The Aerodynamic Characteristics of a Slotted Clark Y Wing as Affected by the Auxiliary Airfoil Position (1932)
NASA Technical Reports Server (NTRS) · leaf 14
13 THE AERODYNAMIC CHARACTERISTICS OF A SLOTTED CLARK Y WING _J I I \ I I 1 J I -/rl 1 I I I 1 ' I il I 16 M IB 10 8 6 4 2 0 18 16 14 12 ■ 10 8 6 4 2 0 Width, per cent ctiord Wid tin, per cent chord Maximum lift coefficient, c. Angle of attack for maximum lift, a.. ^ max. Figure 25—Locus of point X… … Width, per cen t chord Width, per cen t chord Maximum lift coefficient, c. Angle of attack for maximum lift, a_ ' Li max. I'J Figure 26.—Locus of point X to obtain various airfoil characteristics. Qag=2 per cent c I \ 1 \ \ 1 \ il 1 I I \ \ ' ' I I il ■ 16 14 12 10 8 6 4 2 0 16 14 12 10 8 6 4 2 O…
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