Accession Number:

ADA232023

Title:

Model Sensitivity in Stress-Strength Reliability Computations

Descriptive Note:

Final rept.

Corporate Author:

ARMY LAB COMMAND WATERTOWN MA MATERIAL TECHNOLOGY LAB

Report Date:

1991-01-01

Pagination or Media Count:

27.0

Abstract:

There has been a recent interest in determining high statistical reliability in risk assessment of aircraft components. This report identifies the potential consequences of incorrectly assuming a particular statistical distribution for stress or strength data used in obtaining the high reliability values. The computation of the reliability is defined as the probability of the strength being greater than the stress over the range of stress values. This method is often referred to as the stress strength model. A sensitivity analysis was performed involving a comparison of reliability results in order to evaluate the effects of assuming specific statistical distributions. Both known population distributions, and those that differed slightly from the known, were considered. Results showed substantial differences in reliability estimates even for almost nondetectable differences in the assumed distributions. These differences represent a potential problem in using the stress strength model for high reliability computations, since in practice it is impossible to ever know the exact population distribution. An alternative reliability computation procedure is examined involving determination of a lower bound on the reliability values using extreme value distributions. This procedure reduces the possibility of obtaining nonconservative reliability estimates. Results indicated the method can provide conservative bounds when computing high reliability.

Subject Categories:

  • Aircraft
  • Statistics and Probability

Distribution Statement:

APPROVED FOR PUBLIC RELEASE