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On The Influence Of Initial Geometric Imperfections On The Buckling And Postbuckling Behavior Of Fiber-Reinforced Cylindrical Shells Under Uniform Axial Compression.
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
Report number: AFFDL TR 68-136

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