A review of fatigue crack growth in high strength aluminum alloys and the relevant metallurgical factors-Reference-Cited by-同舟云学术

A review of fatigue crack growth in high strength aluminum alloys and the relevant metallurgical factors

Published:1973-09 Issue:3 Volume:5 Page:523-540
ISSN:0013-7944
Container-title:Engineering Fracture Mechanics
language:en
Short-container-title:Engineering Fracture Mechanics

Author:

Hahn C.T.,Simon R.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference58 articles.

1. Numerical analysis of crack propagation in cyclicloaded structures;Forman;ASME J. bas. Engng,1967

2. Axial-load fatigue properties of 245-T and 755-T aluminum alloy as determined on several laboratories;Grover;Nat. Adv. Com. for Aeronautics Tech. Note 2928,1953

3. The Rate of Crack Propagation in Two Aluminum Alloys;McEvily;NASA Tech. Note No. 4394,1958

4. Propagation of fatigue cracks in various sheet materials;Frost;J. Mech. Engng. Science,1959

5. The rate of fatigue-crack propagation of two aluminum alloys under completely reversed loading;McEvily;NASA Tech. Note No. D-52,1959

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