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 39
> .08 > … a /e £-4 3? 0 8 16 24 32 40 Angle of attack, degrees, ct Angle of attach, degrees, a Fig. 9 Rolling-moment coefficients due to roll- Fig.ll Rolling-moment coefficients due to roll- ing at ^ = 0.05 and yaw = 0° far Clark Y ing at = °-05 BJld y&w= 00 ior Clark Y wing with 50 per cent b/2 tip slots…
NASA Technical Reports Server (NTRS)
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