Effect of stabilizer location upon pitching and yawing moments in spins as shown by tests with the spinning balance (1933)
NASA Technical Reports Server (NTRS) · leaf 13
trapolation of cross-plot a gainst angle of sideslip -.04 40 50 60 70 40 50 GO Angle of attack at center of gravity, degrees Angle of attack at center of gravity, H • Figure A.- Yawing-moment coefficients due to Figure 3.- Yawing-moment coefficients due to (A fin and rudder. Sideslip at e.g. 10°…
NASA Technical Reports Server (NTRS)
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