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
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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
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Aeroelastic Analysis of a Tapered Aircraft Wing
4th Ankara International Aerospace Conference, Ankara/TÜRKİYE, 10 Eylül 2007
EKEN SEHER, ÖZDEMİR ÖZGE, KAYA METİN ORHAN
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Aeroelastic Uncertainty Quantification Studies Using the S4T Wind Tunnel Model
AIAA Scitech, Dallas/AMERİKA BİRLEŞİK DEVLETLERİ, 9 Ocak 2017
NİKBAY MELİKE,HEEG JENNİFER
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Multidisciplinary design optimization of aerospace structures with static aeroelastic criteria
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2008
LEVENT ÖNCÜ
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Structural identification and static aeroelastic optimization of ARW-2 wing with multidisciplinary code coupling
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2009
AHMET AYSAN
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Steady-state aeroelastic analysis and numerical design optimization of aircraft structures
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2009
ARDA YANANGÖNÜL
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Flutter analysis of wing/store configurations with applications to robust aeroelastic optimization
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2012
PINAR ACAR
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Reliability based structural and aeroelastic optimization of wing models with high fidelity solvers
Bilişim Enstitüsü, İstanbul Teknik Üniversitesi, 2011
MUHAMMET NASIF KURU
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Dynamic and aeroelastic analysis of advanced aircraft wings carrying external stores
Lisansüstü Eğitim Enstitüsü, İstanbul Teknik Üniversitesi, 2021
ALEV KAÇAR AKSONGUR
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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
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Nonlinear dynamic and aeroelastic analyses of aircraft wings
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2013
SEHER DURMAZ
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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
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Aeroelastic analysis of 2 dof typical airfoil section modeled with shape memory alloy springs
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2020
OSMAN DAĞLI
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Aeroelastic analysis of variable-span morphing wing
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2020
DAMLA DURMUŞ
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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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Uncertainty Quantification of Aeroelastic Systems Using Active Learning Gaussian Process
AeroBest 2021 - ECCOMAS Thematic Conference on Multidisciplinary Design Optimization of Aerospace Systems, 21 Temmuz 2021
YILDIZ ŞIHMEHMET, ÇAKMAK ENES, KARA EMRE, NİKBAY MELİKE
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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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