Programme Load Fatigue Tests: Evaluation of Aircraft Structural Joint Lives
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 February 1962
Abstract
This preliminary investigation has shown that the programme load method of testing provides more useful information than single load level tests enabling a more reliable estimate of a structural joint fatigue life to be obtained.
Citation
Ryman, R.J. (1962), "Programme Load Fatigue Tests: Evaluation of Aircraft Structural Joint Lives", Aircraft Engineering and Aerospace Technology, Vol. 34 No. 2, pp. 34-42. https://doi.org/10.1108/eb033516
Publisher
:MCB UP Ltd
Copyright © 1962, MCB UP Limited