NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Tensile properties of textile compositesThe importance of textile composite materials in aerospace structural applications has been gaining momentum in recent years. With a view to better understand the suitability of these materials in aerospace applications, an experimental program was undertaken to assess the mechanical properties of these materials. Specifically, the braided textile preforms were infiltrated with suitable polymeric matrices leading to the fabrication of composite test coupons. Evaluation of the tensile properties and the analyses of the results in the form of strength moduli, Poisson's ratio, etc., for the braided composites are presented. Based on our past experience with the textile coupons, the fabrication techniques have been modified (by incorporating glass microballoons in the matrix and/or by stabilizing the braid angle along the length of the specimen with axial fibers) to achieve enhanced mechanical properties of the textile composites. This paper outlines the preliminary experimental results obtained from testing these composites.
Document ID
19930005565
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Avva, V. Sarma
(North Carolina Agricultural and Technical State Univ. Greensboro, NC, United States)
Sadler, Robert L.
(North Carolina Agricultural and Technical State Univ. Greensboro, NC, United States)
Lyon, Malcolm
(North Carolina Agricultural and Technical State Univ. Greensboro, NC, United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1992
Publication Information
Publication: NASA. Langley Research Center, FIBER-TEX 1991: The Fifth Conference on Advanced Engineering Fibers and Textile Structures for Composites
Subject Category
Composite Materials
Accession Number
93N14754
Funding Number(s)
CONTRACT_GRANT: NAGW-1331
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available