The Pressure Distribution over the Horizontal and Vertical Tail Surfaces of the F6C-4 Pursuit Airplane in Violent Maneuvers (1929)
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PORT NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS conditions are given for illustration in Table I, Run No. 7. The maximum total load on the horizontal surfaces occurred in a pull-up at 163 M. P. H. In this maneuver, also, the maxi- mum local pressure and the maximum loads on the stabiHzer and… … Fig. 11.—Pressure distribution in a rudder reversal at 153 M. P. H. Run No. 70 (a) is not exact, the true force in this direction, taking into account 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…
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