ARAMA SONUÇLARI

Toplam 23 adet sonuçtan 20 tanesi görüntülenmektedir.

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

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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

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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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