Pressure Distribution Tests on a Series of Clark Y Biplane Cellules with Special Reference to Stability (1933)
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30° 40° 50° 60° 70° 80° 90° oi (Upper wing) cc (Upper wing) Figure 21.—Effect of stagger and decalage on cellule coefficient of normal force Figure 18.—Effect of gap and decalago on cellule coefficient of normal force -10° 0° 10° 20° 30° 40° 50° 60° 70° 80° 90° -10° 0° 10° 20° 30° 40° 50° 60° 70°… … -i0° 0° 10° 20° 30° 40° 50° 60° 70° 80° 90° '-10° 0° 10° 20° 30° 40° 50° 60° 70° 80° 90° cc (Upper wing) cc (Upper wing) Figure 20.—Effect of gap and decalage on lower wing coefficient of normal force Figure 23.—Effect of stagger and decalage on lower wing coefficient of normal force
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