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
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Reduced Order Modelling of Static and Dynamic Aeroelastic Predictions withMultidisciplinary Approach
CEAS Aeronautical Journal / Springer, Vol. 6, No. 3, 2015, s. 455-469, ISSN: 1869-5582
NİKBAY MELİKE,PİNAR ACAR
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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
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Flutter based aeroelastic optimization of an aircraft wing with analytical approach
53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, 23 Nisan 2012
NİKBAY MELİKE,ACAR PİNAR
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Reliability Based Multidisciplinary Optimization of Aeroelastic Systemswith Structural and Aerodynamic Uncertainties
AIAA Journal of Aircraft, Vol. 50, No. 3, 2013, s. 798-715, ISSN: 0021-8669
NİKBAY MELİKE,MUHAMMET NASİF KURU
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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
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Reliability based aeroelastic optimization of a composite aircraft wing via fluid structure interaction of high fidelity solvers
IOP Conference Series: Materials Science and Engineering, Vol. 10, No. 1, Temmuz 2010, s. 12037, ISSN: 1757-899X
NİKBAY MELİKE,NECATİ FAKKUSOGLU,MUHAMMED NASİF KURU
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A Multidisiplinary Code Coupling Approach for Analysis and Optimization of Aeroelastic Systems
12th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, Victoria/KANADA, 10 Eylül 2008
NİKBAY MELİKE,ONCU LEVENT,AYSAN AHMET
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Conceptual layout of aeroelastic wing structures by topology optimization
43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Denver/AMERİKA BİRLEŞİK DEVLETLERİ, 22 Nisan 2002
MAUTE KURT,NİKBAY MELİKE,FARHAT CHARBEL
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Impact of Aeroelastic Uncertainties on Sonic Boom Signature of a Commercial Supersonic Transport Configuration
AIAA Scitech Forum, Dallas/AMERİKA BİRLEŞİK DEVLETLERİ, 9 Ocak 2017
NİKBAY MELİKE,STANFORD BRET,WEST TOM,RALLABHANDİ SRİRAM
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Steady and Unsteady Aeroelastic Computations of HIRENASD Wing for Low and High Reynolds Numbers
54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 8 Nisan 2013
ACAR PİNAR,NİKBAY MELİKE
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Integrating Analytical Aeroelastic Instability Analysis into Design Optimiza tion of Aircraft Wing Structures
TWMS Journal of Applied and Engineering Mathematics, Vol. 1, No. 2, 2011, s. 237-253
NİKBAY MELİKE,PİNAR ACAR
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Euler Solver Based Aeroelastic Predictions for Steady and UnsteadyFlow Characteristics of HIRENASD Wing NATO STO AVT 203 Joined Exercise on Aeroelastic Prediction
Paris/FRANSA, 2017, s. 131-150, NATO Science and Technology Organization
NİKBAY MELİKE,PİNAR ACAR,ZANG ZHİCHAO
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Robust Aeroelastic Design Optimization of Wing Store Configurations Based on Flutter Criteria
14th AIAA/ISSMO Multidisciplinary Analysis and Optimization (MAO) Conference, Indianapolis/AMERİKA BİRLEŞİK DEVLETLERİ, 17 Eylül 2012
NİKBAY MELİKE,PİNAR ACAR
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Multidisciplinary Uncertainty Quantification in Aeroelastic Analyses of Semi Span Supersonic Transport Wing
AIAA Aviation and Aeronautics Forum and Exposition, 22 Haziran 2015
NİKBAY MELİKE,PİNAR ACAR
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Uncertainty Quantification of Aeroelastic Systems Using an Active Learning Gaussian Process
AeroBest 2021, An Eccomas Thematic Conference on Multidisciplinary Design Optimization of Aerospace Systems, Lisbon (Virtual)/PORTEKİZ, 21 Temmuz 2021
YILDIZ ŞIHMEHMET, ÇAKMAK ENES, KARA EMRE, NİKBAY MELİKE
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AEROELASTIC RESPONSE OF AN AIRCRAFT WING MODELED AS A THIN-WALLED COMPOSITE BEAM
ASME-IMECE2013, International Mechanical Engineering Congress & Exposition, San Diego-California/AMERİKA BİRLEŞİK DEVLETLERİ, 14 Kasım 2013
EKEN SEHER, KAYA METİN ORHAN
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Dynamic and Aeroelastic Analyses of a Wind Turbine Blade Modeled as a Thin-Walled Composite Beam
ASME-IMECE2014, International Mechanical Engineering Congress & Exposition, Montreal/KANADA, 14 Kasım 2014
YILMAZ SERHAT, EKEN SEHER, KAYA METİN ORHAN
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Flexural-torsional coupled vibration of anisotropic thin-walled beams with biconvex cross-section
THIN-WALLED STRUCTURES, Vol. 94, Ocak 2015, s. 372-383, ISSN: 0263-8231
EKEN SEHER, KAYA METİN ORHAN
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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
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