Critical buckling load of curved sandwich beams with composite skins subjected to uniform pressure load-Reference-Cited by-同舟云学术

Critical buckling load of curved sandwich beams with composite skins subjected to uniform pressure load

Published:2015-10-13 Issue:6 Volume:38 Page:1805-1816
ISSN:1678-5878
Container-title:Journal of the Brazilian Society of Mechanical Sciences and Engineering
language:en
Short-container-title:J Braz. Soc. Mech. Sci. Eng.

Author:

Poortabib A.

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,General Engineering,Aerospace Engineering,Automotive Engineering,Industrial and Manufacturing Engineering,Applied Mathematics

Link

http://link.springer.com/content/pdf/10.1007/s40430-015-0435-0.pdf

Reference24 articles.

1. Lönnö A (1998) “Experiences from using carbon fiber composites/sandwich construction” in the Swedish navy. In: Olsson KA (eds) Sandwich construction 4. Emacks Publishing

2. Ogorkiewicz RM, Sayigh AAM (1973) Deflection of carbon fiber/acrylic foam sandwich beams. Composite. pp 254–257

3. Bulson PS (1970) The stability of flat plates. Cbatto and Windus, London

4. Brush DO, Almroth BO (1975) Buckling of bars, plates and shells. McGraw-Hill, New York

5. Hunt GE, Da Silva LS (1990) Interaction bending behavior of sandwich beams. J Appl Mech Trans ASME 57(1):189–196

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