Maneuverability Investigation of an F6C-4 Fighting Airplane (1932)
NASA Technical Reports Server (NTRS) · leaf 10
recovery with abrupt is increased. The maximum negative angle of attack control action. The time histories with the respective decreases as the starting speed increases. This would paths are shown in Figures 11, 12, and 13. The be expected with equal normal accelerations. With principal quantities… … \\\ Figure 6.—Protractor sheet illustrating method of determining wind each maneuver were 140 ft, 170 ft, and 175 feet, respectively. With an initial air speed of 100 miles per hour the altitude loss in four seconds was 290 feet with the F6C-4 as compared with 405 feet for the F6C-3. This is…
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