Engineering property comparisons of 7050-T73651, 7010-T7651 and 7010-T73651 aluminium alloy plate-Reference-Cited by-同舟云学术

Engineering property comparisons of 7050-T73651, 7010-T7651 and 7010-T73651 aluminium alloy plate

Published:1983-01 Issue:6 Volume:17 Page:493-507
ISSN:0013-7944
Container-title:Engineering Fracture Mechanics
language:en
Short-container-title:Engineering Fracture Mechanics

Author:

Schra L.,Hart W.G.J.'t

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference26 articles.

1. J. T. Staley, Investigation to develop a high strength stress corrosion resistant naval aircraft aluminum alloy. Final reports under Naval Air Systems Command Contracts N00019-69C-0292 and N00019-70C-0118 Jan. 1970 and Nov. 1970, ALCOA.

2. Further development of aluminium alloy X7050;Staley,1972

3. Stress corrosion cracking in aluminum alloys;Staley;Metals Engng Quart.,1973

4. Ageing kinetics of aluminum-alloy 7050;Staley;Metallurgical Trans.,1974

5. Evaluating new aluminum forging alloys;Staley;Metals Engng Quarterly,1974

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