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Fiber composite structural durability and damage tolerance: Simplified predictive methodsSimplified predictive methods and models (theory) to evaluate fiber/polymer-matrix composite material for determining structural durability and damage tolerance are presented and described. This theory includes equations for (1) fatigue and fracture of composites without and with defects, (2) impact resistance and residual strength after impact, (3) thermal fatigue, and (4) combined stress fatigue. Several examples are included to illustrate applications of the theory and to identify significant parameters and sensitivities. Comparisons with limited experimental data are made.
Document ID
19880004027
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chamis, Christos C.
(NASA Lewis Research Center Cleveland, OH, United States)
Ginty, Carol A.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1987
Subject Category
Composite Materials
Report/Patent Number
E-3755
NASA-TM-100179
NAS 1.15:100179
Report Number: E-3755
Report Number: NASA-TM-100179
Report Number: NAS 1.15:100179
Accession Number
88N13409
Funding Number(s)
PROJECT: RTOP 505-63-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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