The Aerodynamic Forces and Moments on a Spinning Model of the F4B-2 Airplane as Measured by the Spinning Balance (1935)
NASA Technical Reports Server (NTRS) · leaf 20
Figs. 10,11 O.A. Technioal Note Vo. 517 Figure 11.- Variation of C* and Cn with rudder and elevator movement. F4B-4 fin and F4B-3 rudder witn F4B-3 stabilizer, a. » 46° 48' and 0-0° 43' .
NASA Technical Reports Server (NTRS)
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