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High strain rate properties of angle-ply composite laminates, part 3Angle-ply graphite/epoxy and graphite/S-glass/epoxy laminates were characterized in uniaxial tension at strain rates ranging from quasi-static to over 500 s(sup -1). Laminate ring specimens of +/-15(sub 2s), +/-22.5(sub 2s), +/-30(sub 2s), +/-45(sub 2s), +/-60(sub 2s), +/-67.5(sub 2s), and +/-75(sub 2s) degree layups were loaded under internal pressure. Results were presented in the form of stress-strain curves to failure. Properties determined included moduli, Poisson's ratios, strength, and ultimate strain. In all seven laminates for the two materials tested the modulus and strength increase with strain rate. The effect of strain rate varies with layup, being lowest for the fiber dominated +/-15(sub 2s) degree laminates and highest for the matrix dominated +/-75(sub 2s) degree laminates. The highest increments over the static values are 10 to 25 percent for the +/-15(sub 2s) degree layup and 200 to 275 percent for the +/-75(sub 2s) degree layup. Ultimate strains do not show any significant trends with strain rate. In almost all cases the ultimate strain values are within +/-20 percent of the mean value and in half of the cases the deviation from the mean are less than 10 percent.
Document ID
19920011638
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Daniel, I. M.
(IIT Research Inst. Chicago, IL, United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1991
Subject Category
Composite Materials
Report/Patent Number
NASA-CR-189085
NAS 1.26:189085
Report Number: NASA-CR-189085
Report Number: NAS 1.26:189085
Accession Number
92N20880
Funding Number(s)
PROJECT: RTOP 505-63-5B
CONTRACT_GRANT: NAS3-21016
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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