Aerodynamic tests of a low aspect ratio tapered wing with various flaps, for use on tailless airplanes (1933)
NASA Technical Reports Server (NTRS) · leaf 9
BJL.CJL. Technical Mote Ho.463 TlS. 3 -20 ►3 c 20 o ^ 40 1 g «> o Inner flap 7° tip Pi D n n io° " A * " 15° " - & 80 X " « 20° » * + H H 3QO H … figure 3.-CJ,, Cj) and c.p. with full span plain flap divided into four parts of equal span. Outer pair set 7° up, center pair at various angles.
NASA Technical Reports Server (NTRS)
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