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
|
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
|
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
|
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
|
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 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
|
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
|
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
|
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
|
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
|
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
|
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
|
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
|
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
|
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
|
Aeroelastic Predictions for Steady and Unsteady Flow Characteristics of HIRENASD Wing
Progress in Computational Fluid Dynamics, Geneve/İSVİÇRE, Vol. 16, No. 1, Ocak 2016, s. 26-37, ISSN: 1741-5233
NİKBAY MELİKE,PİNAR ACAR
|
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
|
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
|
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
|
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
|