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

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

Title: On The Influence Of Initial Geometric Imperfections On The Buckling And Postbuckling Behavior Of Fiber-Reinforced Cylindrical Shells Under Uniform Axial Compression.
Date: 1968
Index Abstract: Not Available
Photo Quality: Not Needed
Report Number: AFFDL TR 68-136
Creator: Khot, N. S.
Corporate Author: Air Force Flight Dynamics Lab Wright-Patterson AFB OH
Laboratory: Air Force Flight Dynamics Laboratory
Extent: 68
Identifier: AD0680014; AD0680014
Access Rights: This document has been approved for public release and sale; its distribution is unlimited
Distribution Classification: 1
Contract: Laboratory Research - No Contract
DoD Project: 1473
DoD Task: 147306
DTIC Record Exists: Yes
Distribution Change Authority Correspondence: None
Report Availability: Full text available
Date Issued: 1968-10
Abstract: The abstract for this report is either unavailable or has yet to be entered
Provenance: Lockheed Martin Missiles & Fire Control
Type: report
Subject: Shells (Structural Forms); Fibers; Composite Materials; Cylindrical Bodies; Boron; Reinforcing Materials; Glass Textiles; Epoxy Resins; Buckling; Defects (Materials); Loads (Forces)
Format: 1 online resource