ARAMA SONUÇLARI

Toplam 42 adet sonuçtan 20 tanesi görüntülenmektedir.

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Özel Aralık Girişi

Coupled Sensitivity Analysis by Discrete-Analytical Direct and Adjoint Methods with Applications to Aeroelastic Optimization and Sonic Boom Minimization”
Boulder/AMERİKA BİRLEŞİK DEVLETLERİ, 2002, University of Colorado at Boulder
NİKBAY MELİKE
Melike Nikbay Bilimsel Kitap
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
Melike Nikbay Özgün Makale
Kanatcik Acisinin Insansiz Hava Aracinin Aeroelastik Davranisina Etkisi (Investigation of the Effect of Winglet Cant Angle on Aeroelastic Response of an Unmanned Air Vehicle)
8. Ulusal Havacilik ve Uzay Konferansi, Ankara/TÜRKİYE, 9 Eylül 2020
VERGÜN TOLGA, ÖZTÜRK ŞULE, NİKBAY MELİKE
Melike Nikbay Tam metin bildiri aeroelastisite iha
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
Melike Nikbay Özgün Makale aeroelasticity
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
Melike Nikbay Tam metin bildiri
Reliability Based Aeroelastic Optimization of a Com posite Aircraft Wing via Fluid Structure Interaction of High Fidelity Solvers
Materials Science and Engineering, Vol. 10, No. 1, 2010, s. 1-10
NİKBAY MELİKE,NECATİ FAKKUSOGLU,MUHAMMET NASİF KURU
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
Multidisciplinary Code Coupling for Analysis and Optimization of Aeroelastic Systems
AIAA Journal of Aircraft, Vol. 46, No. 6, 2009, s. 1938-1944
NİKBAY MELİKE,LEVENT ONCU,AHMET AYSAN
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
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
Melike Nikbay Tam metin bildiri Aeroelasticity
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
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
Melike Nikbay Tam metin bildiri Aeroelasticity
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
Melike Nikbay Özgün Makale
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
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
Melike Nikbay Özgün Makale
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
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
Seher Eken Tam metin bildiri
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
Seher Eken Tam metin bildiri
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
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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