ESTIMATING RELIABILITY AS A FUNCTION OF STRESS/STRENGTH DATA
Abstract
The mode of failure for guided weapons is shown to be by chance excess of the failure strength of some component of the assemblage rather than by wear out. An expression for the probability of such failure is developed utilizing the assumption of the normal density function for the description of the scatter of maximum stress experience and of failure strength of a component. The effect of reduction of scatter is shown, both for a single component and for a multiplicity of components.
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 01, 1961
- Accession Number
- AD0268363
Entities
People
- J. E. Norman
Organizations
- United States Army Aviation and Missile Command