Fatigue crack propagation in 7050-T7451 plate alloy

Author:

Schubbe Joel J.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference15 articles.

1. Branger, J., Life estimation and prediction of fighter aircraft. In: Proceedings of international conference on structural safety and reliability, Pergamon Press; 1972. p. 213–37.

2. MATWEB: The Online Materials Database, Automation Creations; 2006–2007.

3. Kaiser Aluminum – Technical Reference Library: Alloy 7050; 2007.

4. Hunsicker, HY. Development of Al–Zn–Mg–Cu alloys for aircraft. Philosophical Transactions of the Royal Society of London, Series A: Mathematical and Physical Sciences, vol. 282(1307), Rosenhain Centenary Conference: The Contribution of Physical Metallurgy to Engineering Practice; July 8, 1976. p. 359–76.

5. AFGROW – US Air Force Crack Growth Software; v4.11.14.0, 2006.

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