On The Influence Of Initial Geometric Imperfections On The Buckling And Postbuckling Behavior Of Fiber-Reinforced Cylindrical Shells Under Uniform Axial Compression.

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Report Number: AFFDL TR 68-136
Author(s): Khot, N. S.
Corporate Author(s): Air Force Flight Dynamics Lab Wright-Patterson AFB OH
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1968-10
Pages: 68
Contract: Laboratory Research - No Contract
DoD Project: 1473
DoD Task: 147306
Identifier: AD0680014

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Provenance: Lockheed Martin Missiles & Fire Control

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