Influence of Low Load Truncation Level on Crack Growth for Al 2324-T39 and Al 7050-T7451-Reference-Cited by-同舟云学术

Influence of Low Load Truncation Level on Crack Growth for Al 2324-T39 and Al 7050-T7451

Published:2009-08 Issue:4 Volume:22 Page:401-406
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

Hailing Tian,Rui Bao,Jianyu Zhang,Xiaoling Zheng,Binjun Fei

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference17 articles.

1. Federal Aviation Administration, Advisory Circular. Damage tolerance and fatigue evaluation of structure. Federal Air Regulations 25, AC No.25.271-1C, 1998.

2. The effect of dynamic loading on fatigue scatter factor for Al 7050;Underhill;International Journal of Fatigue,2008

3. Study of underload effects on the delay induced by an overload in fatigue crack propagation;Bacila;International Journal of Fatigue,2007

4. Effect of load sequences on crack propagation under random and program loading;Schijve;Engineering Fracture Mechanics,1973

5. Fatigue of materials;Suresh,1991

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