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Özel Aralık Girişi

A Multi-fidelity Aerodynamic Surrogate Model Implementation for Aeroelastic Optimization of a Nonplanar Lifting Surface
AeroBest 2021, An Eccomas Thematic Conference on Multidisciplinary Design Optimization of Aerospace Systems, Lisbon (Virtual)/PORTEKİZ, 21 Temmuz 2021
PİRLEPELİ BERKAY, NİKBAY MELİKE, KONTİS KONSTANTİNOS
Aeroelastic instability of aircraft wings modeled as thin-walled composite beams
7th Ankara International Aerospace Conference, Ankara/TÜRKİYE, 11 Eylül 2013
EKEN SEHER, KAYA METİN ORHAN
Seher Eken Tam metin bildiri
Aeroelastic Uncertainty Quantification Studies Using the S4T Wind Tunnel Model
AIAA Scitech, Dallas/AMERİKA BİRLEŞİK DEVLETLERİ, 9 Ocak 2017
NİKBAY MELİKE,HEEG JENNİFER
Aeroelastic Analysis of a Tapered Aircraft Wing
4th Ankara International Aerospace Conference, Ankara/TÜRKİYE, 10 Eylül 2007
EKEN SEHER, ÖZDEMİR ÖZGE, KAYA METİN ORHAN
Seher Eken Tam metin bildiri
Steady-state aeroelastic analysis and numerical design optimization of aircraft structures
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2009
ARDA YANANGÖNÜL
Melike Nikbay Tez Yüksek Lisans Tamamlandı
Dynamic and aeroelastic analysis of a wind turbine blade modeled as a thin-walled composite beam
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2018
SERHAT YILMAZ
Metin Orhan Kaya Tez Doktora Tamamlandı
Dynamic and aeroelastic analysis of advanced aircraft wings carrying external stores
Lisansüstü Eğitim Enstitüsü, İstanbul Teknik Üniversitesi, 2021
ALEV KAÇAR AKSONGUR
Metin Orhan Kaya Tez Doktora Tamamlandı
Aeroelastic analysis of 2 dof typical airfoil section modeled with shape memory alloy springs
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2020
OSMAN DAĞLI
Metin Orhan Kaya Tez Yüksek Lisans Tamamlandı
Structural identification and static aeroelastic optimization of ARW-2 wing with multidisciplinary code coupling
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2009
AHMET AYSAN
Melike Nikbay Tez Yüksek Lisans Tamamlandı
Flutter analysis of wing/store configurations with applications to robust aeroelastic optimization
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2012
PINAR ACAR
Melike Nikbay Tez Yüksek Lisans Tamamlandı
Dynamic and aeroelastic analysis of a helicopter blade with actively controlled trailing edge flap in forward flight
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2012
ÖZGE ÖZDEMİR ÖZGÜMÜŞ
Metin Orhan Kaya Tez Doktora Tamamlandı
Reliability based structural and aeroelastic optimization of wing models with high fidelity solvers
Bilişim Enstitüsü, İstanbul Teknik Üniversitesi, 2011
MUHAMMET NASIF KURU
Melike Nikbay Tez Yüksek Lisans Tamamlandı
Nonlinear dynamic and aeroelastic analyses of aircraft wings
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2013
SEHER DURMAZ
Metin Orhan Kaya Tez Doktora Tamamlandı
Multidisciplinary design optimization of aerospace structures with static aeroelastic criteria
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2008
LEVENT ÖNCÜ
Melike Nikbay Tez Yüksek Lisans Tamamlandı
Aeroelastic analysis of variable-span morphing wing
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2020
DAMLA DURMUŞ
Metin Orhan Kaya Tez Yüksek Lisans Tamamlandı
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
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
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
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
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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