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
S5 .03 r. o v Removed o Normal■** Stabilizer + Forward … H • Figure A.- Yawing-moment coefficients due to Figure 3.- Yawing-moment coefficients due to (A fin and rudder. Sideslip at e.g. 10° fin and rudder. Sideslip at e.g. 0°. (inward). Cn (controls 35" with the spin),-Cn. Cn (controls 35" with the spin),-Cn (tail sur- 03 (tail surfaces removed). faces…
NASA Technical Reports Server (NTRS)
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