Add to ORKGThe stage group performance of a 4 1/2 stage turbine with an average stage loading factor of 4.66 an...
An experimental investigation of the stage performance of the J71 three-stage turbine at design spee...
Experimental performance evaluation of radial inflow turbine over range of inlet total pressur
Performance characteristics of high-weight flow, low pressure ratio, single stage turbine rotor and ...
Partial admission performance of single stage supersonic turbine at low Reynolds number
An 8.00-in mean diameter two-stage turbine was investigated over a range of speeds from 0 to 110 per...
Performance of single stage, axial flow turbine designed for Brayton cycle space power syste
The experimental test program results of a 4 1/2-stage turbine with a very high stage loading factor...
An experimental investigation of a highly loaded two-stage turbine with a downstream stator revealed...
The overall performance of an existing high-ratio turbine is calculated analytically over a range of...
Cold performance characteristics of small radial inflow turbine designed for Brayton cycle power sys...
The turbine developed design specific work output at design speed at a total pressure ratio of 6.745...
The over-all component performance characteristics of a J71 experimental three-stage turbine with 97...
The aerodynamic design and rig test evaluation of a small counter-rotating turbine system is describ...
Cold argon and air performance of 6.02 inch radial inflow turbine designed for 10 kilowatt shaft out...
The stage group performance of a 4 1/2 stage turbine with an average stage loading factor of 4.66 an...
An experimental investigation of the stage performance of the J71 three-stage turbine at design spee...
Experimental performance evaluation of radial inflow turbine over range of inlet total pressur
Performance characteristics of high-weight flow, low pressure ratio, single stage turbine rotor and ...
Partial admission performance of single stage supersonic turbine at low Reynolds number
An 8.00-in mean diameter two-stage turbine was investigated over a range of speeds from 0 to 110 per...
Performance of single stage, axial flow turbine designed for Brayton cycle space power syste
The experimental test program results of a 4 1/2-stage turbine with a very high stage loading factor...
An experimental investigation of a highly loaded two-stage turbine with a downstream stator revealed...
The overall performance of an existing high-ratio turbine is calculated analytically over a range of...
Cold performance characteristics of small radial inflow turbine designed for Brayton cycle power sys...
The turbine developed design specific work output at design speed at a total pressure ratio of 6.745...
The over-all component performance characteristics of a J71 experimental three-stage turbine with 97...
The aerodynamic design and rig test evaluation of a small counter-rotating turbine system is describ...
Cold argon and air performance of 6.02 inch radial inflow turbine designed for 10 kilowatt shaft out...
The stage group performance of a 4 1/2 stage turbine with an average stage loading factor of 4.66 an...
An experimental investigation of the stage performance of the J71 three-stage turbine at design spee...
Experimental performance evaluation of radial inflow turbine over range of inlet total pressur