Aerodynamic rolling and yawing moments produced by floating wing-tip ailerons, as measured by spinning balance (1934)
NASA Technical Reports Server (NTRS) · leaf 11
H.A.O.A. Teohnioal lote No. 493 Fig. 3 -O.ll a m 4Q0 ■3 o -o.i p - 0° a * 50° -0.2 … 40 50 60 70 -10 -5 0 5 10 a, degrees p, degrees Figure 3.- Yawing-moment coefficients, body axes, for model with and without float- ing wing-tip ailerons, and oomputed values. Right spin.
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