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Toplam 13 adet sonuçtan 13 tanesi görüntülenmektedir.

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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, No. null, 2015, s. 372-383, ISSN: 0263-8231
EKEN SEHER,KAYA METİN ORHAN
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 instability of spinning launch vehicles modeled as thin-walled composite beams
ACTA MECHANICA, 2017, ISSN: 0001-5970
CİHAN MELAHAT,EKEN SEHER,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
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
Metin Orhan Kaya Özgün Makale
Active Vibration Control of Aircraft Wings Modeled as Thin-Walled Composite Beams Using Piezoelectric Actuation
ASME 2014 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers Digital Collection, MONTREAL/KANADA, 14 Kasım 2014
YILDIZ KAAN, EKEN SEHER, KAYA METİN ORHAN
Kaan Yıldız Tam metin bildiri
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
Kaan Yıldız Tam metin bildiri
Boundary Moment Control of Free Vibration 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
Kaan Yıldız 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, Ekim 2015, s. 292-296, ISSN: 1662-7482
YILDIZ KAAN, EKEN SEHER, KAYA METİN ORHAN
Kaan Yıldız Özgün Makale
DIVERGENCE AND FLUTTER STABILITY BOUNDARIES OF A ROCKET MODELED AS THIN-WALLED COMPOSITE BEAMS
9th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, 20 Eylül 2017
CİHAN MELAHAT,EKEN SEHER,KAYA METİN ORHAN
Seher Eken Özet Bildiri
Dynamic instability of spinning launch vehicles modeled as thin-walled composite beams
ACTA MECHANICA, Vol. 228, No. 12, 2017, s. 4353-4367, ISSN: 0001-5970
CİHAN MELAHAT,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
Free Vibration Analysis of Rotating Thin-Walled Composite Beams
Proceedings of 5th International Conference on Recent Advances in Space Technologies - RAST2011, ISTANBUL/TÜRKİYE, 9 Haziran 2011
EKEN SEHER,ÖZDEMİR ÖZGE,KAYA METİN ORHAN

İLETİŞİM BİLGİLERİ

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