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

Item

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