Add to ORKGOff design aerodynamic performance of the solid version of a cooled radial inflow turbine is analyzed. Rotor surface static pressure data and other performance parameters were obtained experimentally. Overall stage performance and turbine blade surface static to inlet total pressure ratios were calculated by using a quasi-three dimensional inviscid code. The off design prediction capability of this code for radial inflow turbines shows accurate static pressure prediction. Solutions show a difference of 3 to 5 points between the experimentally obtained efficiencies and the calculated values
A procedure for computing the rotor temperature and stress distributions in a cooled radial turbine ...
Radial-inflow turbines (RI turbines) are critical components of air cycle machines (ACM), utilized i...
Specific speed effects on radial inflow turbine performance using different rotor configuration
Two 14.4 inch tip diameter rotors were installed and tested in the Small Engines Component Turbine F...
An evaluation of the aerodynamic performance of the solid version of an Allison-designed cooled radi...
The aerodynamic performance of a solid uncooled version of a cooled radial turbine was evaluated in ...
The advancement of small, cooled, radial inflow turbine technology in the area of operation at highe...
The aerodynamic evaluation of two highly loaded compact radial turbine rotors was conducted at the N...
A brief description of the radial turbine and its analysis needs is followed by discussions of five ...
Radial turbines are commonly used in applications involving operation of the stage through severe o...
Instrumentation has been installed on the surface of a cooled radial-inflow turbine. Thermocouples a...
The aerodynamic design, the performance, and an internal loss breakdown were examined for a 15.04 cm...
An analysis of flow through a radial turbine rotor using the three-dimensional, thin-layer Navier-St...
An experimental aerodynamic evaluation of three compact radial turbine builds was performed. Two rot...
The three-dimensional inviscid DENTON code is used to analyze flow through a radial-inflow turbine r...
A procedure for computing the rotor temperature and stress distributions in a cooled radial turbine ...
Radial-inflow turbines (RI turbines) are critical components of air cycle machines (ACM), utilized i...
Specific speed effects on radial inflow turbine performance using different rotor configuration
Two 14.4 inch tip diameter rotors were installed and tested in the Small Engines Component Turbine F...
An evaluation of the aerodynamic performance of the solid version of an Allison-designed cooled radi...
The aerodynamic performance of a solid uncooled version of a cooled radial turbine was evaluated in ...
The advancement of small, cooled, radial inflow turbine technology in the area of operation at highe...
The aerodynamic evaluation of two highly loaded compact radial turbine rotors was conducted at the N...
A brief description of the radial turbine and its analysis needs is followed by discussions of five ...
Radial turbines are commonly used in applications involving operation of the stage through severe o...
Instrumentation has been installed on the surface of a cooled radial-inflow turbine. Thermocouples a...
The aerodynamic design, the performance, and an internal loss breakdown were examined for a 15.04 cm...
An analysis of flow through a radial turbine rotor using the three-dimensional, thin-layer Navier-St...
An experimental aerodynamic evaluation of three compact radial turbine builds was performed. Two rot...
The three-dimensional inviscid DENTON code is used to analyze flow through a radial-inflow turbine r...
A procedure for computing the rotor temperature and stress distributions in a cooled radial turbine ...
Radial-inflow turbines (RI turbines) are critical components of air cycle machines (ACM), utilized i...
Specific speed effects on radial inflow turbine performance using different rotor configuration