Effects of fibre/matrix adhesion on carbon-fibre-reinforced metal laminates—II. impact behaviour

Author:

Lawcock G.D,Ye L,Mai Y.W,Sun C.T

Publisher

Elsevier BV

Subject

General Engineering,Ceramics and Composites

Reference9 articles.

1. Johnson, W. S., Impact and residual fatigue behaviour of ARALL and AS6/5245 composite materials. NASA Technical Memorandum 89013, 1986.

2. Fatigue crack growth predictions in aramid reinforced aluminium laminates (ARALL);Marissen;J. Aircraft,1988

3. Vlot, A., Impact tests on fibre metal laminates under a tensile load, Report LR-714, Dept. of Aerospace Engineering, Delft University of Technology, The Netherlands, 1993.

4. Vlot, A., Low-velocity impact loading on fibre reinforced aluminium laminates (ARALL and GLARE) and other aircraft sheet materials, Report LR-718, Dept. of Aerospace Engineering, Delft University of Technology, The Netherlands, 1993.

5. Impact loading on fibre metal laminates;Vlot;Int. J. Impact Engng,1996

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