This paper describes a method which has been developed for estimating the safe fatigue life of compact, highly-stressed and inaccessible components for aeroplanes and helicopters of the Royal Air Force. It is explained why the Design Requirements for British Military Aircraft do not favor the use of a damage-tolerance approach in these circumstances.
A method of calculating the safe fatigue life of compact, highly-stressed components
01.09.1994
Aufsatz (Konferenz)
Keine Angabe
Englisch
A Method of Calculating the Safe Fatigue Life of Compact, Highly-Stressed Components
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