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The thickness of a flange on an aircraft component s uniformly distributed between 1.95 and 2.05 millimeters. Determine the following. a) Cumulative distribution function of
The thickness of a flange on an aircraft component s uniformly distributed between 1.95 and 2.05 millimeters. Determine the following.
a) Cumulative distribution function of flange thickness
b) Proportion of flanges that exceeds 2.03 millimeters.
c) thickness exceeded by 95% of the flanges.
d) Mean and variance of flange thickness.
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