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
> … 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 and for wing with full-span…
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
