Experimental and numerical studies on the stability behavior of composite panels stiffened by tilting hat-stringers
Author:
Funder
National Science Foundation of China
Publisher
Elsevier BV
Subject
Civil and Structural Engineering,Ceramics and Composites
Reference17 articles.
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3. COCOMAT—improved material exploitation of composite airframe structures by accurate simulation of postbuckling and collapse;Degenhardt;Compos Struct,2006
4. The behaviour of damage tolerant hat-stiffened composite panels loaded in uniaxial compression;Falzon;Compos A Appl Sci Manuf,2001
5. Postbuckling behaviour of a blade-stiffened composite panel loaded in uniaxial compression;Falzon;Compos A Appl Sci Manuf,2000
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