The interpretation of cumulative frequency distributions of measured flight loads can be increased significantly by an additional extreme value analysis. This method not only leads to a higher reliability in fatigue design but may be used also for a prediction of extreme loading conditions and for a description of the effect of airplane and flight parameters on loads, as is demonstrated for c.g. vertical accelerations and gust velocities measured on airplanes of type C-130. (Author)
Extreme Value Analysis and Its Application to C. G. Vertical Accelerations Measured on Transport Airplanes of Type C-130
1971
28 pages
Report
Keine Angabe
Englisch
Further measurements of normal accelerations on racing airplanes
Engineering Index Backfile | 1936
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