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Y 3.N 21/5:6/2937
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Method for calculating the rolling and yawing moments due to rolling for unswept wings with or without flaps or ailerons by use of nonlinear section lift data / |
1 |
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Y 3.N 21/5:6/2938
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Analysis of heat addition in a convergent-divergent nozzle / |
1 |
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Y 3.N 21/5:6/2939
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Optimum controllers for linear closed-loop systems / |
1 |
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Y 3.N 21/5:6/2940
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Effect of high bulk temperatures on boundary lubrication of steel surfaces by synthetic fluids / |
1 |
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Y 3.N 21/5:6/2941
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The drag of finite-length cylinders determined from flight tests at high Reynolds numbers for a Mach number range from 0.5 to 1.3 / |
1 |
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Y 3.N 21/5:6/2942
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Pressure distributions about finite wedges in bounded and unbounded subsonic streams / |
1 |
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Y 3.N 21/5:6/2943
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The attenuation characteristics of four specially designed mufflers tested on a practical engine setup / |
1 |
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Y 3.N 21/5:6/2944
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The zero-lift drag of a slender body of revolution (NACA RM-10 research model) as determined from tests in several wind tunnels and in flight at supersonic speeds / |
1 |
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Y 3.N 21/5:6/2945
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The creep of single crystals of aluminum / |
1 |
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Y 3.N 21/5:6/2946
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A small Pirani gage for mesurements of nonsteady low pressures / |
1 |
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Y 3.N 21/5:6/2947
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A visualization study of secondary flows in cascades / |
1 |
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Y 3.N 21/5:6/2948
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Investigation of lateral control near the stall. : Flight investigation with a light high-wing monoplane tested with various amounts of washout and various lengths of leading-edge slot / |
1 |
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Y 3.N 21/5:6/2949
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A variable-frequency light synchronized with a high-speed motion-picture camera to provide very short exposure times / |
1 |
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Y 3.N 21/5:6/2950
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A new shadowgraph technique for the observation of conical flow phenomena in supersonic flow and preliminary results obtained for a triangular wing / |
1 |
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Y 3.N 21/5:6/2951
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Flight investigation of the effect of transient wing response on wing strains of a four-engine bomber airplane in rough air / |
1 |
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Y 3.N 21/5:6/2952
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Impingement of water droplets on NACA 65₁-208 and NACA 65₁-212 airfoils at 4 degree angle of attack / |
1 |
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Y 3.N 21/5:6/2953
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An investigation of the experimental aerodynamic loading on a model helicopter rotor blade / |
1 |
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Y 3.N 21/5:6/2954
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The structure of turbulence in fully developed pipe flow / |
1 |
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Y 3.N 21/5:6/2955
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Estimation of forces and moments due to rolling for several slender-tail configurations at supersonic speeds / |
1 |
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Y 3.N 21/5:6/2956
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Creep-buckling analysis of rectangular-section columns / |
1 |
