The experimental and analytical results to date of a study of a two-component gaseous vortex system are presented in this paper. Analytical expressions for tangential velocity and static-pressure profiles in a turbulent vortex show good agreement with experimental data. Airflow rates from 0.075 to 0.14 pound per second and corresponding tangential velocities from 160 to 440 feet per second are correlated by turbulent Reynolds numbers from 1.95 to 2.4. An analysis of an air-bromine gas mixture in a turbulent vortex indicates that a boundary value of bromine-to-air radial velocity ratio (u(2)/u(1)) of 0.999 gives essentially no bromine buildup, while a value of 0.833 results in considerable separation. For a constant value of (u(2)/u(1))(0) t...
Combustion driven hypersonic and supersonic wind tunnels are impaired in their flight simulation abi...
A unique normalized radial pressure profile characterizes the bed of a gas-solid vortex reactor over...
The vortex tube is a very simple device which separates a compressed gas into a cold and a hot stre...
An experimental investigation into the gas dynamics of a jet-driven vortex tube for application of a...
Binary vortex flow fields used as gaseous-fuel- retention devices for gas-core nuclear reactor
The ability of mixing length theory to correlate vortex data is evaluated. Expressions are derived f...
Heavy gas concentration in light gas vortices for heated and unheated vortex flow
An analysis was made to determine the maximum powerplant thrust-to-weight ratio possible with a sing...
Analytical investigations of fluid dynamics problems of relevance to the gaseous core nuclear reacto...
The nuclear rocket is potentially capable of much higher specific impulse than any chemically fuele...
Fuel retention, flow characteristics, and transparence of materials studied as part of gaseous nucle...
A unique normalized radial pressure profile characterizes the bed of a gas-solid vortex reactor over...
AbstractA three-dimensional numerical analysis of the flow in a Gas-Solid Vortex Unit (GSVU) is carr...
Fluid mechanical effects on combustion processes in steady flow combustors, especially gas turbine c...
The vortex tube is a very simple device which separates a compressed gas into a cold and a hot stre...
Combustion driven hypersonic and supersonic wind tunnels are impaired in their flight simulation abi...
A unique normalized radial pressure profile characterizes the bed of a gas-solid vortex reactor over...
The vortex tube is a very simple device which separates a compressed gas into a cold and a hot stre...
An experimental investigation into the gas dynamics of a jet-driven vortex tube for application of a...
Binary vortex flow fields used as gaseous-fuel- retention devices for gas-core nuclear reactor
The ability of mixing length theory to correlate vortex data is evaluated. Expressions are derived f...
Heavy gas concentration in light gas vortices for heated and unheated vortex flow
An analysis was made to determine the maximum powerplant thrust-to-weight ratio possible with a sing...
Analytical investigations of fluid dynamics problems of relevance to the gaseous core nuclear reacto...
The nuclear rocket is potentially capable of much higher specific impulse than any chemically fuele...
Fuel retention, flow characteristics, and transparence of materials studied as part of gaseous nucle...
A unique normalized radial pressure profile characterizes the bed of a gas-solid vortex reactor over...
AbstractA three-dimensional numerical analysis of the flow in a Gas-Solid Vortex Unit (GSVU) is carr...
Fluid mechanical effects on combustion processes in steady flow combustors, especially gas turbine c...
The vortex tube is a very simple device which separates a compressed gas into a cold and a hot stre...
Combustion driven hypersonic and supersonic wind tunnels are impaired in their flight simulation abi...
A unique normalized radial pressure profile characterizes the bed of a gas-solid vortex reactor over...
The vortex tube is a very simple device which separates a compressed gas into a cold and a hot stre...