Buckling of axially compressed CFRP truncated cones with additional lateral load: Experimental and numerical investigation-Reference-Cited by-同舟云学术

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Buckling of axially compressed CFRP truncated cones with additional lateral load: Experimental and numerical investigation

Published:2016-12 Issue: Volume:157 Page:436-447
ISSN:0263-8223
Container-title:Composite Structures
language:en
Short-container-title:Composite Structures

Author:

Khakimova Regina,Zimmermann Rolf,Wilckens Dirk,Rohwer Klaus,Degenhardt Richard

Funder

Seventh Framework Programme

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference39 articles.

1. NASA SP-8007 – buckling of thin-walled circular cylinders;Weingarten;NASA Space Veh Des Criteria Struct,1965

2. Weingarten VI, Seide P. NASA SP-8019 – buckling of thin-walled truncated cones; 1968.

3. The NASA monographs on shell stability. Design recommendations;Nemeth,1998

4. Shell buckling design criteria based on manufacturing imperfection signatures;Hiburger;AIAA J,2006

5. DESICOS, [Online]. Available: http://www.desicos.eu.

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3. Predictive capabilities of Vibration-Correlation Technique applied to axially compressed CFRP truncated cones;Composites Part B: Engineering;2022-07

4. Buckling of launch-vehicle cylinders under axial compression: A comparison of experimental and numerical knockdown factors;Thin-Walled Structures;2020-10

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