An investigation on fatigue crack growth rates through a designed nonsymmetric crack growth test

Author:

He Xiaofan,Tan Mingyi,Xing Jing Tang

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference47 articles.

1. Wanhill RJH. Milestone case histories in aircraft structural integrity. NLR-TP-2002-521. Netherlands: National Aerospace Laboratory; 2002.

2. A history of fatigue;Schutz;Engng Fracture Mech,1996

3. USAF. Military specification airplane damage tolerance requirements. MIL-A-83444; 1974.

4. Gallagher J. Damage tolerant design handbook: guidelines for the analysis and design of damage tolerant aircraft structures. Report MCIC-HB-01R. OH, USA: Air Force Wright Aeronautical Laboratories, Wright-Patterson Air Force Base; 1984.

5. Engle RM, Gallagher JP, Giessler FJ, Berens AP. USAF DT design handbook. Guidelines for the analysis and design of damage tolerant aircraft structures. AFWAL-TR-82-3073; 1984.

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