NDLI: Compression strength of composite primary structural components (Document No: 19890010228)

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Compression strength of composite primary structural components (Document No: 19890010228)

Content Provider	NASA Technical Reports Server (NTRS)
Author	Johnson, Eric R.
Copyright Year	1988
Description	The geometrically nonlinear response and failure of thin-walled structural components made from advanced composite materials is discussed. The materials involved are structural components in flight vehicle structures that are laminated from graphite-epoxy unidirectional tape. The investigation involves the buckling, postbuckling, and failure of structures subject to axial compression. The structural analysis was performed using the Structural Analysis of General Shells (STAGS) computer code. Experimental and theoretical methods are used to study the fundamental mechanisms limiting the load-carrying capacity of these components.
File Size	857345
Page Count	16
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19890010228
Archival Resource Key	ark:/13960/t3xt0m758
Language	English
Publisher Date	1988-01-01
Access Restriction	Open
Subject Keyword	Structural Mechanics Composite Materials Numerical Analysis Axial Compression Loads Thin Walled Shells Graphite-epoxy Composites Shell Stability Composite Structures Buckling Computer Programs Structural Analysis Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Technical Report

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