Print Email Facebook Twitter A method of fatigue life prediction using data obtained under random loading conditions Title A method of fatigue life prediction using data obtained under random loading conditions Author Kirkby, W.T. Edwards, P.R. Institution Royal Aircraft Establishment RAE Date 1966-01-31 Abstract Preliminary tests have been made to investigate a method of fatigue life prediction in which fatigue data obtained under a simple form of random loading are substituted for the data hitherto obtained under sinusoidal test conditions. The results of this work show a significant increase in the accuracy of prediction, but it is evident that further allowance for load interaction effects is necessary, if greater accuracy is to be obtained. To reference this document use: http://resolver.tudelft.nl/uuid:343f69af-8fed-4bbc-896f-5ac57ba0e78d Publisher Ministry of Aviation, Royal Aircraft Establishment, RAE Farnborough Access restriction Campus only Source RAE Technical Report No. 66023 Part of collection Aerospace Engineering Reports Document type report Rights © 1966 Ministry of Aviation, Royal Aircraft Establishment Files PDF Tech_Report_66023.pdf 20.52 MB Close viewer /islandora/object/uuid:343f69af-8fed-4bbc-896f-5ac57ba0e78d/datastream/OBJ/view