Free flexural (or bending) vibrations analysis of certain groups of stiffened composite plates or panels-In flight vehicle structures


Thesis Type: Postgraduate

Institution Of The Thesis: Orta Doğu Teknik Üniversitesi, Faculty of Engineering, Department of Aerospace Engineering, Turkey

Approval Date: 2009

Student: JABER JAVANSHİR HASBESTAN

Supervisor: SİNAN EYİ