Effect of low-temperature overload on fatigue crack growth retardation and prediction of post overload fatigue life-Reference-Cited by-同舟云学术

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Effect of low-temperature overload on fatigue crack growth retardation and prediction of post overload fatigue life

Published:2014-02 Issue:1 Volume:33 Page:100-106
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Sahu Vaneshwar Kr.,Anil Kumar J.K.S.,Mohanty J.R.,Verma B.B.,Ray P.K.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference32 articles.

1. Early fatigue crack growth as the damage accumulation process;Bolotin;Probabilistic Engg. Mechanics,2001

2. Analytical model of fatigue crack growth retardation due to overloading;Bolotin;Int. J. Solids Struct.,1996

3. Plane strain crack toughness testing of high strength metallic materials;Brown;ASTM Spec. Tech. Publ.,1966

4. Analysis of closure in fatigue crack growth;Budiansky;Trans. ASME, J. Appl. Mech.,1978

5. A simple crack closure model for prediction of fatigue crack growth rates under variable amplitude loading;De Koning;ASTM Spec. Tech. Publ.,1981

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