Identification of elastic properties of stiffened composite shell

In the present study a numerical‐experimental method for the identification of the elastic properties of stiffened composite panel from experimental vibration analysis is carried out. The elastic properties of a panel are found by an identification procedure based on the method of experiment design...

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Bibliographic Details
Main Authors: Andrejs Kovalovs, Sandris Ručevskis
Format: Article
Language:English
Published: Vilnius Gediminas Technical University 2009-12-01
Series:Aviation
Subjects:
Online Access:http://journals.vgtu.lt/index.php/Aviation/article/view/6152