The effect of lateral controls in producing motion of an airplane as computed from wind-tunnel data (1937)
NASA Technical Reports Server (NTRS) · leaf 21
to a An analysis of the available data indicates the certain degree. Tests of wings with very large sweep- following values for the parameters: back, such as are used on tailless airplanes, have been made in which the rolling moment due to yaw actually = -0.012 reversed its sign when the stall was… … Aspect ratio -.12 Fioube 2i.—Factors for correcting wind-tunnel value of 6 (j^f) #r for aspect rat o Fioube 24.—EoMng moment doe to sideslip. TJntapered wings without dihedral; and taper. aspect ratio, 6; 7- by KMoot wmd-tannel measurements. where dCi/dfi is in terms of radians and T and A are of…
NASA Technical Reports Server (NTRS)
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