The Effect of Airfoil Thickness and Plan Form on Lateral Control (1924)
NASA Technical Reports Server (NTRS) · leaf 10
EFFECT OF AIRFOIL THICKNESS AND PLAN FORM ON lATERAL CONTROL. 10° 20° 30° 40° 0° 10° aO" 30° 0° 10° 20° SO'' 0° fO° 20° 30 Angle ofot/ock Figs. 18,19,20, and 21.--Eflect of ailerons on angular velocity (iS. P.M.) about X axis. Airspeed 30m/sec. (79.4 ft./sec.)
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