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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 |
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Y 3.N 21/5:6/2215
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Compressibility correction for turning angles of axial-flow inlet guide vanes / |
1 |
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Y 3.N 21/5:6/2216
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Investigation of 75-millimeter-bore cylindrical roller bearings at high speeds. |
1 |
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Y 3.N 21/5:6/2217
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Analysis of plane-stress problems with axial symmetry in strain-hardening range / |
1 |
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Y 3.N 21/5:6/2218
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Diffusion of chromium in alpha-cobalt-chromium solid solutions / |
1 |
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Y 3.N 21/5:6/2219
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The dynamic lateral control characteristics of airplane models having unswept wings with round- and sharp-leading-edge sections / |
1 |
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Y 3.N 21/5:6/2220
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A balsa-dust technnique for air-flow visualization and its application to flow through model helicopter rotors in static thrust / |
1 |
