The propagation of fatigue cracks in various aircraft partshas been the subject of
Chapter 1, Problem 39(choose chapter or problem)
The propagation of fatigue cracks in various aircraft partshas 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 fastenerholes intended for use in military aircraft (StatisticalCrack Propagation in Fastener Holes Under SpectrumLoading, J.Aircraft, 1983: 10281032): .736 .863 .865 .913 .915 .937 .983 1.0071.011 1.064 1.109 1.132 1.140 1.153 1.253 1.394a. Compute and compare the values of the sample meanand median.b. By how much could the largest sample observationbe decreased without affecting the value of themedian?
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