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Y 3.N 21/5:6/2850
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Study of pressure effects on vaporization rate of drops in gas streams / |
1 |
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Y 3.N 21/5:6/2851
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The aerodynamic design of supersonic propellers from structural considerations / |
1 |
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Y 3.N 21/5:6/2852
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An investigation utilizing an electrical analogue of cyclic de-icing of a hollow steel propeller with an external blade shoe / |
1 |
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Y 3.N 21/5:6/2853
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A study of the application of power-spectral methods of generalized harmonic analysis to gust loads on airplanes / |
1 |
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Y 3.N 21/5:6/2854
|
Average skin-friction drag coefficients from tank tests of a parabolic body of revolution (NACA RM-10) / |
1 |
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Y 3.N 21/5:6/2855
|
General correlation of temperature profiles downstream of a heated air jet directed at various angles to air stream / |
1 |
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Y 3.N 21/5:6/2856
|
Estimated power reduction by water injection in a nonreturn supersonic wind tunnel / |
1 |
|
Y 3.N 21/5:6/2857
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A theoretical method of analyzing the effects of yaw-damper dynamics on the stability of an aircraft equipped with a second-order yaw damper / |
1 |
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Y 3.N 21/5:6/2858
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Supersonic wave drag of nonlifting delta wings with linearly varying thickness ratio / |
1 |
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Y 3.N 21/5:6/2859
|
The Langley 2,000-horsepower propeller dynamometer and tests at high speed of an NACA 10-(3)(08)-03 two-blade propeller / |
1 |
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Y 3.N 21/5:6/2860
|
Interaction between a supersonic stream and a parallel subsonic stream bounded by fluid at rest / |
1 |
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Y 3.N 21/5:6/2861
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Analytical investigation of icing limit for diamond-shaped airfoil in transonic and supersonic flow / |
1 |
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Y 3.N 21/5:6/2862
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Influence of nonmartensitic transformation products on mechanical properties of tempered martensite / |
1 |
|
Y 3.N 21/5:6/2863
|
Laminar natural-convection flow and heat transfer of fluids with and without heat sources in channels with constant wall temperatures / |
1 |
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Y 3.N 21/5:6/2864
|
Convection of a pattern of vorticity through a shock wave / |
1 |
|
Y 3.N 21/5:6/2865
|
Investigation of gases evolved during firing of vitreous coatings on steel / |
1 |
|
Y 3.N 21/5:6/2866
|
Icing protection for a turboject transport airplane: heating requirements, methods of protection, and performance penalties / |
1 |
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Y 3.N 21/5:6/2867
|
Heat and momentum transfer between a spherical particle and air streams / |
1 |
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Y 3.N 21/5:6/2868
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Reflection of a weak shock wave from a boundary layer along a flat plate. : 1 - Interaction of weak shock waves with laminar and turbulent boundary layers analyzed by momentum-integral method / |
1 |
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Y 3.N 21/5:6/2869
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Reflection of a weak shock wave from a boundary layer along a flat plate. : 2 - Interaction of oblique shock wave with a laminar boundary layer analyzed by differential-equation method / |
1 |
