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Accession Number:
ADA010422
Title:
Laminate Tubular Specimens Subjected to Biaxial Stress States (Graphite/Epoxy).
Corporate Author:
AIR FORCE FLIGHT DYNAMICS LAB WRIGHT-PATTERSON AFB OHIO
Report Date:
1975-03-01
Abstract:
The responses of 90 degreesplus or minus 30 degrees sub s, 0 degreesplus or minus 60 degrees sub s, 0 degreesplus or minus 45 degrees sub s, and 90 degreesplus or minus 15 degrees sub s graphite epoxy Courtald HTS Fibers in Fiberite-x904 Laminates subjected to biaxial stress states are presented. These results are obtained using tubular specimens with tsub D 0.015 and Lsub D approximately 1. Additionally included are the results of tests conducted on multidirectional flat specimens, both orthotropic and off-axis. The test results are compared with those predicted theoretically. There is reasonable agreement between analytical and experimental results.
Descriptive Note:
Technical rept.,
Supplementary Note:
See also AD-908 917.
Pages:
0113
File Size:
0.00MB
