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Composite materials: Fatigue and fracture. Vol. 3The present volume discusses topics in the fields of matrix cracking and delamination, interlaminar fracture toughness, delamination analysis, strength and impact characteristics, and fatigue and fracture behavior. Attention is given to cooling rate effects in carbon-reinforced PEEK, the effect of porosity on flange-web corner strength, mode II delamination in toughened composites, the combined effect of matrix cracking and free edge delamination, and a 3D stress analysis of plain weave composites. Also discussed are the compression behavior of composites, damage-based notched-strength modeling, fatigue failure processes in aligned carbon-epoxy laminates, and the thermomechanical fatigue of a quasi-isotropic metal-matrix composite.
Document ID
19920056377
Acquisition Source
Legacy CDMS
Document Type
Book
Authors
O'Brien, T. K.
(U.S. Army, Aerostructures Directorate; NASA, Langley Research Center Hampton, VA, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1991
Publication Information
ISBN: 0-8031-1419-2
Subject Category
Structural Mechanics
Report/Patent Number
ASTM STP-1110
Accession Number
92A39001
Distribution Limits
Public
Copyright
Other

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