Published September 1977 | Version v1
Report Restricted

Analytical and experimental studies of graphite-epoxy and boron-epoxy angle-ply laminates in compression

Description

The applicability and adequacy of several computer techniques in predicting satisfactorily the nonlinear/inelastic response of angle-ply laminates were evaluated. The analytical predictions were correlated with the results of a test program on the inelastic response under axial compression of a large variety of graphite-epoxy and boron-epoxy angle-ply laminates. These comparison studies indicate that neither of the above-mentioned analyses can satisfactorily predict either the mode of response or the ultimate stress value corresponding to a particular angle-ply laminate configuration. Consequently, also the simple failure mechanisms assumed in the analytical models were not verified

Availability note (English)

MF available from INIS under the Report Number; Available from NTIS. PC A04/MF A01.

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Additional details

Publishing Information

Imprint Pagination
66 p.
Report number
N--78-16102

INIS

Country of Publication
United States
Country of Input or Organization
United States
INIS RN
10436785
Subject category
S36: MATERIALS SCIENCE;
Descriptors DEI
BORON; COMPOSITE MATERIALS; COMPRESSION STRENGTH; COMPUTER CALCULATIONS; EPOXIDES; FAILURES; MATHEMATICAL MODELS; NONLINEAR PROBLEMS; SIMULATION; STRESS ANALYSIS; STRESSES
Descriptors DEC
ELEMENTS; MECHANICAL PROPERTIES; ORGANIC COMPOUNDS; ORGANIC OXYGEN COMPOUNDS; SEMIMETALS

Optional Information

Secondary number(s)
NASA-CR--145234.