Selection of Aluminium Alloys by Fatigue Properties: A Method of Comparing the Performance of Different Alloy Types under Fatigue Conditions for which Complete Data are not Available
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 January 1957
Abstract
WHEN selecting alloys for use in structures whose life would be limited by fatigue, the choice is greatly aided by consideration of fatigue tests on simple test‐pieces in which the effects due to stress‐raisers, fretting, temperature, etc., are dealt with under idealized conditions.
Citation
Ward, R.G. (1957), "Selection of Aluminium Alloys by Fatigue Properties: A Method of Comparing the Performance of Different Alloy Types under Fatigue Conditions for which Complete Data are not Available", Aircraft Engineering and Aerospace Technology, Vol. 29 No. 1, pp. 19-20. https://doi.org/10.1108/eb032783
Publisher
:MCB UP Ltd
Copyright © 1957, MCB UP Limited