ARAMA SONUÇLARI

Toplam 42 adet sonuçtan 20 tanesi görüntülenmektedir.

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Özel Aralık Girişi

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
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
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
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 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
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
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
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
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
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
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
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
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
Melike Nikbay Bilimsel KitapKitap Bölümü
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
Melike Nikbay Tam metin bildiri aeroelasticity
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
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
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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