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Monitoring Fiber Stress During Curing of Single Fiber Glass- and Graphite-Epoxy CompositesThe difference in thermal expansion characteristics of epoxy matrices and graphite fibers can produce significant residual stresses in the fibers during curing of composite materials. Tests on single fiber glass-epoxy and graphite-epoxy composite specimens were conducted in which the glass and graphite fibers were preloaded in tension, and the epoxy matrix was cast around the fibers. The fiber tension was monitored while the matrix was placed around the fiber and subjected to the temperature-time curing cycle. Two mechanisms responsible for producing stress in embedded fibers were identified as matrix thermal expansion and contraction and matrix cure shrinkage. A simple analysis based on the change in fiber tension during the curing cycle was conducted to estimate the produced stresses. Experimental results on single fiber glass- and graphite-epoxy composites show that the fiber was subjected to significant tensile stresses when the temperature was raised from the first to the second dwell period. When initial fiber pretension is about 60 percent of the fiber failure load, these curing-induced stresses can cause tensile fracture of the embedded fiber.
Document ID
19950007228
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Madhukar, Madhu S.
(Tennessee Univ. Knoxville, TN., United States)
Kosuri, Ranga P.
(Tennessee Univ. Knoxville, TN., United States)
Bowles, Kenneth J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
November 1, 1994
Subject Category
Composite Materials
Report/Patent Number
NASA-TM-4568
NAS 1.15:4568
E-8522
Report Number: NASA-TM-4568
Report Number: NAS 1.15:4568
Report Number: E-8522
Accession Number
95N13641
Funding Number(s)
PROJECT: RTOP 505-63-12
Distribution Limits
Public
Copyright
Public Use Permitted.
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