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- W75282610 abstract "Abstract The effect of impact on static strength and fatigue durability is reviewed. Impacts are categorised in terms of the impact velocity, impacting mass and impact energy. At low-to-medium velocities, delamination damage develops below the impact site with penetration likely at increased velocities. Under in-plane static compression buckling of impacted laminates reduces compression strength as measured by the compression after impact (CAI) test. Models for the prediction of onset of delamination damage and of the reduction in strength are summarised. The effect of impacts and delamination damage on fatigue durability is described. The greatest effects on fatigue strength are found during compression–compression fatigue. For the majority of composite systems, the strength reduction found under static loads is a worst case, with reduced effects at long fatigue lives. Fatigue stresses of 60–70% of the static CAI strength will not produce failure and give indefinite life. Cycling at greater stresses eventually produces delamination crack growth from the impact damage. After this delayed onset, fatigue delamination growth is extremely rapid and offers little or no possibility of achieving polymer composite aircraft damage tolerance via in-service inspection. A zero damage growth criterion is used instead." @default.
- W75282610 created "2016-06-24" @default.
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- W75282610 date "2015-01-01" @default.
- W75282610 modified "2023-09-26" @default.
- W75282610 title "Impact, post-impact strength and post-impact fatigue behaviour of polymer composites" @default.
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- W75282610 doi "https://doi.org/10.1016/b978-0-85709-523-7.00009-8" @default.
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