Add to ORKGPerformance of single stage, axial flow turbine designed for Brayton cycle space power syste
The results of the Task 1 and 2 turbine design work are reported. Preliminary design is discussed. B...
A single-stage axial-flow turbine was investigated to determine the effect of increased stator throa...
Performance characteristics of high-weight flow, low pressure ratio, single stage turbine rotor and ...
An 8.00-in mean diameter two-stage turbine was investigated over a range of speeds from 0 to 110 per...
Design of single-stage turbine for rotor entering at supersonic speed - performance characteristic
Performance data in argon for small, low specific speed, ten stage turbine applicable to SNAP
Modifying the original turbine by closing down the first-rotor throat area and shrouding the first a...
High-altitude turbojet performance is adversely affected by the effects of low air density. This per...
The quasi-three-dimensional method for the aerodynamic design of both stator and rotor blades is pre...
An experimental investigation of a highly loaded two-stage turbine with a downstream stator revealed...
Experimental data from jet-engine tests have indicated that unsteady blade row interactions and sepa...
The experimental test program results of a 4 1/2-stage turbine with a very high stage loading factor...
A comprehensive test program was performed in the Propulsion Systems Laboratory at the NASA Glenn Re...
An experimental investigation of the stage performance of the J71 three-stage turbine at design spee...
Performance of single stage, axial flow turbine designed for Brayton cycle space power syste
The results of the Task 1 and 2 turbine design work are reported. Preliminary design is discussed. B...
A single-stage axial-flow turbine was investigated to determine the effect of increased stator throa...
Performance characteristics of high-weight flow, low pressure ratio, single stage turbine rotor and ...
An 8.00-in mean diameter two-stage turbine was investigated over a range of speeds from 0 to 110 per...
Design of single-stage turbine for rotor entering at supersonic speed - performance characteristic
Performance data in argon for small, low specific speed, ten stage turbine applicable to SNAP
Modifying the original turbine by closing down the first-rotor throat area and shrouding the first a...
High-altitude turbojet performance is adversely affected by the effects of low air density. This per...
The quasi-three-dimensional method for the aerodynamic design of both stator and rotor blades is pre...
An experimental investigation of a highly loaded two-stage turbine with a downstream stator revealed...
Experimental data from jet-engine tests have indicated that unsteady blade row interactions and sepa...
The experimental test program results of a 4 1/2-stage turbine with a very high stage loading factor...
A comprehensive test program was performed in the Propulsion Systems Laboratory at the NASA Glenn Re...
An experimental investigation of the stage performance of the J71 three-stage turbine at design spee...
Performance of single stage, axial flow turbine designed for Brayton cycle space power syste
The results of the Task 1 and 2 turbine design work are reported. Preliminary design is discussed. B...
A single-stage axial-flow turbine was investigated to determine the effect of increased stator throa...