Call Number (LC) Title Results
Y 3.N 21/5:6/2827 Investigation of a diffraction-grating interferometer for use in aerodynamic research / 1
Y 3.N 21/5:6/2828 Effect of a finite trailing-edge thickness on the drag of rectangular and delta wings at supersonic speeds / 1
Y 3.N 21/5:6/2829 Experiments on transonic flow around wedges / 1
Y 3.N 21/5:6/2830 Several combination probes for surveying static and total pressure and flow direction / 1
Y 3.N 21/5:6/2831 Span load distributions resulting from constant angle of attack, steady rolling velocity, steady pitching velocity, and constant vertical acceleration for tapered sweptback wings with streamwise tips. : Subsonic leading edges and supersonic trailing edges / 1
Y 3.N 21/5:6/2832 Theoretical study of the transonic lift of a double-wedge profile with detached bow wave / 1
Y 3.N 21/5:6/2833 An analysis of normal accelerations and airspeeds of one type of twin-engine transport airplane in commercial operations over a northern transcontinental route / 1
Y 3.N 21/5:6/2834 Flow surfaces in rotating axial-flow passages / 1
Y 3.N 21/5:6/2835 Effect of changing passage configuration on internal-flow characteristics of a 48-inch centrifugal compressor. : 2 - Change in hub shape / 1
Y 3.N 21/5:6/2836 Radiant-interchange configuration factors / 1
Y 3.N 21/5:6/2837 Corrections for drag, lift, and moment of an axially symmetrical body placed in a supersonic tunnel having a two-dimensional pressure gradient / 1
Y 3.N 21/5:6/2838 Calorimetric determination of constant-pressure specific heats of carbon dioxide at elevated pressures and temperatures / 1
Y 3.N 21/5:6/2839 Development of turbulence-measuring equipment / 1
Y 3.N 21/5:6/2840 Buckling of low arches or curved beams of small curvature / 1
Y 3.N 21/5:6/2841 Investigation of 75-millimeter-bore deep-groove ball bearings under radial load at high speeds. : 1 - Oil-flow studies / 1
Y 3.N 21/5:6/2842 The planing characteristics of a surface having a basic angle of dead rise of 40 degrees and horizontal chine flare / 1
Y 3.N 21/5:6/2843 Auxiliary equipment and techniques for adapting the constant-temperature hot-wire anemometer to specific problems in air-flow measurements / 1
Y 3.N 21/5:6/2844 Laminar boundary layer on cone in supersonic flow at large angle of attack / 1
Y 3.N 21/5:6/2845 X-ray instrumentation for density measurements in a supersonic flow field / 1
Y 3.N 21/5:6/2846 Effective lubrication range for steel surfaces boundary lubricated at high sliding velocities by various classes of synthetic fluids / 1