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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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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Dynamic instability of spinning launch vehicles modeled as thin-walled composite beams
ACTA MECHANICA, 2017, ISSN: 0001-5970
CİHAN MELAHAT,EKEN SEHER,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 analysis of adaptive aircraft wings modelled as thin-walled composite beams
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2015
KAAN YILDIZ
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DIVERGENCE AND FLUTTER STABILITY BOUNDARIES OF A ROCKET MODELED AS THIN-WALLED COMPOSITE BEAMS
9th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Ankara/TÜRKİYE, 20 Eylül 2017
CİHAN MELAHAT, EKEN SEHER, KAYA METİN ORHAN
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Effect of the Transverse Shear Deformation on the Free Vibration of Rotating Blades Modeled as Thin Walled Composite Beams
Applied Mechanics and Materials, Ekim 2015
YILMAZ SERHAT,SEHER EKEN,KAYA METİN ORHAN
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Vibration Analysis Of Rotating Thin-Walled Composite Beams Via Finite Element Method
IFASD 2011, 15th International Forum on Aeroelasticity and Structural Dynamics, Paris/FRANSA, 26 Haziran 2011
ÖZDEMİR ÖZGE, 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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Dynamic instability of spinning launch vehicles modeled as thin-walled composite beams
ACTA MECHANICA, Vol. 228, No. 12, Aralık 2017, s. 4353-4367, ISSN: 0001-5970
CİHAN MELAHAT, 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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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
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Geometrically nonlinear vibration analysis of thin-walled composite beams
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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Effect of the Transverse Shear Deformation on the Free Vibration of Rotating Blades Modeled as Thin-Walled Composite Beams
Applied Mechanics and Materials, Vol. 798, Ocak 2015, s. 119-124, ISSN: 1660-9336
YILMAZ SERHAT, EKEN SEHER, 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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Free Vibration Analysis Of Rotating Thin-Walled Composite Beams
RAST 2011, 5th International Conference on Recent Advances in Space Technologies, istanbul/TÜRKİYE, 9 Haziran 2011
EKEN SEHER, ÖZDEMİR ÖZGE, KAYA METİN ORHAN
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DIVERGENCE AND FLUTTER STABILITY BOUNDARIES OF A ROCKET MODELED AS THIN-WALLED COMPOSITE BEAMS
9th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Ankara/TÜRKİYE, 20 Eylül 2017
CİHAN MELAHAT, 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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Active Vibration Control Applications for Adaptive Aircraft Wings Modelled as Thin-Walled Composite Beams
57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, San Diego, California, USA/AMERİKA BİRLEŞİK DEVLETLERİ, 4 Ocak 2016
YILDIZ KAAN,EKEN SEHER,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, Ekim 2015, s. 292-296, ISSN: 1662-7482
YILDIZ KAAN, EKEN SEHER, KAYA METİN ORHAN
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