NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
High strain rate properties of off-axis composite laminates, part 2Unidirectional off-axis 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 were loaded by internal pressure with the tensile stress at 22.5, 30, and 45 degrees relative to the fiber direction. 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 three laminates of both materials the modulus and strength increase sharply with strain rate, reaching values roughly 100, 150, and 200 percent higher than corresponding static values for the 22.5(sub 8), 30(sub 8), and 45(sub 8) degree laminates, respectively. In the case of ultimate strain no definite trends could be established, but the maximum deviation from the average of any value for any strain rate was less than 18 percent.
Document ID
19920011652
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-189084
NAS 1.26:189084
Report Number: NASA-CR-189084
Report Number: NAS 1.26:189084
Accession Number
92N20894
Funding Number(s)
CONTRACT_GRANT: NAS3-21016
PROJECT: IITRI PROJ. M-06026
PROJECT: RTOP 505-63-5B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available