The results from stress measurements in flight operation afford data for analyzing the frequency of appearance of certain parts of the static breaking strength during a specified number of operating hours. Appropriate frequency evaluations furnish data for the prediction of the required strength under repeated stress in the wing structures of aircraft of the different stress categories for the specified number of operating hours demanded during the life of a component.
Statistical analysis of the time and fatigue strength of aircraft wing structures
1941-10-01
Sonstige
Keine Angabe
Englisch
Statistical analysis of time and fatigue strength of aircraft wing structures
Engineering Index Backfile | 1941
|Estimation of fatigue damage in aircraft wing structures
Engineering Index Backfile | 1954
|Fatigue Analysis of an Aircraft Wing Spar
SAE Technical Papers | 1999
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