Publication Date

8-1999

Comments

UTEP-CS-99-28.

Published in: J. Ramirez-Angulo (ed.), Proceedings of the 1999 IEEE Midwest Symposium on Circuits and Systems, August 8-11, 1999, Las Cruces, New Mexico, Vol. 1, pp. 435-438.

Abstract

For non-destructive testing of aerospace structures, it is extremely important to know how the probability of detecting a fault depends on its size. Recently, an empirical formula has been found which described this dependence. In this paper, we provide the theoretical justification for this formula by using methods motivated by the neural network approach.

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