NASA Technical NoteNational Aeronautics and Space Administration., 1960 |
Other editions - View all
Common terms and phrases
accelerator air-melted buckets alloy analysis approximately arc-cast argon as-cast assumed balls billets boundary layer calculation carbide Chamber pressure Chamber temperature computed constant cracks cylinder dead band deceleration density determined distance distribution downstream electron engine equation equilibrium composition error evaluated extrusion fracture fuel guidance hardness heat flow rate heat transfer heat-transfer coefficient inch Inconel increment indicated initial integral curves isentropic lb/sq Lewis Research Center Mach number material maximum measured melting method NACA NASA neutralizing grid nitrogen nondimensional nozzle Nozzle-exit Nusselt obtained operation orthohydrogen parameters percent perigee plug potential PRESSURE RATIOS propellant pump radii range reference resistors Reynolds number Rockwell Rolling-contact fatigue shown in figure sintered solution specific heat specific impulse specimens station stress-rupture supersonic surface target thermal thermocouple thrust tion trajectory tungsten turbine turbojet uranium dioxide vacuum vacuum-melted values variation velocity viscosity wall
Popular passages
Page 21 - Braslow, Albert L.; and Knox, Eugene C.: Simplified Method for Determination of Critical Height of Distributed Roughness Particles for BoundaryLayer Transition at Mach Numbers From 0 to 5.
Page 26 - AMES RESEARCH STAFF : Equations, Tables, and Charts for Compressible Flow. NACA Rep. 1135, 1953. ( Supersedes NACA TN 1428.
Page 21 - Turbulent Flat-Plate Theory for Determining Values of Turbulent Aerodynamic Friction and Heat-Transfer Coefficients.
Page 10 - The Heat Transfer and Pressure Loss in Fluid Flow Through Randomly Packed Spheres,
Page 11 - Spangenberg, WG: Heat-Loss Characteristics of Hot-Wire Anemometers at Various Densities in Transonic and Supersonic Flow.
Page 21 - A Summary of Viscosity and Heat Conduction Data for He, A, H2, 02, N2, CO, C02, H20, and Air.
Page 11 - Stalder, Jackson R., Goodwin, Glen, and Creager, Marcus 0.: Heat Transfer to Bodies in a High-Speed Rarefied-Gas Stream.
Page 29 - VENANT (1870) [13] stated the law that the directions of the increments of the principal strains coincide with the directions of the principal stresses.
Page 11 - INTRODUCTION In recent years there has been an increasing interest in the use of LIDAR (laser radar) as an active optical remote sensor.
Page 21 - Ames Research Staff: Equations, Tables, and Charts for Compressible Flow. NACA Rep. 1135, 1953. (Supersedes NACA TN 1428.) 10.