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 15
.03 .03 … : Angle of attack at center of gravity, degrees Angle of attack at center of gravity, degrees i i ! Figure 7. - Yawing-moment coefficients due to Figure 8.- Yawing-moment coefficients due to £ fin and rudder. Sideslip at e.g. 0". fin and rudder. Sideslip at c.g.-l0° ? Cn (controls neutral), -Cn…
NASA Technical Reports Server (NTRS)
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