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Y 3.N 21/5:6/3005
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Heat transfer and skin friction by an integral method in the compressible laminar boundary layer with a streamwise pressure gradient / |
1 |
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Y 3.N 21/5:6/3006
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Correlation of calculation and flight studies of the effect of wing flexibility on structural response due to gusts / |
1 |
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Y 3.N 21/5:6/3007
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Lift and pitching moment at low speeds of the NACA 64A010 airfoil section equipped with various combinations of a leading-edge slat, leading-edge flap, split flap, and double-slotted flap / |
1 |
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Y 3.N 21/5:6/3008
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Effects of finite span on the section characteristics of two 45 degree sweptback wings of aspect ratio 6 / |
1 |
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Y 3.N 21/5:6/3009
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Velocity potential and air forces associated with a triangular wing in supersonic flow, with subsonic leading edges, and deforming harmonically according to a general quadratic equation / |
1 |
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Y 3.N 21/5:6/3010
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Comparison of effectiveness of convection-, transpiration-, and film-cooling methods with air as coolant / |
1 |
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Y 3.N 21/5:6/3012
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An analysis of turbojet-engine-inlet matching / |
1 |
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Y 3.N 21/5:6/3013
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A note on secondary flow in rotating radial channels / |
1 |
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Y 3.N 21/5:6/3014
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Calculated spanwise lift distributions and aerodynamic influence coefficients for unswept wings in subsonic flow / |
1 |
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Y 3.N 21/5:6/3015
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An experimental investigation of secondary flow in an accelerating, rectangular elbow with 90 degrees of turning / |
1 |
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Y 3.N 21/5:6/3016
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Analysis of turbulent heat transfer and flow in the entrance regions of smooth passages / |
1 |
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Y 3.N 21/5:6/3017
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Axial-load fatigue tests on notched and unnotched sheet specimens of 61S-T6 aluminum alloy, annealed 347 stainless steel, and heat-treated 403 stainless steel / |
1 |
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Y 3.N 21/5:6/3018
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A theoretical study of the effect of forward speed on the free-space sound-pressure field around propellers / |
1 |
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Y 3.N 21/5:6/3019
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Investigation of the statistical nature of the fatigue of metals / |
1 |
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Y 3.N 21/5:6/3020
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Determination of boundary-layer transition Reynolds numbers by surface-temperature measurement of a 10 degree cone in various NACA supersonic wind tunnels / |
1 |
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Y 3.N 21/5:6/3021
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A method of deriving frequency-response data for motion of the center of gravity from data measured on an aircraft at locations other than the center of gravity / |
1 |
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Y 3.N 21/5:6/3022
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Method for studying helicopter longitudinal maneuver stability / |
1 |
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Y 3.N 21/5:6/3023
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Results of edge-compression tests on stiffened flat-sheet panels of alclad and nonclad 14S-T6, 24S-T3, and 75S-T6 aluminum alloys / |
1 |
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Y 3.N 21/5:6/3024
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Maximum evaporation rates of water droplets approaching obstacles in the atmosphere under icing conditions / |
1 |
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Y 3.N 21/5:6/3025
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An investigation utilizing an electrical analogue of cyclic de-icing of hollow steel propellers with internal electric heaters / |
1 |
