Add to ORKGPerformance characteristics of high-weight flow, low pressure ratio, single stage turbine rotor and stator blade
Performance data in argon for small, low specific speed, ten stage turbine applicable to SNAP
Overall performance of stator component of cold air turbine determined for application to high tempe...
The stage group performance of a 4 1/2 stage turbine with an average stage loading factor of 4.66 an...
Partial admission performance of single stage supersonic turbine at low Reynolds number
The quasi-three-dimensional method for the aerodynamic design of both stator and rotor blades is pre...
An 8.00-in mean diameter two-stage turbine was investigated over a range of speeds from 0 to 110 per...
An experimental investigation of a highly loaded two-stage turbine with a downstream stator revealed...
Modifying the original turbine by closing down the first-rotor throat area and shrouding the first a...
Design of single-stage turbine for rotor entering at supersonic speed - performance characteristic
In order to insure satisfactory turbine performance under five turbojet-engine operating conditions,...
The over-all component performance characteristics of a J71 experimental three-stage turbine with 97...
A solid version of a 50.8 cm single stage core turbine designed for high temperature was tested in c...
The turbine developed design specific work output at design speed at a total pressure ratio of 6.745...
A single-stage axial-flow turbine was investigated to determine the effect of increased stator throa...
The experimental test program results of a 4 1/2-stage turbine with a very high stage loading factor...
Performance data in argon for small, low specific speed, ten stage turbine applicable to SNAP
Overall performance of stator component of cold air turbine determined for application to high tempe...
The stage group performance of a 4 1/2 stage turbine with an average stage loading factor of 4.66 an...
Partial admission performance of single stage supersonic turbine at low Reynolds number
The quasi-three-dimensional method for the aerodynamic design of both stator and rotor blades is pre...
An 8.00-in mean diameter two-stage turbine was investigated over a range of speeds from 0 to 110 per...
An experimental investigation of a highly loaded two-stage turbine with a downstream stator revealed...
Modifying the original turbine by closing down the first-rotor throat area and shrouding the first a...
Design of single-stage turbine for rotor entering at supersonic speed - performance characteristic
In order to insure satisfactory turbine performance under five turbojet-engine operating conditions,...
The over-all component performance characteristics of a J71 experimental three-stage turbine with 97...
A solid version of a 50.8 cm single stage core turbine designed for high temperature was tested in c...
The turbine developed design specific work output at design speed at a total pressure ratio of 6.745...
A single-stage axial-flow turbine was investigated to determine the effect of increased stator throa...
The experimental test program results of a 4 1/2-stage turbine with a very high stage loading factor...
Performance data in argon for small, low specific speed, ten stage turbine applicable to SNAP
Overall performance of stator component of cold air turbine determined for application to high tempe...
The stage group performance of a 4 1/2 stage turbine with an average stage loading factor of 4.66 an...