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Accession Number:
ADA063796
Title:
Representation of Matrix/Interface-Controlled Strength of Unidirectional Composites.
Corporate Author:
AIR FORCE MATERIALS LAB WRIGHT-PATTERSON AFB OHIO
Report Date:
1978-08-01
Abstract:
The report presents a method of characterizing the matrixinterface-controlled strength, including scatter, of unidirectional composites under combined loading. The failure envelope is represented by a second order polynomial and the scatter is described by the strength vector whose magnitude has a Weibull distriubtion. The method is based on the assumption of failure originating at inherent cracks parallel to the fibers and holds promise as a means of accounting for the size effect under combined loading. In addition, the energy release rate approach is discussed as a physical model and the appropriate data are presented. Author
Descriptive Note:
Final rept. 1 May 76-31 Dec 77,
Pages:
0038
File Size:
11.08MB