Evaluation of fatigue crack growth behavior of GLARE3 fiber/metal laminates using a compliance method

Author:

Takamatsu T.,Shimokawa T.,Matsumura T.,Miyoshi Y.,Tanabe Y.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference16 articles.

1. Schmidt HJ, Schmidt-Brandecker B, Ohrloff N, Fleischer T. Current status of research and development activities for the fuselage of a large airbus aircraft. In: Proceedings of the 20th ICAF Symposium, Bellevue, 1999. p. 537–52

2. Vogelesang LB, Marissen R, Schijve J. A new fatigue resistant material: aramid reinforced aluminum laminate (ARALL). In: Proceedings of the 11th ICAF Symposium, Noordwijkerhout, NLR, 1981, 3.4/1–3.4/39

3. Flight simulation behavior of aramid reinforced aluminum laminates (ARALL);Marissen;Engng. Fract. Mech.,1984

4. Marissen R. Fatigue crack growth in ARALL. A hybrid aluminum–aramid composite material, crack growth mechanics and quantitative predictions of the crack growth rate, Report LR-754, Faculty of Aerospace Engng, Delft University of Technology, 1988

5. Fatigue of aircraft materials and structures;Schijve,1992

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