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Özel Aralık Girişi
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
Seher Eken Özgün Makale Flexural-torsional coupled frequencyThin-walled composite beamsTransverse shearFree warping modelWarping restraint modelCOMPOSITE BOX-BEAMSAEROELASTIC INSTABILITYINCOMPRESSIBLE-FLOWWINGSBEHAVIOR
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
Seher Eken Özgün Makale limit cycle oscillationssweep angleharmonic balance methodNONLINEAR AEROELASTIC ANALYSISHOMOTOPY ANALYSIS METHODINCOMPRESSIBLE-FLOWRESTORING FORCESAIRFOIL MOTIONFLUTTERBIFURCATION
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
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
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
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
Nuriye Leman Okşan Çetiner Yıldırım Vaka Takdimi
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
Nuriye Leman Okşan Çetiner Yıldırım Özgün Makale
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
Nuriye Leman Okşan Çetiner Yıldırım Tam metin bildiri
Free Surface Effects on 2 D Airfoils and 3 D Wings Moving Over Water
Ocean Systems Engineering, An International Journal, Vol. 6, No. 3, Eylül 2016, s. 245-264
BAL ŞAKİR
Şakir Bal Özgün Makale
Optimal Control Procedure Application for Dynamic Response of Adaptive Aircraft Wings Modeled as Thin-Walled Composite Beams
Applied Mechanics and Materials, Vol. 798, Ekim 2015, s. 292-296, ISSN: 1662-7482
YILDIZ KAAN, EKEN SEHER, KAYA METİN ORHAN
Kaan Yıldız Özgün Makale

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