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Evaluation of composite flattened tubular specimenFlattened tubular specimens of graphite/epoxy, S-glass/epoxy, Kevlar-49/epoxy, and graphite/S-glass/epoxy hybrid materials were evaluated under static and cyclic uniaxial tensile loading and compared directly with flat coupon data of the same materials generated under corresponding loading conditions. Additional development for the refinement of the flattened specimen configuration and fabrication was required. Statically tested graphite/epoxy, S-glass/epoxy, and Kevlar 49/epoxy flattened tube specimens exhibit somewhat higher average strengths than their corresponding flat coupons. Flattened tube specimens of the graphite/S-glass/epoxy hybrid and the graphite/epoxy flattened tube specimens failed in parasitic modes with consequential lower strength than the corresponding flat coupons. Fatigue tested flattened tube specimens failed in parasitic modes resulting in lower fatigue strengths than the corresponding flat coupons.
Document ID
19780017190
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
June 1, 1978
Subject Category
Composite Materials
Report/Patent Number
NASA-CR-145353
IITRI-D6131
Report Number: NASA-CR-145353
Report Number: IITRI-D6131
Accession Number
78N25133
Funding Number(s)
CONTRACT_GRANT: NAS1-14663
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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