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Aerodynamic tests of a low aspect ratio tapered wing with an auxiliary airfoil for use on tailless airplanes (1933)
NASA Technical Reports Server (NTRS) · leaf 11
N.A.0.A.Technical Mote Ho.477 Fig. 2 … cL, degrees Figure 2.- CL,CD, and o.p. with flap eet at various anglesNASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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