Add to ORKGDesign of single-stage turbine for rotor entering at supersonic speed - performance characteristic
PaperPg. 90-104.The transformation between work and other forms of energy is accomplished in turboma...
The results of the Task 1 and 2 turbine design work are reported. Preliminary design is discussed. B...
Efficiency evaluation of two-stage turbine with low ratio of blade to jet speed suitable for bleed-t...
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
Performance characteristics and efficiency determined for air cooled turbojet engine suitable for su...
Methods for designing supersonic stator and rotor blading corrected for boundary layer displacement ...
The quasi-three-dimensional method for the aerodynamic design of both stator and rotor blades is pre...
The experimental test program results of a 4 1/2-stage turbine with a very high stage loading factor...
The experimental performance of a modified turbine for driving a supersonic compressor is presented ...
An experimental investigation of a highly loaded two-stage turbine with a downstream stator revealed...
The over-all component performance characteristics of a J71 experimental three-stage turbine with 97...
Modifying the original turbine by closing down the first-rotor throat area and shrouding the first a...
Investigation of high subsonic turbine with high rotor blade suction-surface diffusio
PaperPg. 90-104.The transformation between work and other forms of energy is accomplished in turboma...
PaperPg. 90-104.The transformation between work and other forms of energy is accomplished in turboma...
The results of the Task 1 and 2 turbine design work are reported. Preliminary design is discussed. B...
Efficiency evaluation of two-stage turbine with low ratio of blade to jet speed suitable for bleed-t...
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
Performance characteristics and efficiency determined for air cooled turbojet engine suitable for su...
Methods for designing supersonic stator and rotor blading corrected for boundary layer displacement ...
The quasi-three-dimensional method for the aerodynamic design of both stator and rotor blades is pre...
The experimental test program results of a 4 1/2-stage turbine with a very high stage loading factor...
The experimental performance of a modified turbine for driving a supersonic compressor is presented ...
An experimental investigation of a highly loaded two-stage turbine with a downstream stator revealed...
The over-all component performance characteristics of a J71 experimental three-stage turbine with 97...
Modifying the original turbine by closing down the first-rotor throat area and shrouding the first a...
Investigation of high subsonic turbine with high rotor blade suction-surface diffusio
PaperPg. 90-104.The transformation between work and other forms of energy is accomplished in turboma...
PaperPg. 90-104.The transformation between work and other forms of energy is accomplished in turboma...
The results of the Task 1 and 2 turbine design work are reported. Preliminary design is discussed. B...
Efficiency evaluation of two-stage turbine with low ratio of blade to jet speed suitable for bleed-t...