Experimental and Numerical Investigation on the Influence of the Internal Caldding Layer in Single Hat-Stiffened Composite Panels Under Axial Compressive Load
Author:
Affiliation:
1. National Key Laboratory of Strength and Structural Integrity,Xi'an,China,710065
2. Shanghai polytechnic University,Shanghai,China,201209
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10490442/10490456/10490516.pdf?arnumber=10490516
Reference15 articles.
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2. Stiffener debonding mechanisms in post-buckled CFRP aerospace panels
3. A post-buckling compressive failure analysis framework for composite stiffened panels considering intra-, inter-laminar damage and stiffener debonding
4. Inigo Ortiz de Zarate Alberdi;Orifici;Compression and post-buckling damage growth and collapse analysis of flat composite stiffened panels. Composites Science and Technology,2008
5. Post-buckling behaviour of flat stiffened composite panels: Experiments vs. analysis
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