=+68. According to the article Optimization of Distribution Parameters for Estimating Probability of Crack Detection (J. of
Question:
=+68. According to the article “Optimization of Distribution Parameters for Estimating Probability of Crack Detection” (J. of Aircraft, 2009:
2090–2097), the following “Palmberg” equation is commonly used to determine the probability Pd
(c) of detecting a crack of size c in an aircraft structure:
Pd
(c) 5 (cyc
*
)
1 1 (cyc
*
)
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Related Book For
Applied Statistics For Engineers And Scientists
ISBN: 9781133111368
3rd Edition
Authors: Jay L. Devore, Nicholas R. Farnum, Jimmy A. Doi
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