Beam-Column and Tie-Bar Effects in Internally Pressurized Thin Arbitrarily Laminated Cantilever Cylindrical Shells-Reference-Cited by-同舟云学术

Beam-Column and Tie-Bar Effects in Internally Pressurized Thin Arbitrarily Laminated Cantilever Cylindrical Shells

Published:2015-03 Issue:3 Volume:141 Page:04014131
ISSN:0733-9399
Container-title:Journal of Engineering Mechanics
language:en
Short-container-title:J. Eng. Mech.

Author:

Chaudhuri Reaz A.¹,Oktem A. Sinan²,Soares C. Guedes³

Affiliation:

1. Associate Professor, Dept. of Materials Science and Engineering, Univ. of Utah, Salt Lake City, UT 84112-0560 (corresponding author).

2. Assistant Professor, Dept. of Mechanical Engineering, Gebze Institute of Technology, TR-41400 Gebze Kocaeli, Turkey.

3. Professor, Centre for Marine Technology and Engineering, Instituto Superior Tecnico, Univ. of Lisbon, 1049-001 Lisbon, Portugal.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Mechanics of Materials

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29EM.1943-7889.0000763

Reference34 articles.

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2. Moderately Thick Angle-Ply Cylindrical Shells Under Internal Pressure

3. Ambartsumyan S. A. (1964). “Theory of anisotropic shells.” NASA-TT-F-118 National Aeronautics and Space Administration Washington DC.

4. Balaraman K. Kunukkasseril V. X. and Chaudhuri R. A. (1972). “Bending of asymmetrically laminated anisotropic shells subjected to internal pressure.” Proc. 1st Conf. on Reinforced Plastics and Their Aerospace Applications Vikram Sarabhai Space Centre Indian Space Research Organization Trivandrum India.

5. Cylindrical shells of bimodulus composite materials;Bert C. W.;J. Engrg. Mech. Div.,1982

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