The Pressure Distribution over the Horizontal and Vertical Tail Surfaces of the F6C-4 Pursuit Airplane in Violent Maneuvers (1929)
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-^30 -^20 ^10 ■t20 Lb.-ff.per ft. of span Lb.-ft. per ft. of span Fig. 23—Half roll at 161 M. P. H. Fig. 24.—Right roll at 109 M. P. H. Top Distance from 'fop of rudder^ Distance from top of rudder to bottom of balance bottom of balance iO -20 -30 -40 -SO ^/O *-50 +40 +30 +20 +10 Lb.-ff.per ft. of… … (a) Horizontal surfaces, Curve D: Chord loading in the condition (6) Vertical surfaces, Curve E: Chord loading in the condition of of maximum total load on stabilizer and elevator. Run No. 11 maximum total load on fm and rudder. Run No. 70 Figs. 27 (a) and (6).—Comparison of chord loadings Curve C:…
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