Call Number (LC) Title Results
Y 3.N 21/5:6/2703 Electrical techniques for compensation of thermal time lag of thermocouples and resistance thermometer elements / 1
Y 3.N 21/5:6/2704 Fatigue strengths of 14S-T4 aluminum alloy subjected to biaxial tensile stresses / 1
Y 3.N 21/5:6/2705 Theory of supersonic potential flow in turbomachines / 1
Y 3.N 21/5:6/2706 Effect of changing passage configuration on internal-flow characteristics of a 48-inch centrifugal compressor. : 1 - Change in blade shape / 1
Y 3.N 21/5:6/2707 Analogue-computer simulation of an autopilot servo system having nonlinear response characteristics / 2
Y 3.N 21/5:6/2708 Comparison of three multicylinder icing meters and critque of multicylinder method / 1
Y 3.N 21/5:6/2709 Fatigue and static tests of flush-riveted joints / 1
Y 3.N 21/5:6/2710 Diffusion of heat from a line source in isotropic turbulence / 1
Y 3.N 21/5:6/2711 The aerodynamic design of high Mach number nozzles utilizing axisymmetric flow with application to a nozzle of square test section / 2
Y 3.N 21/5:6/2712 Flow characteristics over a lifting wedge of finite aspect ratio with attached and detached shock waves at a Mach number of 1.40 / 1
Y 3.N 21/5:6/2713 Effect of compressor-outlet air bleed on performance of a centrifugal-flow turbojet engine with a constant-area jet nozzle / 1
Y 3.N 21/5:6/2714 Normal accelerations and operating conditions encountered by a helicopter in air-mail operations / 1
Y 3.N 21/5:6/2715 The theoretical characteristics of trangular-tip control surfaces at supersonic speeds Mach lines behind trailing edges / 1
Y 3.N 21/5:6/2716 Effect of open circular holes on tensile strength and elongation of sheet specimens of a magnesium alloy / 1
Y 3.N 21/5:6/2717 Effect of temperatures from -70 degrees to 600 degrees F on strength of adhesive-bonded lap shear specimens of clad 24S-T3 aluminum alloy and of cotton- and glass-fabric plastic laminates / 1
Y 3.N 21/5:6/2718 Two-dimensional steady nonviscous and viscous compressible flow through a system of equidistant blades / 1
Y 3.N 21/5:6/2719 Investigation of statistical nature of fatigue properties / 1
Y 3.N 21/5:6/2720 Effects of aspect ratio on air flow at high subsonic Mach numbers / 1
Y 3.N 21/5:6/2721 Initial results of instrument-flying trials conducted in a single-rotor helicopter / 1
Y 3.N 21/5:6/2722 Displacement effect of a three-dimensional boundary layer / 1