Call Number (LC) Title Results
Y 3.N 21/5:6/3084 A method for measuring the product of inertia and the inclination of the principal longitudinal axis of inertia of an airplane / 1
Y 3.N 21/5:6/3085 An experimental study of porosity characteristics of perforated materials in normal and parallel flow / 1
Y 3.N 21/5:6/3086 Maneuver accelerations experienced by five types of commercial transport airplanes during routine operations / 1
Y 3.N 21/5:6/3087 Experimental investigation of two-dimensional tunnel-wall interference at high subsonic speeds / 1
Y 3.N 21/5:6/3088 Determination of the flying qualities of the Douglas DC-3 airplane / 1
Y 3.N 21/5:6/3089 One-dimensional, compressible, viscous flow relations applicable to flow in a ducted helicopter blade / 1
Y 3.N 21/5:6/3090 Investigation of sandwich construction under lateral and axial loads / 1
Y 3.N 21/5:6/3091 Flow properties of strong shock waves in xenon gas as determined for thermal equilibrium conditions / 1
Y 3.N 21/5:6/3092 Hydrodynamic drag of 12- and 21-percent-thick surface-piercing struts / 1
Y 3.N 21/5:6/3093 Effect of type of porous surface and suction velocity distribution on the characteristics of a 10.5-percent-thick airfoil with area suction / 1
Y 3.N 21/5:6/3094 The resistance to air flow of porous materials suitable for boundary-layer -control applications using area suction / 1
Y 3.N 21/5:6/3095 The Ames 10- by 14-inch supersonic wind tunnel / 2
Y 3.N 21/5:6/3096 Theoretical prediction of pressure distributions on nonlifting airfoils at high subsonic speeds / 1
Y 3.N 21/5:6/3097 Turbulent boundary-layer and skin-friction measurements in axial flow along cylinders at Mach numbers between 0.5 and 3.6 / 1
Y 3.N 21/5:6/3098 Density profiles of subsonic boundary layers on a flat plate determined by x-ray and pressure measurements / 1
Y 3.N 21/5:6/3099 Impingement of water droplets on an ellipsoid with fineness ratio 5 in axisymmetric flow / 1
Y 3.N 21/5:6/3100 Statistical study of transition-point fluctuations in supersonic flow / 1
Y 3.N 21/5:6/3101 Study of three-dimensinal internal flow distribution based on measurements in a 48-inch radial-inlet centrifugal impeller / 1
Y 3.N 21/5:6/3102 An analytical and experimental study of the transient response of a pressure-regulating relief valve in a hydraulic circuit / 1
Y 3.N 21/5:6/3103 Cooling requirements for stability of laminar boundary layer with small pressure gradient at supersonic speeds / 1