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Investigation of fatigue strength of multilayer advanced fiber compositesThe analytical characterization of a multilayer fiber composite plate (without hole) was accomplished for both static and dynamic loading conditions using the finite difference technique. Thornel 300/5208 composites with and without holes were subjected to static and tensile fatigue testing. Five (5) fiber orientations were submitted to test. Tensile fatigue testing also included three (3) loading conditions and two (2) frequencies. The low-cycle test specimens demonstrated a shorter tensile fatigue life than the high-cycle test specimens. Failure surfaces demonstrated effect of testing conditions. Secondary failure mechanisms, such as: delamination, fiber breakage, and edge fiber delamination were present. Longitudinal delamination between plies also occurred in these specimens.
Document ID
19750011296
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Thornton, H. R.
(Texas A&M Univ. College Station, TX, United States)
Kozik, T. J.
(Texas A&M Univ. College Station, TX, United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1974
Subject Category
Composite Materials
Report/Patent Number
NASA-CR-134691
TEES-2992-74-002
Report Number: NASA-CR-134691
Report Number: TEES-2992-74-002
Accession Number
75N19368
Funding Number(s)
CONTRACT_GRANT: NGR-44-001-149
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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