The goal of the Contrails project is to help preserve and disseminate the technical record of 20th century aerospace research, highlighting in particular the research endeavors of the Illinois Tech community.

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

Report Number: AFFDL TR 68-136
Author: Khot, N. S.
Corporate Author: 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
Project: 1473
Task: 147306
AD Number: AD0680014

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Lockheed Martin Missiles & Fire Control
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