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A-26B AIRPLANE AAF aerodynamic center aileron rolls angle of attack angle of sideslip approximately center of gravity center-of-gravity positions clean condition COMMITTEE FOR AERONAUTICS control characteristics cowl flaps curves data of figure dihedral directional stability Douglas A-26B airplane downwash elevator angle elevator control force elevator deflections required elevator tab flying qualities full aileron deflection fuselage hinge line increment indicated airspeed landing condition landing gear Langley Field lateral and directional level flight lift coefficient maneuver maximum normal-force coefficient mean aerodynamic chord Measurement of Flying miles per hour NACA nacelle NATIONAL ADVISORY COMMITTEE obtained percent M.A.C. percent mean aerodynamic pounds propeller rated power required for trim requirements of reference rudder fixed shown in figure sideslip angle sq ft Stability and Control stalling characteristics stick-fixed neutral point stick-free straight flight take-off thrust axis Trimming tab variation of elevator variation of rudder vertical tail wing