Add to ORKGMolecular sink facility and 25-foot space simulator have been used to distinguish nature of exhaust plumes from nozzles with relatively large internal boundary layer flow. Plume density has been measured by electron beam/photomultiplier system
Measurements of mass flux and flow angle were taken throughout the forward flow region of the exhaus...
An experimental aerodynamic investigation was conducted to provide data for studies to determine the...
Interactions of model rocket plumes and the free stream at varying simulated altitudes have been inv...
A space simulation procedure was developed for studying rocket plume contamination effects using a 5...
As a part of the electrothermal propulsion plume research program at the NASA Lewis Research Center,...
Computer program determines the radiant flux to the base region of a real gas system with an axisymm...
Pitot pressures and flow angles are measured in the plume of a nozzle flowing nitrogen and exhaustin...
Thermal radiation from the plume of any solid rocket motor, containing aluminum as one of the propel...
Quantitative evidence of gas flows in the far upstream region of small nozzles with large boundary l...
A miniature solid propellant rocket motor has been developed to be used in a program to determine th...
The self-induced molecular contamination around the space station could have adverse effects on spac...
Since exhaust plumes affect vehicle base environment (pressure and heat loads) and the orbiter vehic...
Exhaust plume shape simulation is studied, with the major effort directed toward computer program de...
Results are summarized of various analyses of the exhaust plumes of the space shuttle. Specific topi...
A series of tests were conducted to measure the mass flux in the far field of a nozzle plume in a hi...
Measurements of mass flux and flow angle were taken throughout the forward flow region of the exhaus...
An experimental aerodynamic investigation was conducted to provide data for studies to determine the...
Interactions of model rocket plumes and the free stream at varying simulated altitudes have been inv...
A space simulation procedure was developed for studying rocket plume contamination effects using a 5...
As a part of the electrothermal propulsion plume research program at the NASA Lewis Research Center,...
Computer program determines the radiant flux to the base region of a real gas system with an axisymm...
Pitot pressures and flow angles are measured in the plume of a nozzle flowing nitrogen and exhaustin...
Thermal radiation from the plume of any solid rocket motor, containing aluminum as one of the propel...
Quantitative evidence of gas flows in the far upstream region of small nozzles with large boundary l...
A miniature solid propellant rocket motor has been developed to be used in a program to determine th...
The self-induced molecular contamination around the space station could have adverse effects on spac...
Since exhaust plumes affect vehicle base environment (pressure and heat loads) and the orbiter vehic...
Exhaust plume shape simulation is studied, with the major effort directed toward computer program de...
Results are summarized of various analyses of the exhaust plumes of the space shuttle. Specific topi...
A series of tests were conducted to measure the mass flux in the far field of a nozzle plume in a hi...
Measurements of mass flux and flow angle were taken throughout the forward flow region of the exhaus...
An experimental aerodynamic investigation was conducted to provide data for studies to determine the...
Interactions of model rocket plumes and the free stream at varying simulated altitudes have been inv...