The turbine developed design specific work output at design speed at a total pressure ratio of 6.745 with a corresponding efficiency of 0.855. The efficiency (0.855)was 3.1 points lower than the estimated efficiency quoted by the contractor in the design report and 0.7 of a point lower than that determined by a reference prediction method. The performance of the turbine, which was a forced vortex design, agreed with the performance determined by the prediction method to about the same extent as did the performance of three reference high stage loading factor turbines, which were free vortex designs
Performance was obtained over a range of speeds and pressure ratios for a 0.4 linear scale version o...
An air cooled version of a single-stage, axial-flow turbine was investigated to determine aerodynami...
The stator areas of the design two-stage turbine were both decreased and increased by nominally 30 p...
The stage group performance of a 4 1/2 stage turbine with an average stage loading factor of 4.66 an...
The stage work distribution among the three stages was very close to the design value. The specific ...
The experimental test program results of a 4 1/2-stage turbine with a very high stage loading factor...
A solid version of a 50.8 cm single stage core turbine designed for high temperature was tested in c...
The efficiency of a two-stage turbine is discussed. The turbine efficiency was 0.932 for equivalent ...
An 8.00-in mean diameter two-stage turbine was investigated over a range of speeds from 0 to 110 per...
Partial admission performance was obtained for a 0.4 linear scale version of the LF460 lift fan turb...
Performance characteristics of high-weight flow, low pressure ratio, single stage turbine rotor and ...
Overall performance of stator component of cold air turbine determined for application to high tempe...
The results of the Task 1 and 2 turbine design work are reported. Preliminary design is discussed. B...
A solid blade version of a single-stage, axial-flow turbine was investigated to determine its perfor...
A single-stage axial-flow turbine was investigated to determine the effect of increased stator throa...
Performance was obtained over a range of speeds and pressure ratios for a 0.4 linear scale version o...
An air cooled version of a single-stage, axial-flow turbine was investigated to determine aerodynami...
The stator areas of the design two-stage turbine were both decreased and increased by nominally 30 p...
The stage group performance of a 4 1/2 stage turbine with an average stage loading factor of 4.66 an...
The stage work distribution among the three stages was very close to the design value. The specific ...
The experimental test program results of a 4 1/2-stage turbine with a very high stage loading factor...
A solid version of a 50.8 cm single stage core turbine designed for high temperature was tested in c...
The efficiency of a two-stage turbine is discussed. The turbine efficiency was 0.932 for equivalent ...
An 8.00-in mean diameter two-stage turbine was investigated over a range of speeds from 0 to 110 per...
Partial admission performance was obtained for a 0.4 linear scale version of the LF460 lift fan turb...
Performance characteristics of high-weight flow, low pressure ratio, single stage turbine rotor and ...
Overall performance of stator component of cold air turbine determined for application to high tempe...
The results of the Task 1 and 2 turbine design work are reported. Preliminary design is discussed. B...
A solid blade version of a single-stage, axial-flow turbine was investigated to determine its perfor...
A single-stage axial-flow turbine was investigated to determine the effect of increased stator throa...
Performance was obtained over a range of speeds and pressure ratios for a 0.4 linear scale version o...
An air cooled version of a single-stage, axial-flow turbine was investigated to determine aerodynami...
The stator areas of the design two-stage turbine were both decreased and increased by nominally 30 p...