Pressure Distribution Tests on a Series of Clark Y Biplane Cellules with Special Reference to Stability (1933)
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-.02 -03. 50° 40° 0° 10° 20° 30° 10° of (Upper winq) pb Figure 43—Effect of dihedral on rolling moment due to roll at jj/^O.OS Figure 40.—Effect of decalage on rolling moment due to roll at 2V=0M .03r ..03r 4> -02 .02 4! CO CO ^ .01 .01 -.01 -.01 ■8 5) -.02 .02 ■°-3,o 50° 40° 10° 20° 30° -.03 0°… … Figure 45.—Effect of combined sweepback and stagger on rolling Figure 42.—Effect of combined decalage and stagger on rolling moment pb pb moment due to roll at 2y=0.05 =0.05 due to roll at 2 V
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