NACA Wartime Report: Series A. |
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Common terms and phrases
abrupt aileron rolls adverse yaw AERON AUTICS AERONAUTICS Figure aileron droop Ames Aeronautical Laboratory AMES FILLETS angle of attack ANGLE OF BANK ANGLE OF SIDESLIP center of gravity CHANGE IN ANGLE Characteristics in steady COMMITTEE FOR AERON COMMITTEE FOR AERONAUTICS COMPLETE MODEL control force controls in abrupt CRITICAL MACH NUMBER DRAG COEFFICIENT ducts effective balance EMPENNAGE fixed in trim flaps and gear flaps full Flaps two-thirds flight fuselage hinge line HORIZONTAL TAIL INDICATED AIRSPEED lateral controls lateral-control left aileron roll LEFT RIGHT LIBRARIES STANFORD UNIVERSITY lift coefficient maximum rolling velocity mean aerodynamic chord MODEL MINUS MODEL WITH AMES NACA NATIONAL ADVISORY COMMITTEE NORMAL FORCE COEFFICIENT number of divergence NUMBER WITH ANGLE pitching moment RADIANS PER SECOND radiator Reynolds number right aileron roll ROOT CHORD rudder fixed SIDESLIP DEGREES speed stability stall STANFORD UNIVERSITY LIBRARIES STICK FORCE POUNDS tests TOTAL AILERON ANGLE trim position UNIVERSITY LIBRARIES STANFORD VERTICAL TAILS WING CHORD