Force Measurement and Load Estimation Studies at ITU forFlexible Flapping Wings and Maneuvering Wings under Gust
International Workshop on Non-Intrusive Optical Flow Diagnostics, 25 Ekim 2016
SON ONUR,ZALOĞLU BERK,PERÇİN MUSTAFA,ÇETİNER YILDIRIM NURİYE LEMAN OKŞAN
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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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The effect of sweep angle on the limit cycle oscillations of aircraft wings
ADVANCES IN AIRCRAFT AND SPACECRAFT SCIENCE, Nisan 2015
SEHER EKEN,KAYA METİN ORHAN
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Optimal Control Procedure Application for Dynamic Response of Adaptive Aircraft Wings Modeled as Thin Walled Composite Beams
Applied Mechanics and Materials, Ekim 2015
KAAN YILDIZ,SEHER EKEN,KAYA METİN ORHAN
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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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Nonlinear dynamic and aeroelastic analyses of aircraft wings
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2013
SEHER DURMAZ
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Dynamic analysis of adaptive aircraft wings modelled as thin-walled composite beams
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2015
KAAN YILDIZ
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Investigation of flow field around flapping wings
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2007
KEREM ANBARCI
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Introduction to the Virtual Collection: Unsteady Aerodynamic Response of Rigid Wings in Large-Amplitude Gust Encounters
AIAA JOURNAL, Vol. 59, No. 3, Mart 2021, s. 764-764, ISSN: 1748-717X
JONES ANYA R., ÇETİNER YILDIRIM NURİYE LEMAN OKŞAN
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Overview of NATO AVT-282: Unsteady Aerodynamic Response of Rigid Wings in Gust Encounters
AIAA Scitech 2020 Forum, Orlando, Florida/AMERİKA BİRLEŞİK DEVLETLERİ, 6 Ocak 2020
JONES ANYA R., ÇETİNER YILDIRIM NURİYE LEMAN OKŞAN
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Overview of Unsteady Aerodynamic Response of Rigid Wings in Gust Encounters
AIAA JOURNAL, Vol. 59, No. 2, Şubat 2021, s. 731-736, ISSN: 1748-717X
JONES ANYA R., ÇETİNER YILDIRIM NURİYE LEMAN OKŞAN
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Limit Cycle Oscillations of Swept-back Wings In an Incompressible Flow
53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, 23 Nisan 2012
EKEN SEHER, KAYA METİN ORHAN
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Limit Cycle Oscillations Of Swept-Back Wings in an incompressible Flow
AIAA-53rd Structures, Structural Dynamics, and Materials Conference, Honolulu-Hawaii/AMERİKA BİRLEŞİK DEVLETLERİ, 23 Nisan 2012
EKEN SEHER, KAYA METİN ORHAN
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Active vibration control of aircraft wings modeled as thin-walled composite beams using piezoelectric actuation
ASME-IMECE-2014, International Mechanical Engineering Congress & Exposition, Montreal/KANADA, 14 Kasım 2014
YILDIZ KAAN, EKEN SEHER, KAYA METİN ORHAN
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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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Approximate Analytical Solutions Of Nonlinear Flutter Of Aircraft Wings
IFASD 2011, 15th International Forum on Aeroelasticity and Structural Dynamics, Paris/FRANSA, 26 Haziran 2011
EKEN SEHER, KERKİ TİLBE, KAYA METİN ORHAN
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Optimal Control Procedure Application for Dynamic Response of Adaptive Aircraft Wings Modeled as Thin-Walled Composite Beams
Applied Mechanics and Materials, Vol. 798, Ocak 2015, s. 292-296, ISSN: 1660-9336
YILDIZ KAAN, 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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Boundary Moment Control of Free Vıbratıon of Adaptive Aircraft Wings Modeled as Thin-Walled Composite Beams
8th Ankara International Aerospace Conference, ankara/TÜRKİYE, 10 Eylül 2015
YILDIZ KAAN, EKEN SEHER, KAYA METİN ORHAN
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Free vibration analysis of composite aircraft wings modeled as thin-walled beams with NACA airfoil sections
Thin-Walled Structures, Vol. 139, Haziran 2019, s. 362-371, ISSN: 0263-8231
EKEN SEHER
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