The fatigue behavior and delamination properties in fiber reinforced aramid laminates: Case (I):AFRP...
The fatigue behavior and delamination properties in fiber reinforced aramid laminates: Case (I):AFRP/A1 Laminates
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Seoul: Springer Nature B.V
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English
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Seoul: Springer Nature B.V
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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/A1 laminate of fuselage-wing was investigated in this study. The cyclic bending moment fatigue test in AFRP/A1 laminate was performed wi...
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The fatigue behavior and delamination properties in fiber reinforced aramid laminates: Case (I):AFRP/A1 Laminates
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TN_cdi_proquest_journals_1021010501
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https://devfeature-collection.sl.nsw.gov.au/record/TN_cdi_proquest_journals_1021010501
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ISSN
1738-494X
E-ISSN
1976-3824
DOI
10.1007/BF02984360