Reduced-order modeling analysis of shell structures buckling using a co-rotational solid-shell element
Author:
Funder
National Natural Science Foundation of China
Fundamental Research Funds for the Central Universities of China
CALT
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference38 articles.
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2. Optimal design of composite lateral wing upper covers. Part II: Nonlinear buckling analysis;Barkanov;Aerosp. Sci. Technol.,2016
3. Nonlinear mechanical, thermal and thermo-mechanical postbuckling of imperfect eccentrically stiffened thin FGM cylindrical panels on elastic foundations;Duc;Thin-Walled Struct.,2015
4. Nonlinear thermal stability of eccentrically stiffened FGM double curved shallow shells;Quan;J. Therm. Stresses,2017
5. Isogeometric analysis of topologically complex shell structures;Kang;Finite Elem. Anal. Des.,2015
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