Add to ORKGOverall performance of stator component of cold air turbine determined for application to high temperature engine desig
Cascade investigation of cooling characteristics of air-cooled turbine blade for use in turboprop en...
The turbine developed design specific work output at design speed at a total pressure ratio of 6.745...
The aerodynamic performance of the inlet manifold and stator assembly of the compressor drive turbin...
Cold air study of high temperature gas turbine - blade feature effects on stator performanc
The stator areas of the design two-stage turbine were both decreased and increased by nominally 30 p...
The efficiency of a two-stage turbine is discussed. The turbine efficiency was 0.932 for equivalent ...
Cold-air tests to determine performance characteristics of single-stage turbine with stator blades e...
A single-stage axial-flow turbine was investigated to determine the effect of increased stator throa...
A solid, half-scale model of a 50.8-cm (20-in) research turbine designed for a high temperature core...
Cold air tests on axial flow turbine with transpiration cooled discrete hole stator blades to determ...
A solid version of a 50.8 cm single stage core turbine designed for high temperature was tested in c...
Performance of stator with wire mesh shell blading during cold air investigation of turbine with tra...
Single stage turbine operation with various stator cooling techniques and effects on stator, stage, ...
Performance tests of stator component in closed position and effects on performance of single stage ...
A solid blade version of a single-stage, axial-flow turbine was investigated to determine its perfor...
Cascade investigation of cooling characteristics of air-cooled turbine blade for use in turboprop en...
The turbine developed design specific work output at design speed at a total pressure ratio of 6.745...
The aerodynamic performance of the inlet manifold and stator assembly of the compressor drive turbin...
Cold air study of high temperature gas turbine - blade feature effects on stator performanc
The stator areas of the design two-stage turbine were both decreased and increased by nominally 30 p...
The efficiency of a two-stage turbine is discussed. The turbine efficiency was 0.932 for equivalent ...
Cold-air tests to determine performance characteristics of single-stage turbine with stator blades e...
A single-stage axial-flow turbine was investigated to determine the effect of increased stator throa...
A solid, half-scale model of a 50.8-cm (20-in) research turbine designed for a high temperature core...
Cold air tests on axial flow turbine with transpiration cooled discrete hole stator blades to determ...
A solid version of a 50.8 cm single stage core turbine designed for high temperature was tested in c...
Performance of stator with wire mesh shell blading during cold air investigation of turbine with tra...
Single stage turbine operation with various stator cooling techniques and effects on stator, stage, ...
Performance tests of stator component in closed position and effects on performance of single stage ...
A solid blade version of a single-stage, axial-flow turbine was investigated to determine its perfor...
Cascade investigation of cooling characteristics of air-cooled turbine blade for use in turboprop en...
The turbine developed design specific work output at design speed at a total pressure ratio of 6.745...
The aerodynamic performance of the inlet manifold and stator assembly of the compressor drive turbin...