A methodology has been developed and embodied in two computer codes for quantitatively characterizing the material strength degradation of aerospace propulsion system structural components that are subjected to various random effects over the course of their service lives. The codes, PROMISS and PROMISC, constitute a material-resistance model that is used in the NESSUS aerospace structural-reliability program. NESSUS addresses the service life-reducing effects of high temperature, mechanical fatigue, and creep.
Probabilistic material degradation under high temperature, fatigue, and creep
Journal of Aerospace Engineering ; 6 , 4
01.10.1993
Sonstige
Keine Angabe
Englisch
Probabilistic Material Degradation under High Temperature, Fatigue, and Creep.
Online Contents | 1993
|Probabilistic analysis of creep-fatigue failure
AIAA | 2000
|