The Axial Compressive Response of Thin, Elastic, Polygonal Shells

Author:

Tiwari Vishwa Mohan12,D’Mello Royan J.2,Vijayachandran Avinkrishnan Ambika2,Waas Anthony M.2

Affiliation:

1. University of Michigan–Ann Arbor Department of Aerospace Engineering, , Ann Arbor, MI 48109

2. University of Michigan Department of Aerospace Engineering, , Ann Arbor, MI 48109

Abstract

Abstract Thin-walled cylindrical shell structures are revisited with the objective of increasing the axial load-carrying capacity. By using the postbuckling reserve of rectangular plates, polygonal shells are studied, which combines the response of a plate-like structure with a shell-like structure. These “plate-shells” are shown to be imperfection insensitive for a range of polygonal shell designs. Furthermore, their collapse load exceeds the corresponding load for a circular cylindrical shell. These results are a significant departure from the well-known imperfection sensitivity in the axial compressive response of cylindrical shells.

Publisher

ASME International

Reference38 articles.

1. The Buckling of Spherical Shells by External Pressure;Von Karman;J. Aeronaut. Sci.,1939

2. Thompson, J. , 1961, “The Elastic Stability of Spherical Shells,” Ph.D. dissertation, Cambridge University.

3. Imperfection Sensitivity of Externally Pressurized Spherical Shells;Hutchinson;ASME J. Appl. Mech.,1967

4. Buckling of Bars, Plates, and Shells

5. Buckling Experiments: Experimental Methods in Buckling of Thin-Walled Structures

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