Elevated-Temperature Al Alloys for Aircraft Structure-Reference-Cited by-同舟云学术

Elevated-Temperature Al Alloys for Aircraft Structure

Published:1988-05 Issue:5 Volume:40 Page:16-18
ISSN:1047-4838
Container-title:JOM
language:en
Short-container-title:JOM

Author:

Rainen Richard A.,Ekvall John C.

Publisher

Springer Science and Business Media LLC

Subject

General Engineering,General Materials Science

Link

http://link.springer.com/content/pdf/10.1007/BF03258903.pdf

Reference5 articles.

1. R.E. Sanders and G.J. Hildeman, “Elevated Temperature Aluminum Alloy Development,” AFWAL-TR-81-4076, September 1981.

2. S.L. Langenbeck and R.A. Rainen, et al., “Elevated Temperature Aluminum Alloy Development,” AFWAL-R-86-4027, May 1986.

3. “Elevated Temperature Powdered Aluminum Airframe Structure,” AFWAL Contract F33615-82-C-3200, July 1983–February 1990.

4. “Elevated Temperature Aluminum Program (ETAP),” AFWAL Contract F33615-87-C-3206, September 1987–December 1991.

5. “Standard Recommended Practice for Alternate Immersion Stress Corrosion Testing in 3.5 Percent Chloride Solution,” ASTM G44-75, Annual Book of ASTM Standards (1987).

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