An experimental invesitgation of the effect of increasing the first-stator area of the J71-97 experimental three-stage turbine from 97 percent of design to 132 percent revealed (1) the maximum efficiency obtained decreased from 0.891 to 0.869, (2) the choking equivalent weight flows increased by approximately 13.6 percent, and (3) at the turbine match points required to maintain the compressor at constant design equivalent conditions the turbine efficiency decreased from 0.87 to 0.86
Performance tests of stator component in closed position and effects on performance of single stage ...
Adjustable-stator turbines are applied to turbojet engines and probable performance is compared with...
The over-all component performance character is t ics of the 5 7 1 Type I I A three-stage turbine we...
Results of a survey investigation of the J71-97 experimental three-stage turbine equipped with a fir...
The over-all component performance characteristics of a J71 experimental three-stage turbine with 97...
The performance results, as well as a compressor-turbine match point study based on a particular mod...
An experimental investigation of the stage performance of the J71 three-stage turbine at design spee...
An experimental invesitgation of the effect of increasing the first-stator area of the J71-97 experi...
The over-all component performance characteristics of a J71 experimental three-stage turbine with 97...
The performance of a turbojet engine with a two-stage turbine, an adjustable first-stage turbine sta...
The stator areas of the design two-stage turbine were both decreased and increased by nominally 30 p...
Modifying the original turbine by closing down the first-rotor throat area and shrouding the first a...
Variable stator area effect on performance of single stage turbine suitable for air coolin
The experimental performance of a modified turbine for driving a supersonic compressor is presented ...
A single-stage axial-flow turbine was investigated to determine the effect of increased stator throa...
Performance tests of stator component in closed position and effects on performance of single stage ...
Adjustable-stator turbines are applied to turbojet engines and probable performance is compared with...
The over-all component performance character is t ics of the 5 7 1 Type I I A three-stage turbine we...
Results of a survey investigation of the J71-97 experimental three-stage turbine equipped with a fir...
The over-all component performance characteristics of a J71 experimental three-stage turbine with 97...
The performance results, as well as a compressor-turbine match point study based on a particular mod...
An experimental investigation of the stage performance of the J71 three-stage turbine at design spee...
An experimental invesitgation of the effect of increasing the first-stator area of the J71-97 experi...
The over-all component performance characteristics of a J71 experimental three-stage turbine with 97...
The performance of a turbojet engine with a two-stage turbine, an adjustable first-stage turbine sta...
The stator areas of the design two-stage turbine were both decreased and increased by nominally 30 p...
Modifying the original turbine by closing down the first-rotor throat area and shrouding the first a...
Variable stator area effect on performance of single stage turbine suitable for air coolin
The experimental performance of a modified turbine for driving a supersonic compressor is presented ...
A single-stage axial-flow turbine was investigated to determine the effect of increased stator throa...
Performance tests of stator component in closed position and effects on performance of single stage ...
Adjustable-stator turbines are applied to turbojet engines and probable performance is compared with...
The over-all component performance character is t ics of the 5 7 1 Type I I A three-stage turbine we...