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Residual stresses in angleplied laminates and their effects on laminate behaviorEvidence of the presence of lamination residual stresses in angleplied laminates were transply cracks and warpage of unsymmetric laminates which occur prior to application of any mechanical load. Lamination residual strains were measured using the embedded strain gage technique. These strains result from the temperature differences between cure and room temperature and vary linearly within this temperature range. Lamination residual stresses were usually present in angleplied fiber composites laminates; they were also present in unidirectional hybrids and superhybrids. For specific applications, the magnitudes of lamination residual stresses were determined and evaluated relative to the anticipated applied stresses. Particular attention was given to cyclic thermal loadings in applications where the thermal cycling takes place over a wide temperature range.
Document ID
19780011263
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chamis, C. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1978
Subject Category
Composite Materials
Report/Patent Number
NASA-TM-78835
Report Number: NASA-TM-78835
Meeting Information
Meeting: Intern. Conf. on Composite Mater.
Location: Toronto
Start Date: April 16, 1978
End Date: April 23, 1978
Accession Number
78N19206
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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