delaminations Using Different Plate Theories”,Composite Structures., 2010, Vol. 92, No. 5, pp 1176-1183.

24) H. R. Ovesy, J. Loughlan, S. A. M. Ghannadpour, ”An Investigation on the Post-local-buckling Analysis of I-section Struts using Finite Strip Method”, Advanced SteelConstruction., 2010, Vol. 6, No. 1, pp 662-677.

23) M. Kharazi, H. R. Ovesy, “Buckling of Laminates with Multiple Through-the-WidthDelaminations by Using Spring Simulation Model”, Amirkabir International Journal ofModeling, Identification,Simulation & Control., 2010, Vol. 42, No. 2, pp 17-25.


22) S. A. M. Ghannadpour, H. R. Ovesy, ”Exact Postbuckling Stiffness Calculation ofBox Section Struts”, Engineering Computations, Int. J. for Computer Aided Engineeringand Software., 2009, Vol. 26, Issue 7, pp 868-893.

21) H. R. Ovesy, S. A. M. Ghannadpour, ”An Exact Finite Strip for the Calculation ofRelative Post-Buckling Stiffness of Isotropic Plates”, Structural Engineering andMechanics., 2009, Vol. 31, No. 2, pp 181-210.

20) S. A. M. Ghannadpour, H. R. Ovesy, ”The Application of an Exact Finite Strip to theBuckling of Symmetrically Laminated Composite Rectangular Plates and Prismatic PlateStructures”, Composite Structures., 2009, Vol. 89, pp 151-158.

19) H. R. Ovesy, J. Fazilati, ”Stability Analysis of Composite Laminated Plate andCylindrical Shell Structures Using Semi-Analytical Finite Strip Method”, CompositeStructures., 2009, Vol. 89, pp 467-474.

18) H. R. Ovesy, H. Assaee, ”Semi-Energy Finite Strip Post-Buckling Analysis ofLaminated plates Concerning the Effects of Mechanical Coupling”, CompositeStructures., 2009, Vol. 89, pp 120-125.

17) M. Kharazi, H. R. Ovesy, “Compressional Stability Behavior of Composite Plateswith Multiple Through-the-Width Delaminations”, Journal of Aerospace Science andTechnology (JAST), 2008, Vol. 5, No. 1, pp 13-22.

16) S. A. M. Ghannadpour, H. R. Ovesy, ”An Exact Finite Strip for the Calculation ofRelative Post-Buckling Stiffness of I-section Struts”, International Journal of MechanicalSciences., 2008, Vol. 50, pp 1354-1364.

15) M. Kharazi, H. R. Ovesy, ”Postbuckling Behavior of Composite Plates withThrough-the-Width Delaminations”, Thin-Walled Structures., 2008, Vol. 46, pp 939-946.

14) H. R. Ovesy, H. Assaee, “The Effects of Bend-Twist Coupling on the Post-BucklingCharacteristics of Composite Laminated Plates Using Semi-Energy Finite StripApproach”, Thin-Walled Structures., 2007, Vol. 45, pp 209-220.

13) H. R. Ovesy, S. A. M. GhannadPour, “Large Deflection Finite Strip Analysis ofFunctionally Graded Plates Under Pressure Loads”, International Journal of StructuralStability and Dynamics., 2007, Vol. 7, No. 2, pp 1-19.

12) H. Assaee, H. R. Ovesy, “A Multi-term Semi-energy Finite Strip Method for Post-buckling Analysis of Composite Plates” , International Journal of Numerical Methods inEngineering., 2007, Vol. 70, Issue 11, pp 1303-1323.

11) H. Hosseini-Toudeshky, B. Mohammadi, B. Hamidi, H. R. Ovesy, ”Analysis ofComposite Skin/Stiffener Debounding and Failure under Uniaxial Loading” , CompositeStructures., 2006, Vol. 75, pp 428-436.


10) H. R. Ovesy, J. Loughlan, S. A. M. Ghannadpour, G. Morada, “Geometric Non-linear Analysis of Box Sections Under End Shortening, Using Three Different Versions ofthe Finite Strip Method”, Thin-Walled Structures., 2006, Vol. 44, pp 623-637.

9) H. R. Ovesy , S. A. M. Ghannadpour, ”Geometric Nonlinear Analysis of ImperfectComposite Laminated Plates, Under End Shortening and Pressure loading, Using FiniteStrip Method”, Composite Structures., 2006, Vol. 75, pp 100-105.

8) H. R. Ovesy , S. A. M. GhannadPour, G. Morada, ”Post-buckling Behavior ofComposite Laminated Plates Under End Shortening and Pressure Loading, Using TwoVersions of Finite Strip Method”, Composite Structures., 2006, Vol. 75, pp 106-113

7) H. R. Ovesy, J. Loughlan, S. A. M. Ghannadpour, ”Geometric Non-Linear Analysis ofChannel Sections Under End Shortening, Using Different Versions of the Finite StripMethod”, Computers & Structures., 2006, Vol. 84, pp 855-872.

6) H. R. Ovesy, H. Assaee, “An Investigation on the Post-Buckling Behavior ofSymmetric Cross-Ply Laminated Plates Using a Semi-Energy Finite Strip Approach” ,Composite Structures., 2005, Vol. 71, pp 365-370.

5) H. R. Ovesy , S. A. M. Ghannadpour, G. Morada, ”Geometric Nonlinear Analysis ofComposite Laminated Plates with Initial Imperfection Under End Shortening, Using TwoVersions of Finite Strip Method”, Composite Structures., 2005, Vol. 71, pp 307-314.

4) H. Hosseini-Toudeshky, H. R. Ovesy and M. Kharazi, “The Development of anApproximate Method for the Design of Bead-Stiffened Composite Panels”, Thin-WalledStructures., 2005, Vol. 43, pp 1663-1676.

3) H. R. Ovesy, J. Loughlan, S. A. M. Ghannadpour, ”Geometric Non-Linear Analysis ofThin Flat Plates Under End Shortening, Using Different Versions of Finite StripMethod”, International Journal of Mechanical Sciences., 2005, Vol. 47, pp 1923-1948.

2) H. R. Ovesy, H. Assaee, “Finite Strip Buckling Analysis of Some Composite StiffenedBox Sections”, AIAA Journal., 2004, Vol. 42, pp 2382-2384.

1) H. R. Ovesy, J. Loughlan, H. Assaee, “The Compressive Post-Local BucklingBehavior of Thin Plates Using a Semi-Energy Finite Strip Approach”, Thin-WalledStructures., 2004, Vol. 42, pp 449–474.


PEER-REVIEWED CONFERENCE PAPERS:

111) H. Assaee, M. Hajikazemi, H. R. Ovesy, ”Semi-Energy Finite Strip Nonlinear Post-Buckling Analysis of Composite Laminated Plates under Non-uniform Compression”,Proceedings of the 4th Canadian Conference on Nonlinear Solid Mechanics (CanCNSM2013), McGill University, Montreal, Canada, (23-26 July 2013).

110) H. R. Ovesy, J. Fazilati, ”Parametric Instability Analysis of Laminated Flat andCylindrical Panels Subjected to Non-Uniform In-Plane Loads”, Proceedings of theSeventeenth International Conference on Composite Structures (ICCS 17), University ofPorto, Porto, Portugal, (17-21 June 2013).

109) M. Taghizadeh, H. R. Ovesy, S. A. M. Ghannadpour, ”Finite Element BendingAnalysis of Nanoplates Based on Nonlocal Integral Elasticity”, Proceedings of theSeventeenth International Conference on Composite Structures (ICCS 17), University ofPorto, Porto, Portugal, (17-21 June 2013).

108) H. R. Ovesy, S. A. M. Ghannadpour, A. Totounferoush, ”Dynamic BucklingAnalysis of Delaminated Composite Plates with Piezoelectric Layers Subjected toElectro-Mechanical Loads”, Proceedings of the Seventeenth International Conference onComposite Structures (ICCS 17), University of Porto, Porto, Portugal, (17-21 June 2013).

107) S. A. M. Ghannadpour, H. R. Ovesy, E. Zia-Dehkordi, ”An Exact Finite Strip forthe Calculation of Relative Post-Buckling Stiffness of Thick Composite Plates”,Proceedings of the Seventeenth International Conference on Composite Structures (ICCS17), University of Porto, Porto, Portugal, (17-21 June 2013).

106) H. R. Ovesy, H. Shirmohammadali, J. Fazilati, “Buckling Analysis of ThinPerforated Composite Panel by Using Spline Finite Strip Method” , Proceedings (InPersian) of the 12th Conference of Iranian Aerospace Society (Aero 2013), AmirkabirUniversity of Technology, Iran, (20-22 Feb 2013).

105) M. Taherzadeh Esfahani, M. Z. Kabir, H. R. Ovesy, ”Local Buckling of InitiallyDelaminated Composite Columns, Using First Order Shear Deformation Theory”,Proceedings of the Third International Conference on Composites: Characterization,Fabrication and Application (CCFA-3), Tehran, Iran, (18-19 December 2012).

104) N. Kharghani, M. Kharazi, H. R. Ovesy, ”Prediction of the Initiation of MultipleThrough-the-Width Delaminations Propagation in Cross Ply Composite Laminates UsingLayerwise Theory”, Proceedings of the Third International Conference on Composites:Characterization, Fabrication and Application (CCFA-3), Tehran, Iran, (18-19 December2012).


103) H. R. Ovesy, M. Naghinejad, ”The Layup Configuration Effects on the PostBuckling and Delamination Growth Characteristic of Composite Plates”, Proceedings ofthe Third International Conference on Composites: Characterization, Fabrication andApplication (CCFA-3), Tehran, Iran, (18-19 December 2012).

102) H. R. Ovesy, S. A. M. GhannadPour, M. Nassirnia, ”Thermal PostbucklingBehaviour of Rectangular Functionally Grade Plate Using Finite Strip Method”,Proceedings of the Eleventh International Conference on Computational StructuresTechnology, B.H.V. Topping (Editor), Civil-Comp Press, Dubrovnik, Croatia, (4-7September 2012).

101) S. A. M. GhannadPour, H. R. Ovesy, E. Zia-Dehkordi, ”Calculation of Initial Post-Buckling Behavior of Moderately Thick Plates Using an Exact Finite Strip”, Proceedingsof the Eleventh International Conference on Computational Structures Technology,B.H.V. Topping (Editor), Civil-Comp Press, Dubrovnik, Croatia, (4-7 September 2012).

100) M. Taghizadeh, H. R. Ovesy, M. Kharazi, ”Semi-Analytical Post-Buckling Analysisof Composite Plates Containing Free Edge Embedded Delaminations by Using HigherOrder Shear Deformation Theory”, Proceedings of the 8th European Solid MechanicsConference (ESMC 2012), Graz University of Technology, Graz, Austria, (9-13 July2012).

99) J. Fazilati, H. R. Ovesy, ”Parametric Instability of Laminated LongitudinallyStiffened Curved Panels with Cutout Using Higher Order FSM”, Proceedings of theInternational Conference on Mechanics of Nano, Micro and Macro Composite Structures(ICNMMCS), Politecnico di Torino, Torino, Italy, (18-20 June 2012).

98) M. Kharazi, N. Kharghani, H. R. Ovesy, ”Prediction of The Initiation ofDelamination Propagation in Composite Laminates Using Layerwise FSDT ForUnsymmetric Lay-Up Sequences”, Proceedings of the International Conference onMechanics of Nano, Micro and Macro Composite Structures (ICNMMCS), Politecnico diTorino, Torino, Italy, (18-20 June 2012).

97) H. R. Ovesy, S. A. M. Ghannadpour, E. Zia-Dehkordi, ”Buckling Analysis ofModerately Thick Composite Plates and Plate Structures Using an Exact Finite Strip”,Proceedings of the International Conference on Mechanics of Nano, Micro and MacroComposite Structures (ICNMMCS), Politecnico di Torino, Torino, Italy, (18-20 June2012).

96) M. H. Sherafat, H. R. Ovesy, S.A.M. Ghannadpour, ”Buckling Analysis ofFunctionally Graded Plates (FGPs) under Mechanical Loading Using Higher OrderFunctionally Graded Strip (FGS)”, Proceedings of the Fourth International Conferenceon Structural Stability and Dynamics (ICSSD 2012), Jaipur, India, (4-6 January 2012).


95) M. H. Sherafat, S.A.M. Ghannadpour, H. R. Ovesy, ”Through- Thickness ShearingEffects on Post-Buckling Behavior of Composite Laminated Plates under End Shorteningand Pressure Loading, Using Finite Strip Method”, Proceedings of the FourthInternational Conference on Structural Stability and Dynamics (ICSSD 2012), Jaipur,India, (4-6 January 2012).

94) A. Nikou, H. R. Ovesy, ”Evaluation of a Set of Nonlinear Dynamic Equations ofInextensional Beams with Application in Modeling High Aspect-Ratio Wings”,Proceedings of the First International Conference on Acoustics and Vibration (ISAV2011), Amirkabir University of Technology, Tehran, Iran, (20-21 December 2011).

93) H. R. Ovesy, M. Taghizadeh, M. Kharazi, ”Post-Buckling Analysis of CompositePlates Containing Embedded Delaminations with Arbitrary Shape by Using HigherOrder Shear Deformation Theory”, Proceedings of the Sixteenth InternationalConference on Composite Structures (ICCS 16), University of Porto, Porto, Portugal,(28-30 June 2011).

92) H. Assaee, M. Hajikazemi, H. R. Ovesy, ”The Effect of Anisotropy on Post-BucklingBehavior of Laminated Plates Using Semi-Energy Finite Strip Method”, Proceedings ofthe Sixteenth International Conference on Composite Structures (ICCS 16), University ofPorto, Porto, Portugal, (28-30 June 2011).

91) J. Fazilati, H. R. Ovesy, ”Finite Strip Dynamic Instability Analysis of PerforatedCylindrical Shell Panels”, Proceedings of the Sixteenth International Conference onComposite Structures (ICCS 16), University of Porto, Porto, Portugal, (28-30 June 2011).

90) H. R. Ovesy, J. Fazilati, ”Buckling and Free Vibration Finite Strip Analysis ofComposite Plates with Cutout Based on Two Different Modeling Approaches”,Proceedings of the Sixteenth International Conference on Composite Structures (ICCS16), University of Porto, Porto, Portugal, (28-30 June 2011).

89) M. Hajikazemi, H. R. Ovesy, M. H. Sadr, ”A Semi-Energy Finite Strip Method forPost-Buckling Analysis of Relatively Thick Anti-Symmetric Cross-Ply Laminates”,Proceedings of the Eight International Conference on Composite Science & Technology(ICCST/8), Kuala Lumpur, Malaysia, (22-24 March 2011).

88) H. R. Ovesy, M. H. Sadr, M. Hajikazemi, H. Assaee, ”Large Deflection Behaivior ofComposite Laminated Plates Under End-shortening and Normal Pressure Loading Usinga Semi-Energy Finite Strip Method”, Proceedings of the Eight International Conferenceon Composite Science & Technology (ICCST/8), Kuala Lumpur, Malaysia, (22-24March 2011).

87) M. Javadiyeh, H. R. Ovesy, “Lay-up configuration effects on the transient responseof laminated composite plates by finite strip method” , Proceedings of the 9th IranianAerospace Society Conference , Islamic Azad University, Science and Research Branch,Tehran, Iran, (8-10 Feb. 2010).


86) A. Hadi, H. R. Ovesy, “ Investigation of Torsional Behavior of Thin-Walled Glass-Epoxy Composite Box Beams in Helicopter Main Rotor Blade Application” , Proceedingsof the 9th Iranian Aerospace Society Conference , Islamic Azad University, Science andResearch Branch, Tehran, Iran, (8-10 Feb. 2010).

85) H. Assaee, H. R. Ovesy, M. Hajikazemi, M.H. Sadr, ”Post-Buckling Behavior ofThin and Relatively Thick Symmetric Laminated Plates Under End-Shortening andNormal Pressure Loading Using Semi Energy Finite Strip Method”, Proceedings of theFourth European Conference on Computational Mechanics Solids, Structures andCoupled Problems in Engineering (ECCM 2010), Paris, France, (16-21 May 2010).

84) H. R. Ovesy, P. Khaneh Masjedi, ”Free Vibration of Torsion-Bending Coupled Thin-walled Composite Beams”, Proceedings of the Fourth European Conference onComputational Mechanics Solids, Structures and Coupled Problems in Engineering(ECCM 2010), Paris, France, (16-21 May 2010).

83) S. A. M. GhannadPour, H. R. Ovesy, M. Nassirnia, ”Thermal Buckling Analysis ofFunctionally Graded Plates using the Finite Strip Method”, Proceedings of the TenthInternational Conference on Computational Structures Technology, B.H.V. Topping,J.M. Adam, F.J. Pallarés, R. Bru and M.L. Romero (Editors), Civil-Comp Press,Valencia, Spain, (14-17 September 2010).

82) H. Assaee, H. R. Ovesy, M. Hajikazemi, M.H. Sadr Lahidjani, ”The Effects of AspectRatio on Postbuckling Behavior of Rectangular Plates of Functionally GradedMaterials”, Proceedings of the Tenth International Conference on ComputationalStructures Technology, B.H.V. Topping, J.M. Adam, F.J. Pallarés, R. Bru and M.L.Romero (Editors), Civil-Comp Press, Valencia, Spain, (14-17 September 2010).

81) H. R. Ovesy, J. Fazilati, ”Dynamic Stability of Functionally Graded MaterialCylindrical Shells Based on Higher-Order Theory Using the Finite Strip Method”,Proceedings of the Tenth International Conference on Computational StructuresTechnology, B.H.V. Topping, J.M. Adam, F.J. Pallarés, R. Bru and M.L. Romero(Editors), Civil-Comp Press, Valencia, Spain, (14-17 September 2010).

80) H. R. Ovesy, M. Hajikazemi, H. Assaee, ”A Semi Energy Finite Strip Method forPost-Buckling Analysis of Relatively Thick Laminates”, Proceedings of the TenthInternational Conference on Computational Structures Technology, B.H.V. Topping,J.M. Adam, F.J. Pallarés, R. Bru and M.L. Romero (Editors), Civil-Comp Press,Valencia, Spain, (14-17 September 2010).

79) H. R. Ovesy, M. Kharazi, M. Taghizadeh, ”Post-Buckling Analysis of CompositePlates Containing Embedded Delaminations by using Higher Order Shear DeformationTheory”, Proceedings of the Tenth International Conference on Computational StructuresTechnology, B.H.V. Topping, J.M. Adam, F.J. Pallarés, R. Bru and M.L. Romero(Editors), Civil-Comp Press, Valencia, Spain, (14-17 September 2010).


78) M. Kharazi, M. Taghizadeh, H. R. Ovesy, ”Compressional Stability Analysis ofComposite Plates with Multiple Through-the-Width Delaminations by using HigherOrder Shear Deformation Theory”, Proceedings of the Tenth International Conference onComputational Structures Technology, B.H.V. Topping, J.M. Adam, F.J. Pallarés, R. Bruand M.L. Romero (Editors), Civil-Comp Press, Valencia, Spain, (14-17 September 2010).

77) S. A. M. GhannadPour, H. R. Ovesy, M. Nassirnia, ”High Accuracy Post-bucklingAnalysis of Box Section Struts using Three Different Versions of Finite Strip Method”,Proceedings of the Tenth International Conference on Computational StructuresTechnology, B.H.V. Topping, J.M. Adam, F.J. Pallarés, R. Bru and M.L. Romero(Editors), Civil-Comp Press, Valencia, Spain, (14-17 September 2010).

76) H. R. Ovesy, S. A. M. Ghannadpour, M. Nassirnia, ”Buckling Analysis of ModeratelyThick FGM Plates using the Finite Strip Method”, Proceedings of the SecondInternational Conference on Composites: Characterization, Fabrication and Application(CCFA-2), Kish Island, Iran, (27-30 December 2010).

75) H. R. Ovesy, M. Kharazi, M. Asghari Mooneghi, ”Buckling Analysis of CompositeLaminates with Through-The-Width Delamination Using a Novel Layerwise Theory”,Proceedings of the Second International Conference on Composites: Characterization,Fabrication and Application (CCFA-2), Kish Island, Iran, (27-30 December 2010).

74) H. R. Ovesy, H. Assaee, M. Hajikazemi, ”An Investigation on Post BucklingBehavior of Functionally Graded Plate Using A Semi Energy Finite Strip Approach” ,Proceedings of the IJSSD Symposium on Progress in Structural Stability and Dynamics,Hong Kong, China, (16-18 December 2009).

73) H. R. Ovesy, S.A.M. Ghannadpour, M. Nassirnia, ”High Accuracy PostbucklingAnalysis of Some Isotropic Plates Using Two Different Versions of Finite Strip Method” ,Proceedings of the IJSSD Symposium on Progress in Structural Stability and Dynamics,Hong Kong, China, (16-18 December 2009).

72) J. Fazilati, H. R. Ovesy, ”Dynamic Stability of Laminated Cylindrical Shells Basedon A Higher-Order Shear Deformation Theory Using FSM” , Proceedings of the IJSSDSymposium on Progress in Structural Stability and Dynamics, Hong Kong, China, (16-18December 2009).

71) J. Fazilati, H. R. Ovesy, “Prediction of The Dynamic Behavior of FunctionallyGraded Thin Cylindrical Shells Using Finite Strip Method” , Proceedings of the 17th

Annual Conference (International) of Mechanical Engineering (ISME 2009), TehranUniversity, Iran,( May 2009).


70) J. Fazilati, H. R. Ovesy, ”Dynamic Instability Analysis of Composite LaminatedThin-Walled Structures Using Two Versions Of Fsm” , Proceedings of the FifteenthInternational Conference on Composite Structures (ICCS/15), University of Porto, Porto,Portugal, (15-17 June 2009).

69) M. Kharazi, H. R. Ovesy, M. Taghizadeh, ”Buckling of The Composite LaminatesContaining Through-The-Width Delaminations Using Different Plate Theories” ,Proceedings of the Fifteenth International Conference on Composite Structures(ICCS/15), University of Porto, Porto, Portugal, (15-17 June 2009).

68) H. R. Ovesy, M. Kharazi, M. Taghizadeh, ”The Effects of The Bend-Twist CouplingTerms On The Buckling Behavior Of The Composite Laminates Containing EmbeddedDelaminations” , Proceedings of the Fifteenth International Conference on CompositeStructures (ICCS/15), University of Porto, Porto, Portugal, (15-17 June 2009).

67) S. G. Mousavi, H. R. Ovesy, “Effects of Nonlinearity on the Flutter Speed of HighAspect Ratio Wings” , Proceedings of the 8th Iranian Aerospace Society Conference(International), Isfahan Malek-e-Ashtar University of Technology, Iran, (17-19 Feb2009).

66) P. Khaneh Masjedi, H. R. Ovesy, “Free Vibrations of Aircraft Wings Modeled asThin-walled Composite Beam” , Proceedings of the 8th Iranian Aerospace SocietyConference (International), Isfahan Malek-e-Ashtar University of Technology, Iran, (17-19 Feb 2009).

65) H. R. Ovesy, M. H. Sherafat, S. A. M. GhannadPour, ”Higher Order Semi –Analytical Finite Strip Post Buckling Analysis of Laminated Composite Plates”,Proceedings of the Seventh International Conference on Composite Science &Technology (ICCST/7), The American University of Sharjah, UAE, (20-22 Jan. 2009).

64) M. Kharazi, H. R. Ovesy, ”Large Deflection Compressional Analysis ofUnsymmetric Delaminated Composite Plates with Consideration of ContactPhenomenon”, Proceedings of the Seventh International Conference on CompositeScience & Technology (ICCST/7), The American University of Sharjah, UAE, (20-22Jan. 2009).

63) J. Fazilati, H. R. Ovesy, ”Dynamic Instability Analysis of Composite LaminatedPlate and Cylindrical Shell Structures Using Semi-Analytical Finite Strip Method”,Proceedings of the Seventh International Conference on Composite Science &Technology (ICCST/7), The American University of Sharjah, UAE, ( 20-22 Jan. 2009).

62) H. Assaee, H. R. Ovesy, “Semi-Energy Finite Strip Post-buckling Analysis of Anti-symmetric Cross-ply Laminated plates Concerning the Effects of Mechanical Coupling” ,Proceedings of The Fifth International Conference on Thin-Walled Structures, Brisbane,Australia, (18-20 June 2008).


61) J. Fazilati, H. R. Ovesy, ”Using Finite Strip Method to Predict Dynamic InstabilityRegions (DIR) for Thin-Walled Flat Composite Plates”, Proceedings of the FirstInternational Conference on Composites: Characterization, Fabrication and Application(CCFA-1), Kish Island, Iran, (15-18 December 2008).

60) M. Kharazi, H. R. Ovesy, ”Compressional Stability Behavior of Composite Plateswith Embedded Delaminations by Using Classical Laminate Plate Theory”, Proceedingsof the First International Conference on Composites: Characterization, Fabrication andApplication (CCFA-1), Kish Island, Iran, (15-18 December 2008).

59) H. R. Ovesy, S. A. M. GhannadPour, M. H. Sherafat, ”Buckling Analysis ofLaminated Composite Plates Using Higher Order Semi – Analytical Finite StripMethod”, Proceedings of the First International Conference on Composites:Characterization, Fabrication and Application (CCFA-1), Kish Island, Iran, (15-18December 2008).

58) S. A. M. Ghannadpour, M. Hajikazemi, H. R. Ovesy, ”Large Deflection Behavior ofFunctionally Graded Plates under Pressure Loads Using First-order Shear DeformationTheory”, Proceedings of the First International Conference on Composites:Characterization, Fabrication and Application (CCFA-1), Kish Island, Iran, (15-18December 2008).

57) A. M. Sohrabi, H. R. Ovesy, G. Morada, “Post Buckling Analysis of ThickRectangular Laminates By Using Higher Order Shear Deformable Spline Finite StripMethod” , Proceedings of the 16th Annual Conference (International) of MechanicalEngineering (ISME 2008), Shahid Bahonar University of Kerman, Iran, (May 2008).

56) H. R. Ovesy, S. A. M. GhannadPour, ”The Application of an Exact Finite Strip forCalculation of Initial Post-buckling Stiffness of Channel Section Struts”, Proceedings ofthe Ninth International Conference on Computational Structures Technology, B.H.V.Topping and M. Papadrakakis (Editors), Civil-Comp Press, Athens, Greece, (2-5September 2008).

55) H. R. Ovesy, M. Kharazi, ”Compressional Stability Behavior of Composite Plateswith Multiple Through-the-Width Delaminations by Using First Order ShearDeformation Theory”, Proceedings of the Ninth International Conference onComputational Structures Technology, B.H.V. Topping and M. Papadrakakis (Editors),Civil-Comp Press, Athens, Greece, (2-5 September 2008).

54) M. Kharazi, H. R. Ovesy, “Compressional Stability Behavior of Composite Plateswith Multiple Through-the-Width Delaminations” , Proceedings of the 7th IranianAerospace Society Conference (International), Sharif University of Technology, Iran,(19-21 Feb 2008).


53) A. M. Sohrabi, H. R. Ovesy, “Free Vibration of Thick Plates Using Higher OrderFinite Strip” , Proceedings of the 7th Iranian Aerospace Society Conference(International), Sharif University of Technology, Iran, (19-21 Feb 2008).

52) J. Fazilati, H. R. Ovesy, “Free Vibration Analysis of Composite Laminated Thin-walled Cylindrical Shells Using Semi-Analytical Finite Strip Method” , Proceedings (inPersian) of the 7th Iranian Aerospace Society Conference (International), SharifUniversity of Technology, Iran, (19-21 Feb 2008).

51) H. R. Ovesy, A. M. Sohrabi, “Spline FSM Buckling Analysis of Higher Order ShearDeformable Rectangular Laminates” , Proceedings of Third Asian-Pacific Congress onComputational Mechanics (APCOM'07) and the Eleventh International Conference onthe Enhancement and Promotion of Computational Methods in Engineering and Science(EPMESC XI), Kyoto, Japan, (3-6 December 2007).

50) M. Kharazi, H. R. Ovesy, ”Postbuckling Behaviour of Composite Plates withthrough the Width Delaminations”, Proceedings of the Conference to Celebrate the Workof Prof Jim Rhodes, Dr. David Nash (Chairman), Department of MechanicalEngineering, University of Strathclyde, Glasgow, UK, (26-27 June 2007).

49) H. R. Ovesy, J. Fazilati, “Buckling Analysis of Thin-Walled Composite CylindricalShells Using Finite Strip Method (A Full Energy Approach)” , Proceedings of the 15th

Annual Conference (International) of Mechanical Engineering (ISME 2007), AmirkabirUniversity of Technology, Iran, (May 2007).

48) H. R. Ovesy, A. M. Sohrabi, “Buckling Stability Analysis of Composite LaminatedPlates Using Higher Order Spline Finite Strip” , Proceedings of the 15th AnnualConference (International) of Mechanical Engineering (ISME 2007), AmirkabirUniversity of Technology, Iran, (May 2007).

47) H. R. Ovesy, J. Loughlan, S. A. M. GhannadPour, “An Investigation On TheGeometric Non-Linear Analysis of I-Section Struts Using Finite Strip Method” ,Proceedings of the Sixth International Conference on Steel and Aluminium Structures(ICSAS'07), Oxford, England, (24-27 July 2007).

46) H. R. Ovesy, S. A. M. GhannadPour, M. N. Montazer Saheb, “Non-linear FiniteStrip Analysis of Composite Laminated Plates Under End Shortening, Using ShearDeformation Plate Theory” , Proceedings of the 6th Conference of Iranian AerospaceSociety (Aero 2007), K. N. Toosi University of Technology, Iran, (24-26 Feb 2007).

45) H. R. Ovesy, M. Kharazi, A. Sedaghati, “Analysis of the Buckling Behavior ofThrough –The-Width Delamination in Laminated Composites by Using Neural Network” ,Proceedings of the 6th Conference of Iranian Aerospace Society (Aero 2007), K. N. ToosiUniversity of Technology, Iran, (24-26 Feb 2007).


44) H. Assaee, H. R. Ovesy, “Post-Buckling Analysis of Laminated Plates Concerningthe Effects of Fiber Orientation in Layers” , Proceedings of the Sixth InternationalConference on Composite Science & Technology (ICCST/6), Durban, South Africa, (22-24 January 2007).

43) H. R. Ovesy, and J. Fazilati, “Finite Strip Buckling Analysis of Composite LaminatedThin-walled Cylindrical Shells” , Proceedings (in Persian) of the 6th Conference of IranianAerospace Society (Aero 2007), K. N. Toosi University of Technology, Iran, (24-26 Feb2007).

42) H. Hosseini-Toudeshky, B. Hamidi, B. Mohammadi, H. R. Ovesy, "Finite elementbased prediction of failure in laminated composite plates", Proceedings of the ECF16Conference, Alexandroupolis, Greece, (3-7 July 2006).

41) S. A. M. GhannadPour, H. R. Ovesy, M. Kharazi, ”Finite Strip Analysis ofFunctionally Graded Plates Under Pressure Loads”, Proceedings of the EighthInternational Conference on Computational Structures Technology, B.H.V. Topping, G.Montero and R. Montenegro (Editors), Civil-Comp Press, Las Palmas de Gran Canaria,Spain, (12-15 September 2006).

40) M. Kharazi, H. R. Ovesy, S. A. M. GhannadPour, ”The Buckling of LaminatesIncluding Bending-Twisting Coupling Effects with Multiple Delaminations Using SpringSimulation”, Proceedings of the Eighth International Conference on ComputationalStructures Technology, B.H.V. Topping, G. Montero and R. Montenegro (Editors), Civil-Comp Press, Las Palmas de Gran Canaria, Spain, (12-15 September 2006).

39) H. R. Ovesy , H. Hosseini-Toudeshky, M. Kharazi, ”Buckling Analysis of Laminateswith Multiple Through-the-width Delaminations by Using Spring Simulated Model”,Proceedings of the Third European Conference on Computational Mechanics Solids,Structures and Coupled Problems in Engineering (ECCM 2006), C.A. Mota Soares et.al.(eds.), Lisbon, Portugal, (5–8 June 2006).

38) H. R. Ovesy , S. A. M. GhannadPour, ”Large Deflection Behaviour of FunctionallyGraded Plates under Pressure Loads, Using Finite Strip Method”, Proceedings of theThird European Conference on Computational Mechanics Solids, Structures and CoupledProblems in Engineering (ECCM 2006), C.A. Mota Soares et.al. (eds.), Lisbon, Portugal,(5–8 June 2006).

37) H. R. Ovesy and S. A. M. GhannadPour, “Geometric Non-linear Finite StripAnalysis of Thin Flat Plates, Under End Shortening” , Proceedings of the 14th AnnualConference (International) of Mechanical Engineering (ISME 2006), Isfahan Universityof Technology, Iran, (May 2006).


36) A. Hadi, H. R. Ovesy and A. Shafiee, “Stiffness Analysis of Helicopter Rotor Bladein Beam and Chordwise Direction Using Empirical/Analytical Formulae” , Proceedings(in Persian) of the 14th Annual Conference (International) of Mechanical Engineering(ISME 2006), Isfahan University of Technology, Iran, (May 2006).

35) H. Hosseini-Toudeshky, B. Mohammadi, B. Hamidi, H. R. Ovesy, ”Analysis ofComposite Skin/Stiffener Debounding and Failure under Uniaxial Loading” , Proceedingsof the Thirteenth International Conference on Composite Structures (ICCS/13), MonashUniversity, Melbourne, Australia, (Nov. 2005).

34) H. R. Ovesy , S. A. M. GhannadPour, ”Geometric Nonlinear Analysis of ImperfectComposite Laminated Plates, Under End Shortening and Pressure loading, Using FiniteStrip Method” , Proceedings of the Thirteenth International Conference on CompositeStructures (ICCS/13), Monash University, Melbourne, Australia, (Nov. 2005).

33) H. R. Ovesy , S. A. M. GhannadPour, G. Morada, ”Post-buckling Behavior ofComposite Laminated Plates Under End Shortening and Pressure Loading, Using TwoVersions of Finite Strip Method” , Proceedings of the Thirteenth International Conferenceon Composite Structures (ICCS/13), Monash University, Melbourne, Australia, (Nov.2005).

32) H. R. Ovesy , A. Hadi, ” The Influence of Bend-Twist Coupling on The TorsionalResponse of Thin-Walled Box Section Composite Beam” , presented in the 4th AustralianCongress on Applied Mechanics, Melbourne, Australia, (Feb. 2005).

31) H. R. Ovesy , S. A. M. GhannadPour, ”Nonlinear Analysis of Composite laminatedplates under end-shortening using finite strip method” , presented in the 4th AustralianCongress on Applied Mechanics, Melbourne, Australia, (Feb. 2005).

30) H. R. Ovesy, H. Assaee, “An Investigation on the Post-Local Buckling Behavior ofSymmetric-Balanced Laminated Plates Using a Semi-Energy Finite Strip Approach” ,Proceedings of the Fifth International Conference on Composite Science & Technology(ICCST/5), pp. 377-382, The American University of Sharjah, UAE, (1-3 Feb. 2005).

29) H. R. Ovesy , S. A. M. GhannadPour, G. Morada,” Geometric Nonlinear Analysis ofComposite Laminated Plates with Initial Imperfection Under End Shortening, Using TwoVersions of Finite Strip Method”, Proceedings of the Fifth International Conference onComposite Science & Technology (ICCST/5), pp. 437-442, The American University ofSharjah, UAE, (1-3 Feb. 2005).

28) H. R. Ovesy , S. A. M. GhannadPour, G. Morada,” Post-buckling Analysis ofComposite Laminated Plates, Using Finite Strip Method”, Proceedings of the FifthInternational Conference on Composite Science & Technology (ICCST/5), pp. 173-178,The American University of Sharjah, UAE, (1-3 Feb. 2005).


27) H. Assaee, H. R. Ovesy, “Optimum Buckling Analysis of Some Composite ShearPanels Using the Finite Strip Approach and Genetic Algorithm Technique” , Proceedingsof the Fifth International Conference on Composite Science & Technology (ICCST/5),pp. 107-112, The American University of Sharjah, UAE, (1-3 Feb. 2005).

26) H. R. Ovesy, and H. Assaee, “Optimum Buckling Design of Composite Stiffened BoxSections Using Finite Strip Approach and Genetic Algorithm Technique” , Proceedings ofThe Fourth International Conference on Thin-Walled Structures, pp. 635-642,Loughborough University, UK, (June. 2004).

25) H. R. Ovesy, J. Loughlan and H. Assaee, “ Post-Buckling Analysis of Plates UsingThe Semi-Energy Finite Strip Approach” , Proceedings of The Fourth InternationalConference on Thin-Walled Structures, pp. 549-556, Loughborough University, UK,(June. 2004).

24) H. R. Ovesy and A. Hadi, “The Constrained Torsional Characteristics of Thin-Walled Box Section Composite Beams” Proceedings of the 5th National and 2nd

International Iranian Aerospace Society Conference, pp. 428, Aerospace ResearchInstitute, Iran, (Feb. 2004).

23) H. R. Ovesy and S. A. M. GhannadPour,” Nonlinear Analysis of Composite PlatesUnder End Shortening, Using Finite Strip Method and Classical Plate Bending Theory”Proceedings (in Persian) of the 5th National and 2nd International Iranian AerospaceSociety Conference, Aerospace Research Institute, Iran, (Feb. 2004).

22) M. H. Sadr-Lahidjani, A. Ahangari and H. R. Ovesy, “Buckling Analysis of Axi-Symmetric Shells Subjected to External Pressure Using a New Element” Proceedings (inPersian) of the 5th National and 2nd International Iranian Aerospace Society Conference,Aerospace Research Institute, Iran, (Feb. 2004).

21) H. R. Ovesy and A. Aghaee, “The Derivation and Solution of the EquationsGoverning the Aircraft Loading Actions in the Un-Symmetric Maneuvers for thePreliminary Structural Design” Proceedings (in Persian) of the 5th National and 2nd

International Iranian Aerospace Society Conference, Aerospace Research Institute, Iran,(Feb. 2004).

20) H. R. Ovesy, H. Poor-Abbasi and R. Saffar-Khozanie, “Aircraft LongitudinalLoading Analysis in the Symmetric Maneuvers due to Elevator Sinusoidal Movement”Proceedings (in Persian) of the 5th National and 2nd International Iranian AerospaceSociety Conference, Aerospace Research Institute, Iran, (Feb. 2004).

19) H. Hosseini-Toudeshky, H. R. Ovesy and M. Kharazi, “A Comprehensive Study ofComposite Panels Stiffened by Beads” , Proceedings of the Conference of ExperimentalTechniques and Design in Composite Materials 6, pp. 85, University of Padova, Italy,(18-20 June 2003).


18) H. R. Ovesy and A. Hadi, “Parametric Study of Closed Section Thin-Walled FibrousComposite Beams Subjected to Torsion” , Proceedings of the 11th Annual Conference(International) of Mechanical Engineering (ISME), pp. 417-424, Ferdowsi University ofMashhad, Iran, (May 2003).

17) H. R. Ovesy and H. Assaee, “Buckling Analysis of Composite Z-Section BeamsUnder Longitudinal Compression Using Finite Strip Method” , AIAA-2003-1987,Norfolk, VA, USA, (April 2003).

16) H. R. Ovesy and H. Assaee, “Buckling Characteristics of Some Composite StiffenedBoxes Under Longitudinal Compression or Bending Using Finite Strip Approach” ,AIAA-2003-1791, Norfolk, VA, USA, (April 2003).

15) M. H. Sadr-Lahidjani, H. R. Ovesy and Sh. Shams, “Aeroelastic and Flutter Analysisof a Flexible Wing” , AIAA-2003-1492, Norfolk, VA, USA, (April 2003).

14) H. Hosseini-Toudeshky, M. Kharazi and H. R. Ovesy, “A Simple Method to EstimateBuckling Loads of Bead Stiffened Composite Panels” , Proceedings of the 4th IASConference, Vol. 4, pp. 1-7, Amirkabir University of Technology, Iran, (Jan. 2003).

13) H. R. Ovesy and H. Assaee, “A Finite Strip Approach to Investigate the Effects ofLay-Up Properties on the Buckling Characteristics of a Composite Plate Under In-PlaneInteractive Loading” , Proceedings of the 4th IAS Conference, Vol. 4, pp. 99-104,Amirkabir University of Technology, Iran, (Jan. 2003).

12) H. R. Ovesy and A. Hadi, “Torsional Analysis of Thin-Walled Box SectionComposite Beams” , Proceedings of the 4th IAS Conference, Vol. 4, pp. 16-24, AmirkabirUniversity of Technology, Iran, (Jan. 2003).

11) M. H. Sadr-Lahidjani, H. R. Ovesy and N. Shaeri, “Finite Element Model of Piezo-Electric Material” , Proceedings (in Persian) of the 4th IAS Conference, Vol. 1, pp. 420-427, Amirkabir University of Technology, Iran, (Jan. 2003).

10) M. H. Sadr-Lahidjani, H. R. Ovesy and A. Ahangari, “A Semi-Analytical Element forthe Buckling Analysis of Axi-Symmetric Shells” , Proceedings (in Persian) of the 4th IASConference, Vol. 1, pp. 218-228, Amirkabir University of Technology, Iran, (Jan. 2003).

9) H. R. Ovesy, H. Poor-Abbasi and R. Saffar-Khozanie, “The Derivation of theDifferential Equations Governing the Aircraft Longitudinal Loading Actions in theSymmetric Maneuvers” , Proceedings (in Persian) of the 4th IAS Conference, Vol. 1, pp.115-126, Amirkabir University of Technology, Iran, (Jan. 2003).

8) H. R. Ovesy, H. Poor-Abbasi and R. Saffar-Khozanie, “Aircraft Longitudinal LoadingAnalysis in the Symmetric Maneuvers” , Proceedings (in Persian) of the 4th IASConference, Vol. 1, pp. 127-137, Amirkabir University of Technology, Iran, (Jan. 2003).


7) M. A. Koochakzadeh, H. R. Ovesy and B. Alem, “A Method on the Application of theBoundary Conditions for the Analysis of a Fuselage Using Finite Element Method” ,Proceedings (in Persian) of the 4th IAS Conference, Vol. 1, pp. 167-1176, AmirkabirUniversity of Technology, Iran, (Jan. 2003).

6) H. Hosseini-Toudeshky, H. R. Ovesy and M. Kharazi, “Buckling Behavior of StiffenedComposite Panels Containing Vertical Beads” , Proceedings of the 10th ISMEConference, pp. 553-558, K. N. Toosi University of Technology, Iran, (May 2002).

5) H. R. Ovesy and H. Assaee, “Finite Strip Buckling Analysis of Composite I-SectionBeams Subjected to Longitudinal Compression” , Proceedings of the 10th ISMEConference, pp. 481-486, K. N. Toosi University of Technology, Iran, (May 2002).

4) H. R. Ovesy and H. Assaee, “Buckling Analysis of Composite Stiffened PlateStructures due to Interaction of In-plane Compression and Shear Loading, Using FiniteStrip Method” , Proceedings of the Third Australasian Congress on Applied Mechanics,pp. 533-538, Sydney University, Australia, (Feb. 2002).

3) H. R. Ovesy and H. Assaee, “Buckling Analysis of Composite Thin-Walled StructuresUsing Finite Strip Method” , Proceedings (in Persian) of the Fifth Annual Congress ofIranian Metallurgical Engineering Society, pp. 793-801, Amirkabir University ofTechnology, Iran, (Nov. 2001).

2) H. R. Ovesy and H. Assaee, “Buckling Analysis of Some Composite Stiffened PlateStructures due to In-plane Compression and Shear Loading Using Finite Strip Method” ,Proceedings of ISME 2001, pp. 75-82, Guilan University, Iran, (May 2001).

1) H. R. Ovesy and R. Saffar-Khozanie, “Local Buckling Analysis of Isotropic PanelsSubjected to In-Plane Compressional, Shear and Bending Using Finite Strip Method”Proceedings (in Persian) of the 3rd National and 1st International IAS Conference, pp.1195-1204, Sharif Univ. of Technology, Tehran, Iran, (Jan. 2001).


SUPERVISED M.Sc. THESES (Selected):

28) Mahmoudabadi, M. R., “Finite Strip Analysis of the Dynamic Instability ofLaminated Composite Cylindrical Shells with Delaminations under Parametric HarmonicForces”, M.Sc. Thesis, Aerospace Eng. Dept., Amirkabir University of Technology, Feb.2014.

27) Amini, E., “Investigation of Effect of Ply Orientation on Delamination Behavior ofLaminated Composites under Compressive Load”, M.Sc. Thesis, Textile Eng. Dept.,Amirkabir University of Technology, Jan. 2014, (Co-supervised with Prof. A. A.Asgharian Jeddi).

26) Totounferoush, A., “Dynamic Buckling Analysis of Delaminated Composite Plateswith Piezoelectric Layers Subjected to Electro-Mechanical Loads”, M.Sc. Thesis,Aerospace Eng. Dept., Amirkabir University of Technology, Oct. 2013.

25) Yousefpoor, M., “Buckling Analysis of Composite Plates with Piezoelectric LayersUsing FSM under End-shortening and Electrical Loading”, M.Sc. Thesis, Aerospace Eng.Dept., Amirkabir University of Technology, Oct. 2013.

24) Barooti, M. M., “Stability Analysis of Symmetric Orthotropic Composite Plates withThrough-the-width Delamination”, M.Sc. Thesis, Mechanical Eng. Dept., AmirkabirUniversity of Technology, Sept. 2013, (Co-supervised with Prof. M. Mohammadi-Aghdam).

23) Chitsaz, N., “Non-Linear Buckling Analysis of Delaminated Piezoelectric CompositePlates Based on Layer-Wise Theory”, M.Sc. Thesis, Aerospace Eng. Dept., AmirkabirUniversity of Technology, June. 2013.

22) Bahrami, S., “Analysis of Laminated Cylindrical Panel (FGM) with PiezoelectricLayer Under Dynamic Loads”, M.Sc. Thesis, Mechanical Eng. Dept., AmirkabirUniversity of Technology, Feb. 2013, (Co-supervised with Prof. M. Shakeri).

21) Taherzadeh Esfahani, M., “Buckling of Initially Delaminated Composite Beams”,M.Sc. Thesis, Mechanical Eng. Dept., Amirkabir University of Technology, Sept. 2012,(Co-supervised with Prof. M. Z. Kabir)..

20) Shirmohammadali, H., “Buckling Analysis of Perforated Composite Thin Panel withthe Spline Finite Strip Method”, M.Sc. Thesis, Aerospace Eng. Dept., AmirkabirUniversity of Technology, June. 2012.

19) Zia-Dehkordi, E., “Stability Analysis of Moderately Thick Plates Using Exact FiniteStrip Solution Method”, M.Sc. Thesis, Aerospace Eng. Dept., Amirkabir University ofTechnology, Feb. 2012.


18) Nikou, A., “Full Nonlinear Aeroelastic Analysis of Highly Flexible Wings”, M.Sc.Thesis, Aerospace Eng. Dept., Amirkabir University of Technology, Feb. 2012.

17) Nassirnia, M., “Buckling and Post-buckling Analysis of FGM Plates Using FSMunder End-shortening and Thermal Loading”, M.Sc. Thesis, Aerospace Eng. Dept.,Amirkabir University of Technology, Oct. 2010.

16) Asghari Mooneghi, M., “Stability Analysis of Delaminated Composite LaminatesBased on Layerwise Theory”, M.Sc. Thesis, Aerospace Eng. Dept., Amirkabir Universityof Technology, July. 2010.

15) Javadiyeh, M., “Transient Analysis of Composite Laminated Plates by Finite StripMethod”, M.Sc. Thesis, Aerospace Eng. Dept., Amirkabir University of Technology, Jan.2010.

14) Taghizadeh, M., “Buckling and Post Buckling Behavior of Delaminated Compositeswith Higher Order Shear Deformation Theory”, M.Sc. Thesis, Aerospace Eng. Dept.,Amirkabir University of Technology, Jan. 2010.

13) Hajikazemi, M., “Post Buckling Analysis of Relatively Thick Composite Plates WithSemi Energy Finite Strip Method”, M.Sc. Thesis, Aerospace Eng. Dept., AmirkabirUniversity of Technology, Jan. 2010.

12) Mousavi, S. G., “Effects of Geometric Structural Nonlinearity on Flutter Of High-Aspect-Ratio Wings”, M.Sc. Thesis, Aerospace Eng. Dept., Amirkabir University ofTechnology, Feb. 2009.

11) Khaneh Masjedi, P., “Aeroelastic Instability of Aircraft Wings Modeled asComposite Thin-Walled Beams”, M.Sc. Thesis, Aerospace Eng. Dept., AmirkabirUniversity of Technology, Feb. 2009.

10) Sherafat, M. H., “Buckling And Post Buckling Analysis of Composite LaminatedPlates Subject To Mechanical/Thermal Loading By Using Higher Order Semi-AnalyticalFinite Strip Method”, M.Sc. Thesis, Aerospace Eng. Dept., Amirkabir University ofTechnology, Feb. 2009.

9) Sohrabi, A., “Stability Analysis Of Moderately Thick Composite Structures UsingGeneralized Finite Strip Method”, M.Sc. Thesis, Aerospace Eng. Dept., AmirkabirUniversity of Technology, May 2007.

8) Montazer-Saheb, M. H., “Nonlinear Analysis of Functionally Graded Plates UsingFinite Strip Methods”, M.Sc. Thesis, Aerospace Eng. Dept., Amirkabir University ofTechnology, April 2007.

7) Sedaghati, A., “Delamination Analysis Using Neural Networks”, M.Sc. Thesis,Aerospace Eng. Dept., Amirkabir University of Technology, April 2007.


6) Fazilati, J., “Finite Strip Buckling and Post - Buckling Analysis of CompositeShells”, M.Sc. Thesis, Aerospace Eng. Dept., Amirkabir University of Technology, Feb.2006.

5) Morada, G., “Post-Buckling Analysis of Laminated Composite Structures with theSpline Finite Strip Method”, M.Sc. Thesis, Aerospace Eng. Dept., Amirkabir Universityof Technology, Feb. 2005.

4) Ghannadpour, S. A. M., "Finite Strip Post Buckling Analysis of Composite PrismaticPlate Structures ", M.Sc. Thesis, Aerospace Eng. Dept., Amirkabir University ofTechnology, Nov. 2003.

3) Hadi, A., "Torsional Analysis of Thin-Walled Section Composite Beams", M.Sc.Thesis, Aerospace Eng. Dept., Amirkabir University of Technology, Oct. 2001.

2) Assaee, H., "Finite Strip Buckling Analysis of Composite Laminated Plates and PlateStructures", M.Sc. Thesis, Aerospace Eng. Dept., Amirkabir University of Technology,Oct. 2001.

1) Azadmanesh, A., "Stress Analysis of Helicopter Metallic Blade", M.Sc. Thesis,Aerospace Eng. Dept., Amirkabir University of Technology, Nov. 2000.

SUPERVISED Ph.D. THESES:

4) Fazilati, J., "Higher Order Finite Strip Dynamic Instability Analysis of CompositeStiffened Cylindrical Panels Having Cut-outs under Parametric In-plane Loads", Ph.D.Thesis, Dept. of Aerospace Eng., Amirkabir University of Technology, (June. 2010).

3) Kharazi, M., "Buckling and Post-buckling Analysis in Predicting the Onset of TheDelamination Growth in Laminated Composite Plates", Ph.D. Thesis, Dept. of AerospaceEng., Amirkabir University of Technology, (Feb. 2009).

2) Ghannadpour, S. A. M., "Relative Post-Buckling Stiffness Calculation of CompositePrismatic Plate Structures Using Full-Analytical Finite Strip Method", Ph.D. Thesis,Aerospace Eng. Dept., Amirkabir University of Technology, (Oct. 2008).

1) Assaee, H., "Post-Local-Buckling Analysis of Composite Thin-Walled Sections UsingSemi-Energy Finite Strip Method", Ph.D. Thesis, Aerospace Eng. Dept., AmirkabirUniversity of Technology, (Feb. 2008).

Documents

Hamid Reza Ovesy - Amirkabir University of Technologyaerospace.aut.ac.ir/autcms/res/upload/aerospace-engineering/ovesy... · Calculation of Initial Post-Buckling Stiffness of Shear-Deformable