Wind tunnel research concerning lateral control devices, particularly at high angles of attack VII : Handley Page tip and full-span slots with ailerons and spoilers (1933)
NASA Technical Reports Server (NTRS) · leaf 38
N.A.C.A. Technical Note No. 443 Figs. 8,10 8 16 24 32 40 48 Angle of attack, degrees, cL Fig. 8 Lift , drag, and center of pressure for Clark. Y wing with 50 per cent b/2 tip slots and for plain wing. Yaw = 0° … Fig.10 Lift, drag, and center of pressure for Clark Y wing with full-span slot and for plain wing. Yaw = 0°
NASA Technical Reports Server (NTRS)
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