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The Aerodynamic Characteristics of a Slotted Clark Y Wing as Affected by the Auxiliary Airfoil Position (1932)

NASA Technical Reports Server (NTRS) · leaf 12

An illustration from The Aerodynamic Characteristics of a Slotted Clark Y Wing as Affected by the Auxiliary Airfoil Position, 1932, leaf 12
THE AERODYNAMIC CHARACTERISTICS OF A SLOTTED CLARK Y WING 1.8 /.6 1.4 1.2 8 -10 10 aO 30 40 '50 oc, degrees Figure 21. Cl and Cd versus a. Slot gap=3.5 per cent c. Slot depth=3.5 Figure 23.—and Co versus a. Slot gap=3.5 per cent c. Slot depth = 1.5 per cent c above c per cent c below c … per cent c above c per cent c below c

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