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Özel Aralık Girişi
The effect of sweep angle on the limit cycle oscillations of aircraft wings
ADVANCES IN AIRCRAFT AND SPACECRAFT SCIENCE, Vol. 2, No. 2, Ocak 2015, s. 199-215, ISSN: 2287-528X
EKEN SEHER, KAYA METİN ORHAN
Seher Eken Özgün Makale limit cycle oscillationssweep angleharmonic balance methodNONLINEAR AEROELASTIC ANALYSISHOMOTOPY ANALYSIS METHODINCOMPRESSIBLE-FLOWRESTORING FORCESAIRFOIL MOTIONFLUTTERBIFURCATION
Analytically Based Sensitivity Analysis and Optimization of Nonlinear Aeroelastic Systems
AIAA 8th Symposium on Multidisciplinary Analysis and Optimization, Long Beach/AMERİKA BİRLEŞİK DEVLETLERİ, 5 Eylül 2000
MAUTE KURT,NİKBAY MELİKE,FARHAT CHARBEL
Melike Nikbay Tam metin bildiri AeroelasticityOptimization
Coupled Analytical Sensitivity Analysis and Optimization ofThree Dimensional Nonlinear Aeroelastic Systems
AIAA Journal, Vol. 39, 2001, s. 2051-2061
KURT MAUTE,NİKBAY MELİKE,CHARBEL FARHAT
Melike Nikbay Özgün Makale Fluid-Structure InteractionOptimizationSensitivity Analysis
Sensitivity Analysis and Design Optimization of Three Dimensional Nonlinear Aeroelastic Systems by the Adjoint Method
International Journal for Numerical Methods in Engineering, Vol. 56, 2003, s. 911-933
NİKBAY MELİKE,KURT MAUTE,CHARBEL FARHAT
Melike Nikbay Özgün Makale sensitivityaeroelasticityadjoint

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