Thin and Moderately Thick Anisotropic Cylinders under Torsion, Axial Compression and Combined Load-Reference-Cited by-同舟云学术

Thin and Moderately Thick Anisotropic Cylinders under Torsion, Axial Compression and Combined Load

Published:2013 Issue:806 Volume:79 Page:1471-1485
ISSN:0387-5008
Container-title:TRANSACTIONS OF THE JAPAN SOCIETY OF MECHANICAL ENGINEERS Series A
language:en
Short-container-title:Trans.JSME, Ser.A

Author:

TAKANO Atsushi¹

Affiliation:

1. Mitsubishi Electric Corporation, Kamakura Works

Publisher

Japan Society of Mechanical Engineers

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Link

https://www.jstage.jst.go.jp/article/kikaia/79/806/79_1471/_pdf

Reference27 articles.

1. (3) Cheng, S., and Ho, B. P. C., “Stability of Heterogeneous Aeolotropic Cylindrical Shells under Combined Loading”, AIAA Journal, Vol. 1, No. 4 (1963), pp. 892-898.

2. (4) Wong, K. F. W., and Weaver, P. M., “Approximate Solution for the Compression Buckling of Fully Anisotropic Cylindrical Shells”, AIAA Journal, Vol. 43, No. 12 (2005), pp. 2639-2645.

3. (5) Wong, K.W., Weaver, P.M. and Jones, D.P., “A Reduced Solution for Fully Anisotropic Circular Cylindrical Shells subject to Axial Compression Buckling”, 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Austin, Texas, April, (2005), pp. 18-21.

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