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Y 3.N 21/5:11/L88
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Determination from flight tests of thrust coefficients for 10 full-scale airplanes in the gliding condition with engine idling / |
1 |
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Y 3.N 21/5:11/L89
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Preliminary flight research on an all-movable horizontal tail as a longitudinal control for flight at high Mach numbers / |
1 |
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Y 3.N 21/5:11/L9
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Comparisons of methods of computing bending moments in helicopter rotor blades in the plane of flapping / |
1 |
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Y 3.N 21/5:11/L90
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Flight investigation at high Mach numbers of several methods of measuring static pressure on an airplane wing / |
1 |
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Y 3.N 21/5:11/L91
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Flight investigation at high speeds of flow conditions over an airplane wing as indicated by surface tufts / |
1 |
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Y 3.N 21/5:11/L92
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Effect of lateral shift of center of gravity on rudder deflection required for trim / |
1 |
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Y 3.N 21/5:11/L93
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Flight studies of the horizontal-tail loads experienced by a modern pursuit airplane in abrupt maneuvers / |
1 |
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Y 3.N 21/5:11/L94
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Flight investigation of boundary-layer transition and profile drag of an experimental low-drag wing installed on a fighter-type airplane / |
1 |
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Y 3.N 21/5:11/L95
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A method for predicting the elevator deflection required to land / |
1 |
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Y 3.N 21/5:11/L96
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Spinning of large airplanes / |
1 |
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Y 3.N 21/5:11/L97
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Effect of rotor-tip speed on helicopter hovering performance and maximum forward speed / |
1 |
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Y 3.N 21/5:11/L98
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Flight investigation at high speeds of profile drag of wing of a P-47D airplane having production surfaces covered with camouflage paint / |
1 |
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Y 3.N 21/5:11/L99
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Comparison of wind-tunnel and flight measurements of stability and control characteristics of a Douglas A-26 airplane / |
1 |
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Y 3.N 21/5:11/W-10
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An investigation of aircraft heaters. : VI - Heat transfer equations for the single pass longitudinal exchanger / |
1 |
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Y 3.N 21/5:11/W-11
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An investigation of aircraft heaters. : V - Theory and use of heat meters for the measurement of rates of heat transfer which are independent of time / |
1 |
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Y 3.N 21/5:11/W-13
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An investigation of aircraft heaters. : VII - Thermal radiation from athermanous exhaust gases / |
1 |
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Y 3.N 21/5:11/W-14
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An investigation of aircraft heaters. : VIII - A simplified method for the calculation of the unit thermal conductance over wings / |
1 |
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Y 3.N 21/5:11/W-15
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An investigation of aircraft heaters. : XI - Measured and predicted performance of a slotted-fin exhaust gas and air heat exchanger / |
1 |
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Y 3.N 21/5:11/W-16
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An investigation of aircraft heaters. : X - Measured and predicted performance of a fluted-type exhaust gas and air heat exchanger / |
1 |
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Y 3.N 21/5:11/W-17
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An investigation of aircraft heaters. : XII - Performance of a formed-plate crossflow exhaust gas and air heat exchanger / |
1 |
