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Y 3.N 21/5:6/3695
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An analysis of buzzing in supersonic ram jets by a modified one-dimensional nonstationary wave theory / |
2 |
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Y 3.N 21/5:6/3696
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A study of the high-speed performance characteristics of 90 degree bends in circular ducts / |
1 |
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Y 3.N 21/5:6/3697
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Flight tests at supersonic speeds to determine the effect of taper on the zero-lift drag of sweptback low-aspect-ratio wings / |
1 |
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Y 3.N 21/5:6/3698
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Preliminary investigation of self-excited vibrations of single planing surfaces / |
1 |
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Y 3.N 21/5:6/3699
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Some effects of joint conductivity on the temperatures and thermal stresses in aerodynamically heated skin-stiffener combinations / |
1 |
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Y 3.N 21/5:6/3700
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On subsonic flow past a paraboloid of revolution / |
1 |
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Y 3.N 21/5:6/3701
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Comparison of several methods for obtaining the time response of linear systems to either a unit impulse or arbitrary input from frequency-response data / |
1 |
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Y 3.N 21/5:6/3702
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Measurements of atmospheric turbulence over a wide range of wavelength for one meteorological condition / |
1 |
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Y 3.N 21/5:6/3703
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The flow past an unswept- and a swept-wing-body combination and their equivalent bodies of revolution at Mach numbers near 1.0 / |
1 |
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Y 3.N 21/5:6/3704
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Minimum-drag ducted and closed three-point body of revolution based on linearized supersonic theory / |
1 |
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Y 3.N 21/5:6/3705
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An investigation of forward-located fixed spoilers and deflectors as gust alleviators on an unswept-wing model / |
1 |
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Y 3.N 21/5:6/3706
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Investigation of the laminar aerodynamic heat-transfer characteristics of a hemisphere-cylinder in the Langley 11-inch hypersonic tunnel at a Mach number of 6.8 / |
1 |
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Y 3.N 21/5:6/3707
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Flutter of thin propeller blades, including effects of Mach number, structural damping, and vibratory-stress measurements near the flutter boundaries / |
1 |
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Y 3.N 21/5:6/3708
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Investigation at supersonic speeds of the variation with Reynolds number and Mach number of the total, base, and skin-friction drag of seven boattail bodies of revolution designed for minimum wave drag / |
1 |
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Y 3.N 21/5:6/3709
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Aerodynamic investigation of a parabolic body of revolution at Mach number of 1.92 and some effects of an annular supersonic jet exhausting from the base / |
2 |
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Y 3.N 21/5:6/3710
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Preliminary investigation of the effects of external wing fuel tanks on ditching behavior of a sweptback-wing airplane / |
1 |
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Y 3.N 21/5:6/3711
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Some effects of guide-vane turning and stators on the rotating stall characteristics of a high hub-tip ratio single-stage compressor / |
1 |
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Y 3.N 21/5:6/3712
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Boundary layer behind shock or thin expansion wave moving into stationary fluid / |
1 |
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Y 3.N 21/5:6/3713
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Selection of optimum configurations for heat exchanger with one dominating film resistance / |
1 |
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Y 3.N 21/5:6/3714
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A sonic-flow orifice probe for the in-flight measurement of temperature profiles of a jet engine exhaust with afterburning / |
1 |
