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