Y 3.N 21/5:6/1148
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Flow tests of an NACA-designed supercharger inlet elbow and the effects of various components on the flow characteristics at the elbow outlet / |
1 |
Y 3.N 21/5:6/1149
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Performance of hoods for aircraft exhaust-gas turbines / |
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Y 3.N 21/5:6/1150
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A Relaxation procedure for the stress analysis of a continuous beam-column elastically restrained against deflection and rotation at the supports / |
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Y 3.N 21/5:6/1151
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Summary of drag characteristics of practical-construction wing sections / |
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Y 3.N 21/5:6/1152
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Flight investigation of the effect of a local change in wing contour on chordwise pressure distribution at high speeds / |
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Y 3.N 21/5:6/1153
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Foaming volume and foam stability / |
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Y 3.N 21/5:6/1154
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A Comparison of the lateral motion calculated for tailless and conventional airplanes / |
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Y 3.N 21/5:6/1155
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A Preliminary study of a propeller powered by gas jets issuing from the blade tips / |
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Y 3.N 21/5:6/1156
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Column and plate compressive strengths of aircraft structural materials. : Extruded 0-1HTA magnesium alloy / |
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Y 3.N 21/5:6/1157
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Compressive strength of 24S-T aluminum-alloy flat panels with longitudinal formed hat-section stiffeners / |
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Y 3.N 21/5:6/1158
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Flutter and oscillating air-force calculations for an airfoil in a two-dimensional supersonic flow / |
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Y 3.N 21/5:6/1159
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Turbosupercharger-rotor temperatures in flight / |
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Y 3.N 21/5:6/1160
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The Infrared spectra of spiropentane, methylenecyclobutane, and 2-methyl-1-butene / |
1 |
Y 3.N 21/5:6/1161
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Effect of catalysts and pH on strength of resin-bonded plywood / |
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Y 3.N 21/5:6/1162
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Effect of brake forming in various tempers on the strength of alclad 75S-T aluminum-alloy sheet / |
1 |
Y 3.N 21/5:6/1163
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The Synthesis and purification of aromatic hydrocarbons. : 4-1,2,3-trimethylbenzene / |
1 |
Y 3.N 21/5:6/1164
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The Synthesis and purification of aromatic hydrocarbons. : 5 - 1-ethyl-3-methylbenzene / |
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Y 3.N 21/5:6/1165
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Tensile properties of a sillimanite refractory at elevated temperatures / |
1 |
Y 3.N 21/5:6/1166
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Variation of hydrodynamic impact loads with flight-path angle for a prismatic float at 0 degrees and -3 degrees trim and with a 22 1/2 degree angle of dead rise / |
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Y 3.N 21/5:6/1167
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Pressure distributions and force tests of an NACA 65-210 airfoil section with a 50-percent-chord flap / |
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