ARAMA SONUÇLARI

Toplam 23 adet sonuçtan 20 tanesi görüntülenmektedir.

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

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

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