Crack Propagation of 7050 Aluminum alloy Under Constant Amplitude Loading and Peak Overloads-Reference-Cited by-同舟云学术

Crack Propagation of 7050 Aluminum alloy Under Constant Amplitude Loading and Peak Overloads

Published:2015 Issue: Volume:114 Page:613-620
ISSN:1877-7058
Container-title:Procedia Engineering
language:en
Short-container-title:Procedia Engineering

Author:

Borrego L.P.,Costa J.D.,Ferreira J.A.M.

Publisher

Elsevier BV

Subject

Applied Mathematics

Reference15 articles.

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2. Elber W. The significance of fatigue crack closure. In: Damage Tolerance in Aircraft Structures, ASTM STP 486. Philadelphia: ASTM 1971; p. 230-242.

3. Borrego LP, Ferreira JM, Costa JM. Evaluation of overload effects on fatigue crack growth and closure. Engng Fract Mech 2003; 70: 1379-1397.

4. Shin CS, Hsu SH. On the mechanisms and behaviour of overload retardation in AISI 304 stainless steel. Int J Fatigue 1993;15: 181-192.

5. American Society for Testing and Materials. Standard test method for microhardness of materials. Annual Book of ASTM Standards 2000: Volume 03.01, ASTM E 647.

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