ASD Technical Report, Numéro 62,Partie 910

aerodynamic AILERON airplane angle of attack angle-of-attack signal approximately block diagram CONAX Cornell Aeronautical Laboratory deg volts DEMOD design criteria DIVE BRAKES DIVE BRAKES 100 drag coefficient DRAG PER PETAL drag petals dump valves dynamic pressure effective L/D equivalent airspeed FEEDBACK Figures 29 FILTER flap deflection flap drag flaps and landing FLAPS UP DIVE Flight Dynamics flight test Function on Card GEAR UP FLAPS horsepower hydraulic system indicated airspeed input jettisoned knots L/D CALIBRATION CHART L/D computer landing gear LB hp MAXIMUM OPERATING LOAD obtained petal angle petal deflections petal drag PETAL EXTENSION PETAL FLANGE petal position petal rate pilot pitching pitching moment potentiometer pounds programmed reservoir RESISTORS safety of flight SCHEMATIC servo set of petals shown in Figure SIMULATED Sp/Ve spoilers Tactair TELEFLEX through-shaft pump tip tank trim change ULATOR variable stability VIAS voltage wind tunnel wind tunnel tests wing flaps x-force Δα бе