Device for suppressing sound and heat produced by high-velocity exhaust jets Patent
Device for adding water to high velocity exhaust jets to reduce velocity, noise, and temperature
Kramer, F.↗
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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Scaling parameters for the simulation of highly expanded rocket exhaust plumes and the resultant impingement forces on an immersed body
Scaling parameters for simulating highly expanded rocket exhaust plumes and resultant impingement forces on immersed bodies
Stephens, J. T.↗
Propellant condensation on surfaces near an electric rocket exhaust
Propellant condensation on surfaces near electric rocket exhaust, calculating particle arrival rates, backflow and desorption energies
Reynolds, T. W.↗
The Mach disc in underexpanded exhaust plumes
Mach disk in underexpanded exhaust plume predicted by dividing flow field into subregions
Abbett, M.↗
Electrostatic rocket exhaust effects on solar- electric spacecraft subsystems
Electrostatic rocket exhaust condensation on spacecraft solar electric panels cover glasses, noting deleterious effects
Hall, D. F.↗
Prediction of radiation from rocket exhaust gases
Rocket exhaust gases radiant heat transfer prediction, using band models with computer program
Reardon, J. E.↗
Exhaust plume convective heat transfer measurements from a space firing of the ATS rocket motor
ATS-C satellite rocket exhaust plume convective heating measurements of VHF whip antennas, discussing nozzle flow and heating rate
Fehr, R. W.↗
Analysis of liquid rocket propellant engine exhaust plumes
Liquid rocket propellant engine exhaust plume flow field, discussing mathematical models for combustion chamber, throat region and nozzle
Greenwood, T.↗
Thruster exhaust effects upon spacecraft
Thrustor exhaust effluent characteristics relating to spacecraft contamination
Lyon, W. C.↗
Exhaust characteristics of a megawatt nitrogen MPD-ARC thruster
Exhaust velocity, electron density and temperature of pulsed megawatt nitrogen MPD-ARC thrustor, using Thomson scattering of pulsed laser light
Michels, C. J.↗
Flight and wind tunnel investigation of installation effects on underwing supersonic cruise exhaust nozzles at transonic speeds
Airframe installation effects at transonic speeds on underwing supersonic cruise exhaust nozzles, using flight and wind tunnel tests
Blaha, B. J.↗
Hydrogen peroxide motor exhaust heating to components at cryogenic temperatures in the vacuum of space
Temperature measurement on thin steel shield subjected to hydrogen peroxide motor exhaust heating at cryogenic temperatures in space
Pleasant, R. L.↗
Carbon monoxide oxidation rates computed for automobile exhaust manifold reactor conditions
Carbon monoxide oxidation rates for automobile exhaust manifold reactor conditions
Bittker, D. A.↗
Pressure measurements in the exhaust of a pulsed megawatt MPD arc thruster
Exhaust pressure measurements on pulsed magnetoplasmadynamic arc thrustor
Michels, C. J.↗
Investigation of engine-exhaust-airframe interference on a cruise vehicle at Mach 6
Investigation of engine-exhaust-airframe interference on cruise vehicle at Mach 6
Cubbage, J. M.↗
Engine exhaust noise during ground operation of the XB-70 airplane
Measurement of engine exhaust noise during ground operation of XB-70 aircraft
Lasagna, P. L.↗
Flow field resulting from forward-facing nozzles exhausting near a large cylindrical body at free-stream Mach numbers of 3.0, 4.5, and 6.0
Measurement of flow distribution caused by forward facing nozzles exhausting near large cylindrical body at hypersonic speed
Martin, J. A.↗
Application of moderate resolution band models to the prediction of heat transfer from rocket exhaust plumes
Computer program for resolution band model prediction of heat transfer from rocket exhaust plumes
Mc Kay, G. B.↗