EFFECT OF DISSOCIATION ON EXHAUST-NOZZLE PERFORMANCE
Effect of dissociation on exhaust nozzle performance
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Effect of dissociation on exhaust nozzle performance
Investigation of air-cooled, plug-type, variable- area exhaust nozzle at high temperature
Exhaust jets - manned space flight
Achieving noise suppression & high thrust performance with plug-type exhaust nozzles for supersonic transports
Exhaust nozzle recombination for hydrogen-fueled subsonic combustion ramjet engines
Effect of exhaust nozzle recombination on hypersonic ramjet performance
Exhaust nozzle recombination of hydrogen fuel in subsonic ramjet engines at hypersonic speeds
Exhaust nozzle testing using cold air flow to find effect of exit design on thrust & jet wake dynamic pressure for use in vtol downwash suppression
In recent months there has been interest in the problem of the impingement of a jet exhaust on simulated lunar surfaces. The problem has been described both experimentally and theoretically. In the June issue of the AIAA Journal there appeared two Technical Notes that seemed to complicate unnecessarily the analysis of the free-jet expansion and the surface pressure distribution. The purpose of the present comment is to recall briefly the simple results of the theory and to make a more complete comparison with the experiniental data of Ref. 1
Effects of ion engine exhaust fluctuations on signal phase and amplitude modulation in antenna radiation field
Base heating by radiation from exhaust gases
Environmental exposure for fuel and exhaust products with preliminary estimates
Simulated rocket jet exhaust effect on stability and control of research aircraft configuration
Investigation on size and density of boric oxide exhaust cloud of turbojet engine operating on trimethylborate fuel
Base pressures and convective heat transfer coefficients for clustered sonic nozzles with emphasis on choked exhaust backflow
Exhaust backflow from simulated cluster of three wide-spaced rocket nozzles in near-space environment
Electron density and temperature profiles measured in exhaust of magnetoplasma-dynamic source
Exhaust of pinched plasma from axial orifice involves electromagnetic current profile diffraction and thermal expansion of gas column