Preliminary results of one phase of a control-motion study program are presented in the form of plots of load factor.and angular acceleration against indicated airspeed and of time histories of several measured quantities. The results were obtained from 197 maneuvers performed by an F-86A jet-fighter airplane during normal squadron operational training. Most of the tactical maneuver8 of which the F-86A is capable were performed at pressure altitudes ranging from 0 to 32,000 feet and at indicated airspeeds ranging from 95 to 650 miles per hour.
Time-History Data of Maneuvers Performed by an F-86A Airplane During Squadron Operational Training
1952-05-23
Miscellaneous
No indication
English
Integration of F-100 airplane into air force squadron service
Engineering Index Backfile | 1957
|Engineering Index Backfile | 1960
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