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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 |
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Y 3.N 21/5:6/2201
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Measurement of the moments of inertia of an airplane by a simplified method / |
1 |
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Y 3.N 21/5:6/2202
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Effect of heat and power extraction on turbojet-engine performance. : 3 - Analytical determination of effects of shaft-power extraction / |
1 |
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Y 3.N 21/5:6/2203
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Boundary-layer measurements in 3.84- by 10-inch supersonic channel / |
1 |
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Y 3.N 21/5:6/2204
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Gust-tunnel investigation of a wing model with semichord line swept back 60 degrees / |
1 |
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Y 3.N 21/5:6/2205
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Theoretical supersonic characteristics of inboard trailing-edge flaps having arbitrary sweep and taper. : Mach lines behnid flap leading and trailing edges / |
1 |
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Y 3.N 21/5:6/2206
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Graphical method for obtaining flow field in two-dimensional supersonic stream to which heat is added / |
1 |
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Y 3.N 21/5:6/2207
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Analysis of turbulent free-convection boundary layer on flat plate / |
1 |
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Y 3.N 21/5:6/2208
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Analysis of shear strength of honeycomb cores for sandwich constructions / |
1 |
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Y 3.N 21/5:6/2209
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Free oscillations of an atmosphere in which temperature increases linearly with height / |
1 |
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Y 3.N 21/5:6/2210
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Impact-pressure interpretation in a rarefied gas at supersonic speeds / |
1 |
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Y 3.N 21/5:6/2211
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An approximate method of calculating pressures in the tip region of a rectangular wing of circular-arc section at supersonic speeds / |
1 |
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Y 3.N 21/5:6/2212
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The effect of ice formations on propeller performance / |
1 |
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Y 3.N 21/5:6/2213
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Aerodynamic coefficients for an oscillating airfoil with hinged flap, with tables for a Mach number of 0.7 / |
2 |
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Y 3.N 21/5:6/2214
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Formulas and tables of coefficients for numerical differentiation with function values given at unequally spaced points and application to solution of partial differential equations / |
1 |
