To read this content please select one of the options below:

Research and Test Apparatus

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 November 1962

27

Abstract

Numerous components in high temperature machines are subjected during their working life to both static (creep) stresses and cyclic (fatigue) stresses. For example, with turbine blades, centrifugal force gives the creep increment of stress, and vibration gives the fatigue increment.

Citation

(1962), "Research and Test Apparatus", Aircraft Engineering and Aerospace Technology, Vol. 34 No. 11, pp. 342-342. https://doi.org/10.1108/eb033648

Publisher

:

MCB UP Ltd

Copyright © 1962, MCB UP Limited

Related articles