NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Nonlinear effects on composite laminate thermal expansionAnalyses of Graphite/Polyimide laminates shown that the thermomechanical strains cannot be separated into mechanical strain and free thermal expansion strain. Elastic properties and thermal expansion coefficients of unidirectional Graphite/Polyimide specimens were measured as a function of temperature to provide inputs for the analysis. The + or - 45 degrees symmetric Graphite/Polyimide laminates were tested to obtain free thermal expansion coefficients and thermal expansion coefficients under various uniaxial loads. The experimental results demonstrated the effects predicted by the analysis, namely dependence of thermal expansion coefficients on load, and anisotropy of thermal expansion under load. The significance of time dependence on thermal expansion was demonstrated by comparison of measured laminate free expansion coefficients with and without 15 day delay at intermediate temperature.
Document ID
19790009094
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hashin, Z.
(Materials Sciences Corp. Blue Bell, PA, United States)
Rosen, B. W.
(Materials Sciences Corp. Blue Bell, PA, United States)
Pipes, R. B.
(Materials Sciences Corp. Blue Bell, PA, United States)
Date Acquired
September 3, 2013
Publication Date
February 1, 1979
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-3088
MSC/TFR/800/1015
Report Number: NASA-CR-3088
Report Number: MSC/TFR/800/1015
Accession Number
79N17265
Funding Number(s)
PROJECT: RTOP 524-71-01-01
CONTRACT_GRANT: NAS1-14964
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available