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Micromechanics of composite laminate compression failureThe Dugdale analysis for metals loaded in tension was adapted to model the failure of notched composite laminates loaded in compression. Compression testing details, MTS alignment verification, and equipment needs were resolved. Thus far, only 2 ductile material systems, HST7 and F155, were selected for study. A Wild M8 Zoom Stereomicroscope and necessary attachments for video taping and 35 mm pictures were purchased. Currently, this compression test system is fully operational. A specimen is loaded in compression, and load vs shear-crippling zone size is monitored and recorded. Data from initial compression tests indicate that the Dugdale model does not accurately predict the load vs damage zone size relationship of notched composite specimens loaded in compression.
Document ID
19870017544
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Guynn, E. Gail
(Texas A&M Univ. College Station, TX, United States)
Bradley, Walter L.
(Texas A&M Univ. College Station, TX, United States)
Date Acquired
September 5, 2013
Publication Date
November 15, 1986
Subject Category
Composite Materials
Report/Patent Number
NAS 1.26:180348
NASA-CR-180348
Report Number: NAS 1.26:180348
Report Number: NASA-CR-180348
Accession Number
87N26977
Funding Number(s)
CONTRACT_GRANT: NAG1-659
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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