Wartime Report A, Issues 76-79 |
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Common terms and phrases
150 aileron abrupt aileron rolls adverse yaw AERON AUTICS AERONAUTICS Figure aileron droop airplane was controllable Ames Aeronautical Laboratory angle of attack ANGLE OF BANK angle of sideslip center of gravity center-of-gravity CHANGE IN ANGLE Characteristics in steady Cmc.g COMMITTEE FOR AERON COMMITTEE FOR AERONAUTICS control force controls in abrupt deflector vane drag coefficient effective balance fixed in trim flaps and gear flaps deflected flaps full Flaps two-thirds flight hinge line horizontal tail lateral controls left aileron roll LEFT RIGHT lift coefficient Mach number maximum rolling velocity mean aerodynamic chord miles per hour NACA NATIONAL ADVISORY COMMITTEE NORMAL ACCELERATION NORMAL FORCE COEFFICIENT original condition percent mean aerodynamic pitching-moment coefficient power on left power on right RADIANS PER SECOND right aileron roll ROLLING VELOCITY RADIANS ROOT CHORD rudder fixed SECONDS Figure shown in figure sideslip angle SIDESLIP DEGREES speed stall STICK FORCE POUNDS tests TOTAL AILERON ANGLE trim position