Arbitrarily laminated, anisotropic cylindrical shell under internal pressure-Reference-Cited by-同舟云学术

Arbitrarily laminated, anisotropic cylindrical shell under internal pressure

Published:1986-11 Issue:11 Volume:24 Page:1851-1858
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Chaudhuri Reaz A.¹,Balaramant K.²,Kunukkasseril Vincent X.²

Affiliation:

1. University of Utah, Salt Lake City, Utah

2. Indian Institute of Technology, Madras, India

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.9534

Reference19 articles.

1. Composite Material Mechanics: Structural Mechanics

2. Composite Materials;Bert C. W.,1974

3. 4Chaudhuri, R. A. "Static Analysis of Fiber Reinforced Laminated Plates and Shells with Shear Deformation Using Quadratic Triangular Elements," Ph.D. Dissertation,Dept. of Civil Engineering, Universityof Southern California, Los Angeles,1983.

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