Panel buckling of stiffened shell structures with torsional stiff stringer-Reference-Cited by-同舟云学术

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Panel buckling of stiffened shell structures with torsional stiff stringer

Published:2020-12 Issue: Volume:107 Page:106257
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Krause Max^ORCID,Lyssakow Pawel,Friedrich Linus,Schröder Kai-Uwe^ORCID

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference58 articles.

1. Buckling research for imperfection tolerant fiber composite structures;Zimmermann,1996

2. Structural Design of Aerospace Vehicles III;Öry,1991

3. Towards robust design concepts for shell structures of space launch vehicles;Friedrich,2016

4. Buckling and post-buckling analysis of cracked stiffened panels via an x-Ritz method;Gulizzi;Aerosp. Sci. Technol.,2019

5. Post-buckling analysis of cracked multilayered composite plates by pb-2 Rayleigh–Ritz method;Milazzo;Compos. Struct.,2015

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