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- W354578822 abstract "Since 1984 the NLR has done many fatigue crack growth tests to compare the modern Al-Li alloys 2090, 2091 and 8090 with the conventional damage tolerant alloys 2024 and 2324. Under constant amplitude loading the Al-Li alloy crack growth behaviour is often equivalent or superior to that of the conventional alloys. However, under gust spectrxim loading the conventional alloys are generally better. The changes in rankings are explained from fracture surface analysis. The practical significance of the results is discussed, and guidelines for further investigation are given." @default.
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- W354578822 date "1991-04-24" @default.
- W354578822 modified "2023-09-24" @default.
- W354578822 title "Flight simulation and constant amplitude fatigue crack growth in aluminium-lithium sheet and plate" @default.
- W354578822 hasPublicationYear "1991" @default.
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