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Composite laminate warpageSet of simplified equations predicts warpage that often occurs upon removal from fabrication mold. Equations predict corner deflection and are based upon micromechanics and macromechanics of composites, as well as laminate theory. Factors considered include ply misorientation, fiber migration, and void/volume ratio nonuniformity.
Document ID
19760000355
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Chamis, C. C.
Date Acquired
August 8, 2013
Publication Date
January 1, 1977
Publication Information
Publication: NASA Tech Briefs
Volume: 1
Issue: 3
ISSN: 0145-319X
Subject Category
Materials
Report/Patent Number
LEW-12615
Accession Number
76B10355
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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