Wartime Report: L 1-787 |
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aerodynamic AERONAUTICS Figure aileron effectiveness airfoil airplane 13 airplane 9 airspeed angle of attack approx areas of separation boundary-layer cannon installations Chaplygin characteristics of airplane chord line CImax CLmax COMMITTEE FOR AERONAUTICS differential equation drag coefficient duct Effect of propeller F6F-3 airplane faired and sealed flaps deflected functions hodograph Imax incompressible increased inlet Jacobian Langley Field Langley full-scale tunnel leading edge log q maximum lift coefficient measured miles per hour mock-up NACA LMAL nacelles NATIONAL ADVISORY COMMITTEE obtained Original slat particular solutions peller pressure profile drag propeller blade propeller operation Propeller removed pusher propeller reference Reynolds number Riccati equation rotational service condition shown in figure slat installation slipstream slotted flap Spanwise station speed spring-tab ailerons Stall progressions stalling characteristics taper ratio test velocity thrust coefficient tion trailing edge tuft observations values variables velocity potential wake wing section wing surface ат