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Evaluation of hybrid composite materials in cylindrical specimen geometriesStatic and fatigue properties of three composite materials and hybrids were examined. The materials investigated were graphite/epoxy, S-glass/epoxy, PRD-49 (Kevlar 49)/epoxy, and hybrids in angle-ply configurations. A new type of edgeless cylindrical specimen was developed. It is a flattened tube with two flat sides connected by curved sections and it is handled much like the standard flat coupon. Special specimen fabrication, tabbing, and tab region reinforcing techniques were developed. Axial modulus, Poisson's ratio, strength, and ultimate strain were obtained under static loading from flattened tube specimens of nine laminate configurations. In the case of graphite/epoxy the tubular specimens appeared to yield somewhat higher strength and ultimate strain values than flat specimens. Tensile fatigue tests were conducted with all nine types of specimens and S-N curves obtained. Specimens surviving 10 million cycles of tensile loading were subsequently tested statically to failure to determine residual properties.
Document ID
19760020273
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Liber, T.
(IIT Research Inst. Chicago, IL, United States)
Daniel, I. M.
(IIT Research Inst. Chicago, IL, United States)
Date Acquired
September 3, 2013
Publication Date
March 31, 1976
Subject Category
Composite Materials
Report/Patent Number
NASA-CR-145006
IITRI-D6089
Report Number: NASA-CR-145006
Report Number: IITRI-D6089
Accession Number
76N27361
Funding Number(s)
CONTRACT_GRANT: NAS1-12645
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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