Probabilistic Fatigue Methodology for Safe Retirement Lives
Author:
Affiliation:
1. Aerostructures Directorate, US Army AVSCOM, Langley Research Center, Hampton, Va.
Publisher
American Helicopter Society
Cited by 4 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. Analysis of Fatigue Crack Growth Rate Data in an Aircraft 7175-T7351 Al-Alloy Generated at Different Accredited Laboratories with Probability Life Assessment Example;Journal of Multiscale Modelling;2018-12
2. Generation and use of standardised load spectra and load–time histories;International Journal of Fatigue;2005-08
3. From Six-Nines Expectation to Three-Nines Reality: Calculating Reliability Correctly;Journal of the American Helicopter Society;2003-10-01
4. Quantifying Spectrum Loading Effects on Fatigue Crack Growth in 7075-T73 Aluminum;Journal of the American Helicopter Society;2000-01-01
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