Research and Test Apparatus
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 November 1962
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