Mathematics, 02.09.2020 01:01 preservations
The propagation of fatigue cracks in various aircraft parts has been the subject of extensive study in recent years. The accompanying data consists of propagation lives (flight hours/104) to reach a given crack size in fastener holes intended for use in military aircraft (A1Statistical Crack Propagation in Fastener Holes Under Spectrum Loading, A1 J. Aircraft, 1983: 1028A11032):
.736 .863 .865 .913 .915 .937 .983 1.007 1.011 1.064 1.109 1.132 1.140 1.153 1.253 1.394
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The propagation of fatigue cracks in various aircraft parts has been the subject of extensive study...
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