The Pressure Distribution over the Horizontal and Vertical Tail Surfaces of the F6C-4 Pursuit Airplane in Violent Maneuvers (1929)
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t the elevator angle, which in this case is 33.3°, being —490 pounds, while the component of force on the elevator parallel to the stabilizer chord is 160 pounds. In the pull-up at 173 M. P. H., although the accelera- tion obtained at the center of gravity was higher (fig. 29), the tail loading was… … Fig. 12. Pressure distribution in a reversal at 153 M. P. II. Run No. 70 (b) Fig. 13.—Pressure distribution in a reversal at 153 M. P. II. Run No. 70 (c) The total loads in the dives were relatively small, although the leading edge pressures and stabilizer loads were high. Little diiference existed…
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