Non-linear buckling analysis of delaminated hat-stringer panels using variational asymptotic method-Reference-Cited by-同舟云学术

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Non-linear buckling analysis of delaminated hat-stringer panels using variational asymptotic method

Published:2024-10 Issue: Volume:345 Page:118276
ISSN:0263-8223
Container-title:Composite Structures
language:en
Short-container-title:Composite Structures

Author:

Kumar A. Phanendra^ORCID,Méndez Javier Paz^ORCID,Burela Ramesh Gupta,Bisagni Chiara,Harursampath Dineshkumar,Ponnusami Sathiskumar Anusuya^ORCID

Publisher

Elsevier BV

Reference45 articles.

1. POSICOSS—improved post-buckling simulation for design of fibre composite stiffened fuselage structures;Zimmermann;Compos Struct,2006

2. Experiment and analysis of hat-stringer-stiffened composite curved panels under axial compression;Mo;Compos Struct,2015

3. Analytical and experimental investigation of transverse loading on grid stiffened composite panels;Ahmadi;Composites B,2019

4. Compressive buckling and post-buckling behaviors of J-type composite stiffened panel before and after impact load;Wu;Compos Struct,2023

5. On the use of selective stitching in stiffened composite panels to prevent skin-stringer debonding;Riccio;Composites B,2017

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