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Thermal expansion properties of composite materialsThermal expansion data for several composite materials, including generic epoxy resins, various graphite, boron, and glass fibers, and unidirectional and woven fabric composites in an epoxy matrix, were compiled. A discussion of the design, material, environmental, and fabrication properties affecting thermal expansion behavior is presented. Test methods and their accuracy are discussed. Analytical approaches to predict laminate coefficients of thermal expansion (CTE) based on lamination theory and micromechanics are also included. A discussion is included of methods of tuning a laminate to obtain a near-zero CTE for space applications.
Document ID
19810023033
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Johnson, R. R.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Kural, M. H.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Mackey, G. B.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
September 4, 2013
Publication Date
July 1, 1981
Publication Information
Publisher: NASA. Langley Research Center
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-165632
Accession Number
81N31576
Funding Number(s)
CONTRACT_GRANT: NAS1-14887
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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