Add to ORKGCold-air tests to determine performance characteristics of single-stage turbine with stator blades employing transpiration coolant ejection through wire mesh shel
The effect of coolant discharge on the aerodynamic performance of a film cooled turbine stator blade...
The efficiency of a two-stage turbine is discussed. The turbine efficiency was 0.932 for equivalent ...
Previously published experimental aerodynamic efficiency results for a film cooled turbine stator bl...
Cold air tests on axial flow turbine with transpiration cooled discrete hole stator blades to determ...
Performance of stator with wire mesh shell blading during cold air investigation of turbine with tra...
Tests were made on a 0.762-meter-tip-diameter research turbine to determine the effect of blade cool...
Single stage turbine operation with various stator cooling techniques and effects on stator, stage, ...
Trailing-edge slot configurations were investigated in a two-dimensional cascade of turbine stator b...
Experimentally determined efficiencies of turbine stator blades having trailing-edge coolant ejectio...
An air cooled version of a single-stage, axial-flow turbine was investigated to determine aerodynami...
Overall performance of stator component of cold air turbine determined for application to high tempe...
Cold air study of high temperature gas turbine - blade feature effects on stator performanc
A solid blade version of a single-stage, axial-flow turbine was investigated to determine its perfor...
The effect of film coolant ejection from the pressure side of a stator blade was determined in a two...
Published experimental aerodynamic efficiency results were compared with results predicted from two ...
The effect of coolant discharge on the aerodynamic performance of a film cooled turbine stator blade...
The efficiency of a two-stage turbine is discussed. The turbine efficiency was 0.932 for equivalent ...
Previously published experimental aerodynamic efficiency results for a film cooled turbine stator bl...
Cold air tests on axial flow turbine with transpiration cooled discrete hole stator blades to determ...
Performance of stator with wire mesh shell blading during cold air investigation of turbine with tra...
Tests were made on a 0.762-meter-tip-diameter research turbine to determine the effect of blade cool...
Single stage turbine operation with various stator cooling techniques and effects on stator, stage, ...
Trailing-edge slot configurations were investigated in a two-dimensional cascade of turbine stator b...
Experimentally determined efficiencies of turbine stator blades having trailing-edge coolant ejectio...
An air cooled version of a single-stage, axial-flow turbine was investigated to determine aerodynami...
Overall performance of stator component of cold air turbine determined for application to high tempe...
Cold air study of high temperature gas turbine - blade feature effects on stator performanc
A solid blade version of a single-stage, axial-flow turbine was investigated to determine its perfor...
The effect of film coolant ejection from the pressure side of a stator blade was determined in a two...
Published experimental aerodynamic efficiency results were compared with results predicted from two ...
The effect of coolant discharge on the aerodynamic performance of a film cooled turbine stator blade...
The efficiency of a two-stage turbine is discussed. The turbine efficiency was 0.932 for equivalent ...
Previously published experimental aerodynamic efficiency results for a film cooled turbine stator bl...