Calculation of the collapse load of an axially compressed laminated composite stringer-stiffened curved panel–An engineering approach-Reference-Cited by-同舟云学术

Calculation of the collapse load of an axially compressed laminated composite stringer-stiffened curved panel–An engineering approach

Published:2008-06 Issue:4 Volume:83 Page:341-353
ISSN:0263-8223
Container-title:Composite Structures
language:en
Short-container-title:Composite Structures

Author:

Pevzner P.,Abramovich H.,Weller T.

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference21 articles.

1. The strength of thin plates in compression;von Kármán;ASME Appl Mech Trans,1932

2. Sechler EE. The ultimate strength of flat sheets in compression, GALCIT Publication 27, Guggenheim Aeronautics Laboratory, California Institute of Technology, Pasadena; 1933.

3. Cox HL. Buckling of thin plates in compression, Aeronautical Research Committee, R.&M. No. 1554; 1933.

4. Versuche zur Ermittlung der mittragenden Breite von verbeulten Blechen;Lahde-Wagner;Luftfahrt-Forchung,1936

5. Stress distribution in stiffened panels under compression;Sechler;J Aeronaut Sci,1937

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