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Thermal expansion of composites using Moire interferometryAn experimental technique for precise measurement of the thermal response of fiber-reinforced composite materials uses moire interferometry with fringe multiplication which yield a sensitivity of 833 nm (32.8 mu in.) per fringe. Results from the technique are compared with those obtained from electrical resistance strain gages, and also those predicted from classical lamination theory. Temperature dependent coefficients of thermal expansion for composite materials subjected to thermal cycling in the temperature range of 297 K (75 F) to 422 K (300 F) were determined for four laminate configurations (0, 90, 0/ + or - 45/90 sub s and 0/90/ + or - 45 sub s) of T300/5208 graphite epoxy, and ranged from -0.107 mu epsilon K/1 (-0.059 mu epsilon deg F/-) for the 0 laminate to 32.18 mu epsilon K/1 (17.88 mu epsilon F/1) for the 90 laminate. Moisture was found to greatly influence the thermal response of a quasi-isotropic laminate, resulting in hysteresis and residual compressive strain as the moisture content was reduced. Comparisons between moire and strain gage measurements were inconclusive with both techniques giving consistent but systematically different results. Differences of as much as 29% were observed.
Document ID
19800020928
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Bowles, D. E.
(Virginia Polytech. Inst. and State Univ. Blacksburg, United States)
Post, D.
(Virginia Polytech. Inst. and State Univ. Blacksburg, United States)
Herakovich, C. T.
(Virginia Polytech. Inst. and State Univ. Blacksburg, United States)
Tenny, D. R.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
August 1, 1980
Subject Category
Composite Materials
Report/Patent Number
IR-20
VPI-E-80-19
NASA-TM-80788
Accession Number
80N29429
Funding Number(s)
CONTRACT_GRANT: NGR-47-004-129
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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