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
1994-09-01
Conference paper
No indication
English
A Method of Calculating the Safe Fatigue Life of Compact, Highly-Stressed Components
British Library Conference Proceedings | 1994
|Helicopter Dynamic Components Fatigue Safe Life Prediction
British Library Conference Proceedings | 2006
|Low cycle fatigue behaviour of alternative steels for highly stressed rail components
Tema Archive | 2008
|A Framework to Implement Probabilistic Fatigue Design of Safe-Life Components
Springer Verlag | 2019
|