The fatigue behavior and delamination properties in fiber reinforced aramid laminates. - Case (I):AF...
The fatigue behavior and delamination properties in fiber reinforced aramid laminates. - Case (I):AFRP/Al Laminates
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English
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The fuselage-wing intersection suffers from the cyclic bending moment of variable amplitude. Therefore, the influence of cyclic bending moment on the delamination and the fatigue crack propagation behavior in AFRP/Al laminate of fuselage-wing was investigated in this study. The cyclic bending moment fatigue test in AFRP/Al laminate was performed wi...
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The fatigue behavior and delamination properties in fiber reinforced aramid laminates. - Case (I):AFRP/Al Laminates
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TN_cdi_proquest_miscellaneous_1266759656
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https://devfeature-collection.sl.nsw.gov.au/record/TN_cdi_proquest_miscellaneous_1266759656
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1738-494X
DOI
10.1007/BF02984360