Delamination during buckling of composite constructional elements

Laminated constructional elements have widespread applications in aerospace. This paper presents of the buckling for E‐Glass. Design solution based by the criteria of strength materials. The delamination of composite constructional elements is determined by the normal and shear stress. The non‐line...

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Bibliographic Details
Main Author: Antanas Žiliukas
Format: Article
Language:English
Published: Vilnius Gediminas Technical University 2010-06-01
Series:Aviation
Subjects:
Online Access:https://www.tede.vgtu.lt/index.php/Aviation/article/view/5673