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Özel Aralık Girişi

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
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
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
Metin Orhan Kaya Özgün Makale
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
Metin Orhan Kaya Özgün Makale
Dynamic analysis of adaptive aircraft wings modelled as thin-walled composite beams
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2015
KAAN YILDIZ
Metin Orhan Kaya 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
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
Investigation of flow field around flapping wings
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2007
KEREM ANBARCI
Fırat Oğuz Edis Tez Yüksek Lisans Tamamlandı
Active Vibration Control Applications for Adaptive Aircraft Wings Modelled as Thin-Walled Composite Beams
AIAA-57th Structures, Structural Dynamics, and Materials Conference, San Diego-California/AMERİKA BİRLEŞİK DEVLETLERİ, 4 Ocak 2016
YILDIZ KAAN, EKEN SEHER, KAYA METİN ORHAN
Seher Eken Tam metin bildiri
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
Seher Eken Tam metin bildiri
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
Seher Eken Tam metin bildiri
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
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
Seher Eken Özgün Makale
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
Seher Eken Tam metin bildiri
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
Seher Eken Özgün Makale
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
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
Seher Eken Tam metin bildiri
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
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
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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