=+68. According to the article Optimization of Distribution Parameters for Estimating Probability of Crack Detection (J. of

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=+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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Applied Statistics For Engineers And Scientists

ISBN: 9781133111368

3rd Edition

Authors: Jay L. Devore, Nicholas R. Farnum, Jimmy A. Doi

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