Call Number (LC) Title Results
Y 3.N 21/5:11/L81 A solution of the direct and inverse potential problems for arbitrary cascades of airfoils / 1
Y 3.N 21/5:11/L82 Effects of Reynolds number and leading-edge roughness on lift and drag characteristics of the NACA 65,3-418, a = 1.0 airfoil section / 1
Y 3.N 21/5:11/L83 Comparison of yaw characteristics of a single-engine airplane model with single-rotating and dual-rotating propellers / 1
Y 3.N 21/5:11/L84 Low-pressure boundary-layer control in diffusers and bends / 1
Y 3.N 21/5:11/L85 Use of variable-ratio geared tabs to improve stick-force characteristics in turning flight / 1
Y 3.N 21/5:11/L86 Fight investigation of boundary-layer and profile-drag characteristics of smooth wing sections of a P-47D airplane / 1
Y 3.N 21/5:11/L87 A comparison of data obtained by two flight techniques for determining the sideslip characteristics of a fighter airplane / 1
Y 3.N 21/5:11/L88 Determination from flight tests of thrust coefficients for 10 full-scale airplanes in the gliding condition with engine idling / 1
Y 3.N 21/5:11/L89 Preliminary flight research on an all-movable horizontal tail as a longitudinal control for flight at high Mach numbers / 1
Y 3.N 21/5:11/L9 Comparisons of methods of computing bending moments in helicopter rotor blades in the plane of flapping / 1
Y 3.N 21/5:11/L90 Flight investigation at high Mach numbers of several methods of measuring static pressure on an airplane wing / 1
Y 3.N 21/5:11/L91 Flight investigation at high speeds of flow conditions over an airplane wing as indicated by surface tufts / 1
Y 3.N 21/5:11/L92 Effect of lateral shift of center of gravity on rudder deflection required for trim / 1
Y 3.N 21/5:11/L93 Flight studies of the horizontal-tail loads experienced by a modern pursuit airplane in abrupt maneuvers / 1
Y 3.N 21/5:11/L94 Flight investigation of boundary-layer transition and profile drag of an experimental low-drag wing installed on a fighter-type airplane / 1
Y 3.N 21/5:11/L95 A method for predicting the elevator deflection required to land / 1
Y 3.N 21/5:11/L96 Spinning of large airplanes / 1
Y 3.N 21/5:11/L97 Effect of rotor-tip speed on helicopter hovering performance and maximum forward speed / 1
Y 3.N 21/5:11/L98 Flight investigation at high speeds of profile drag of wing of a P-47D airplane having production surfaces covered with camouflage paint / 1
Y 3.N 21/5:11/L99 Comparison of wind-tunnel and flight measurements of stability and control characteristics of a Douglas A-26 airplane / 1