Effects of fibre/matrix adhesion on carbon-fibre-reinforced metal laminates—II. impact behaviour
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Research context
OpenAlex topics: Mechanical Behavior of Composites · Fiber-reinforced polymer composites · Natural Fiber Reinforced Composites
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References (9)
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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)10.2514/3.45553 ↗
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 laminates10.1016/0734-743X(96)89050-6 ↗
6. Lee, T. C. and Wilson, D. A., An investigation of the effects of temperature on the impact behaviour and residual strength of an aramid aluminium laminate (ARALL-2). In Composite Materials: Fatigue and Fracture ASTM STP 1110, ed. K. O'Brien. ASTM, Philadelphia, PA, 1991, p. 806.10.1520/STP17750S ↗
7. Lawcock, G. D., Ye, L., Mai, Y. W. and Sun, C. T., Effects of fibre/matrix adhesion on carbon fibre reinforced metal laminates. Part I: Residual strength. Composites Sci. Technol., in press.
8. Characterization of impact damage in ARALL laminates10.1016/0266-3538(93)90053-J ↗
9. Progressive damage and residual strength of a carbon fibre reinforced metal laminate10.1177/002199839703100802 ↗