The buffeting loads measured on the wing and tail of a fighter airplane during 194 maneuvers are given in tabular form, along with the associated flight conditions. Measurements were made at altitudes of 30,000 to 10,000 feet and at speeds up to a Mach number of 0.8. Least-squares methods have been used for a preliminary analysis of the data. The agreement between the results of this analysis and the loads measured in stalls is sufficiently good to suggest the examination of the buffeting of other airplanes on the same basis.
Measurement and Analysis of Wing and Tail Buffeting Loads on a Fighter Airplane
1955-01-01
Miscellaneous
No indication
English
Measurement and analysis of wing and tail buffeting loads on fighter airplane
Engineering Index Backfile | 1955
|Measurement and analysis of wing and tail buffeting loads on fighter-type airplane
Engineering Index Backfile | 1954
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