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Y 3.N 21/5:6/2181
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The aerodynamic forces and moments on a 1/10-scale model of a fighter airplane in spinning attitudes as measured on a rotary balance in the Langley 20-foot free-spinning tunnel / |
2 |
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Y 3.N 21/5:6/2182
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Analysis of effect of variations in primary variables on time constant and turbine-inlet-temperature overshoot of turbojet engine / |
1 |
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Y 3.N 21/5:6/2183
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Analysis for control application of dynamic characteristics of turbojet engine with tail-pipe burning / |
2 |
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Y 3.N 21/5:6/2184
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Investigation of frequency-response characteristics of engine speed for a typical turbine-propeller engine / |
1 |
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Y 3.N 21/5:6/2185
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Analytical determination of coupled bending-torsion vibrations of cantilever beams by means of station functions / |
1 |
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Y 3.N 21/5:6/2186
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Method for determining pressure drop of air flowing through constant-area passages for arbitrary heat-input distributions / |
1 |
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Y 3.N 21/5:6/2187
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Bonding investigation of titanium carbide with various elements / |
1 |
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Y 3.N 21/5:6/2188
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Experimental investigation of stiffened circular cylinders subjected to combined torsion and compression / |
1 |
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Y 3.N 21/5:6/2189
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The development and performance of two small tunnels capable of intermittent operation at Mach numbers between 0.4 and 4.0 / |
1 |
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Y 3.N 21/5:6/2190
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The use of an uncalibrated cone for determination of flow angles and Mach numbers at supersonic speeds / |
1 |
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Y 3.N 21/5:6/2191
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Theoretical investigation and application of transonic similarity law for two dimensional flow / |
1 |
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Y 3.N 21/5:6/2192
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A survey of the flow at the plane of the propeller of a twin-engine airplane / |
1 |
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Y 3.N 21/5:6/2193
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Effect of heat-capacity lag on a variety of turbine-nozzle flow processes / |
1 |
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Y 3.N 21/5:6/2194
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The NACA oil-damped V-G recorder / |
1 |
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Y 3.N 21/5:6/2195
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A flight investigation and analysis of the lateral-oscillation characteristics of an airplane / |
1 |
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Y 3.N 21/5:6/2196
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Effect of heat-capacity lag on the flow through oblique shock waves / |
1 |
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Y 3.N 21/5:6/2197
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Pressure distribution and damping in steady pitch at supersonic Mach numbers of flat swept-back wings having all edges subsonic / |
1 |
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Y 3.N 21/5:6/2198
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Sintering mechanism between zirconium carbide and columbium / |
1 |
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Y 3.N 21/5:6/2199
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Wind-tunnel investigation at low speed of the lateral control characteristics of an unswept untapered semispan wing of aspect ratio 3.13 equipped with various 25-percent-chord plain ailerons / |
1 |
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Y 3.N 21/5:6/2200
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A study of second-order supersonic-flow theory / |
1 |
