Effects of 50,000 h of thermal aging on graphite/epoxy and graphite/polyimide composites

AIAA Journal

Volumn 22, Issue 1, 1984, Pages 96-102

  Kerr, J R ^a   Haskins, J F ^a  

^a GENERAL DYNAMICS   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

PLASTICS, REINFORCED - THERMAL EFFECTS;

COMPOSITE MATERIALS;

EID: 0021197244     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.8345     Document Type: Article

References (3)

1. Kerr, J. R. and Haskins, J. F., “Time-Temperature-Stress Capabilities of Composite Materials for Advanced Supersonic Technology Application,” General Dynamics Convair Division, San Diego, Calif., Rept. NASA CR-159267 (GDC-MAP-80-001), prepared for NASA-Langley Research Center, April 1980.
2. Chase, V. and Beeler, D., “Manufacturing Methods for Large High-Temperature Sandwich Structures,” Air Force Materials Laboratory, Dayton, Ohio, Tech. Rept. AFML-TR-70-211, 1970.
3. Haskins, J. E., Kerr, J. R., and Stein, B. A., “Flight Simulation Testing of Advanced Composites for Supersonic Cruise Aircraft Applications,” Proceedings of AIAA/ASME 18th Structures, Structural Dynamics, and Material Conference, March 1977