A Response Surface for the Complex Modulus of Composite Materials
Technical rept. 1 Jul 1972-30 Apr 1974
VIRGINIA POLYTECHNIC INST AND STATE UNIV BLACKSBURG COLL OF ENGINEERING
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The complex modulus of boronepoxy and graphiteepoxy laminates has been measured in forced vibration tests at frequencies rang-ing from 20 to 17, 000 Hz and temperatures varied between -50 and 300F. The data was analyzed using response surface methodo-logy. Based on the response surface time- temperature shift para-meters, master curves, and probability relations have been developed.
- Laminates and Composite Materials