NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
An investigation of the compressive strength of Kevlar 49/epoxy compositesTests were performed to evaluate the effect of a wide range of variables including matrix properties, interface properties, fiber prestressing, secondary reinforcement, and others on the ultimate compressive strength of Kevlar 49/epoxy composites. Scanning electron microscopy is used to assess the resulting failure surfaces. In addition, a theoretical study is conducted to determine the influence of fiber anisotropy and lack of perfect bond between fiber and matrix on the shear mode microbuckling. The experimental evaluation of the effect of various constituent and process characteristics on the behavior of these unidirectional composites in compression did not reveal any substantial increase in strength. However, theoretical evaluations indicate that the high degree of fiber anisotropy results in a significant drop in the predicted stress level for internal instability. Scanning electron microscope data analysis suggests that internal fiber failure and smooth surface debonding could be responsible for the measured low compressive strengths.
Document ID
19750059217
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Kulkarni, S. V.
Rosen, B. W.
(Materials Sciences Corp. Blue Bell, Pa., United States)
Rice, J. S.
(United Engineers and Constructors, Inc. Philadelphia, Pa., United States)
Date Acquired
August 8, 2013
Publication Date
September 1, 1975
Publication Information
Publication: Composites
Volume: 6
Subject Category
Composite Materials
Accession Number
75A43289
Funding Number(s)
CONTRACT_GRANT: NAS1-11780
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available