The efficiency of a two-stage turbine is discussed. The turbine efficiency was 0.932 for equivalent design operating conditions (speed) and specific work, which compares closely to the value of 0.929 that would be estimated using the first-stage efficiency. The mass flow obtained with the two-stage configuration indicated that the mass flow characteristics of the two stages were closely matched at design operating conditions. The stage work split at these conditions was 0.505-0.495, which was close to the design work split of 0.515-0.485
An air cooled version of a single-stage, axial-flow turbine was investigated to determine aerodynami...
Cold air tests on axial flow turbine with transpiration cooled discrete hole stator blades to determ...
A single-stage axial-flow turbine was investigated to determine the effect of increased stator throa...
The stator areas of the design two-stage turbine were both decreased and increased by nominally 30 p...
An 8.00-in mean diameter two-stage turbine was investigated over a range of speeds from 0 to 110 per...
A solid version of a 50.8 cm single stage core turbine designed for high temperature was tested in c...
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
The stage group performance of a 4 1/2 stage turbine with an average stage loading factor of 4.66 an...
Flow analysis to determine turbine efficiency as function of inlet temperature for two stage turbin
An experimental investigation of a highly loaded two-stage turbine with a downstream stator revealed...
Tests were made on a 0.762-meter-tip-diameter research turbine to determine the effect of blade cool...
Cold-air tests to determine performance characteristics of single-stage turbine with stator blades e...
The turbine developed design specific work output at design speed at a total pressure ratio of 6.745...
A solid, half-scale model of a 50.8-cm (20-in) research turbine designed for a high temperature core...
An air cooled version of a single-stage, axial-flow turbine was investigated to determine aerodynami...
Cold air tests on axial flow turbine with transpiration cooled discrete hole stator blades to determ...
A single-stage axial-flow turbine was investigated to determine the effect of increased stator throa...
The stator areas of the design two-stage turbine were both decreased and increased by nominally 30 p...
An 8.00-in mean diameter two-stage turbine was investigated over a range of speeds from 0 to 110 per...
A solid version of a 50.8 cm single stage core turbine designed for high temperature was tested in c...
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
The stage group performance of a 4 1/2 stage turbine with an average stage loading factor of 4.66 an...
Flow analysis to determine turbine efficiency as function of inlet temperature for two stage turbin
An experimental investigation of a highly loaded two-stage turbine with a downstream stator revealed...
Tests were made on a 0.762-meter-tip-diameter research turbine to determine the effect of blade cool...
Cold-air tests to determine performance characteristics of single-stage turbine with stator blades e...
The turbine developed design specific work output at design speed at a total pressure ratio of 6.745...
A solid, half-scale model of a 50.8-cm (20-in) research turbine designed for a high temperature core...
An air cooled version of a single-stage, axial-flow turbine was investigated to determine aerodynami...
Cold air tests on axial flow turbine with transpiration cooled discrete hole stator blades to determ...
A single-stage axial-flow turbine was investigated to determine the effect of increased stator throa...