Downstream radiation flux to blunt entry vehicles.
Downstream radiation flux distribution calculated for blunt entry bodies, considering self absorption effects
Burns, R. K.↗
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Downstream cooling effectiveness of massive upstream transpiration from a slender cone.
Radiation equilibrium temperature measured downstream of transpiration cooled gas flow near slender cone vertex in continuous flow hypersonic tunnel
Dunavant, J. C.↗
The effects of upstream mass injection on downstream heat transfer
Downstream heat transfer of upstream mass injectio in supersonic laminar boundary layer flow
Wolfram, W. R., Jr.↗
Boundary-layer velocity profiles downstream of three-dimensional transition trips on a flat plate at Mach 3 and 4
Boundary layer velocity profiles downstream of three dimensional transition trips on flat plates at Mach 3 and 4
Peterson, J. B., Jr.↗
Explorator heat-transfer measurements at Mach 10 on a 7.5 deg total-angle cone downstream of a region of air and helium transpiration cooling
Heat transfer measurements at Mach 10 on total angle cone downstream of air and helium transpiration cooling region
Dunavant, J. C.↗
Condensation on spacecraft surfaces downstream of a Kaufman thruster
Thruster exhaust products condensation on surfaces downstream of mercury electron bombardment ion thruster
Reynolds, T. W.↗
Initial performance data on a low-power MPD arc thruster with a downstream cathode
Low power MPD arc thrustor performance with downstream cathode, using Xe propellant
Burkhart, J. A.↗
The effects of upstream mass injection on downstream heat transfer
Upstream mass injection effects on downstream heat transfer of supersonic reacting boundary layer
Walker, W. F.↗
Effect of simulated downstream flow blockage doors on the performance of an axial-flow fan rotor
Simulating downstream flow blockage doors in bypass air duct of turbofan engine with axial flow fan rotor
Osborn, W. M.↗
An integral analysis of heat transfer downstream of a rearward-facing step with small coolant injection
Integral analysis of heat transfer downstream of rearward-facing step with small coolant injection
Karashima, K.↗
Contamination of spacecraft surfaces downstream of a Kaufman thruster
Effects of mercury electron bombardment ion thruster exhaust products on surfaces located downstream
Reynolds, T. W.↗
Acoustical measurements of the vortex noise for a rotating blade operating with and without its shed wake blown downstream
Acoustical measurements of vortex noise for rotating blade with and without shed wake blown downstream - tables
Hilton, D. A.↗
The effects of upstream mass injection on downstream heat transfer
Laminar boundary layer downstream heat transfer to sharp and blunt nosed isothermal flat plates under upstream mass injection, discussing insulating effect
Walker, W. F.↗
Exploratory tests on a downstream-cathode MPD thruster
Low power MPD arc thrustor performance with downstream cathode, using Xe propellant
Burkhart, J. A.↗
Calculation of relaxing turbulent boundary layers downstream of tangential slot injection
Turbulent boundary layers calculation downstream of compressible relaxing slot injection flows, using finite difference method based on eddy viscosity model
Bushnell, D. M.↗
Viscous slipstream flow downstream of a centerline Mach reflection
Viscous slipstream flow downstream of triple shock wave intersection in supersonic diffuser air flow, using Pitot and static pressure probe measurements
Back, L. H.↗
A model for analysis of the temperature field downstream of a heated jet injected into an isothermal crossflow at an angle of 90 deg
The temperature distribution downstream of a heated jet entering an isothermal crossflow at an angle of 90 deg is predicted using two conduction models with energy sources above the point of injection, in one case a point source and in the second a line source. The models use effective turbulent diffusivities that are determined empirically from previous measurements. Temperatures predicted by the models are compared to experimental results.
Eriksen, V. L.↗
Optical radiation from regions downstream of mercury bombardment thrusters
A 0.5 meter focal length, plane grating monochromator was used to measure the radiance of spectral radiation emanating from regions downstream of a mercury bombardment thruster. The wavelength range investigated was 2800 A. This radiation was due primarily to the radiative decay of excited mercury atoms exhausted from the thruster. Radiance values ranged from 10 to the minus 11th power to 10 to the minus 9th power W/sq cm sr, varying with wavelength. For resonant radiation, the spectral radiance may exceed 10 to the minus 8th power W/sq cm sr. From such radiance measurements, it was concluded that the thruster background radiation should not interfere with the control functions of a star tracker viewing through the thruster exhaust, provided that the tracker is designed to operate with a sufficiently small field of view.
Milder, N. L.↗