Add to ORKGA wind tunnel investigation was conducted to determine the performance of a 4000-pound-thrust axial-flow turbojet engine with a high flow compressor. Pressure altitudes included 5000 to 40000 feet with ram pressure ratios from 1.00 to 1.82. Altitudes included 20000 to 40000 feet and ram pressure ratios from 1.09 to 1.75. A comparison is made between engine performance with high flow and low flow compressors
An investigation to determine the performance and operational characteristics of an axial-flow gas t...
A preliminary investigation of an axial-flow gas turbine-propeller engine was conduxted. Performance...
Performance properties and operational characteristics of an axial-flow gas turbine-propeller engine...
The results of altitude-wind-tunnel tests conducted to determine the performance of an axial-flow-ty...
A wind tunnel investigation was conducted to determine the performance of a 4000-pound-thrust axial-...
Performance characteristics of the turbine of a 4000-pound-thrust axial-flow turbojet engine was det...
Combustion chamber performance properties of a 3000-pound-thrust axial-flow turbojet engine were det...
An investigation was conducted to evaluate the operational characteristics of a 3000 pound thrust ax...
An investigation has been conducted in the NACA Cleveland altitude wind tunnel to evaluate the perfo...
A wind tunnel investigation was conducted to determine the performance of a turbine operating as an ...
Temperature and pressure distributions for an original and modified 3000 pound thrust axial flow tur...
The results of altitude-wind-tunnel tests conducted to determine the performance of an axial-flow-ty...
As part of an investigation of the performance and operational characteristics of the axial-flow gas...
An investigation was conducted in the Cleveland altitude wind tunnel to determine the operational ch...
Performance characteristics of the turbine of a 4000-pound-thrust axial-flow turbojet engine was det...
An investigation to determine the performance and operational characteristics of an axial-flow gas t...
A preliminary investigation of an axial-flow gas turbine-propeller engine was conduxted. Performance...
Performance properties and operational characteristics of an axial-flow gas turbine-propeller engine...
The results of altitude-wind-tunnel tests conducted to determine the performance of an axial-flow-ty...
A wind tunnel investigation was conducted to determine the performance of a 4000-pound-thrust axial-...
Performance characteristics of the turbine of a 4000-pound-thrust axial-flow turbojet engine was det...
Combustion chamber performance properties of a 3000-pound-thrust axial-flow turbojet engine were det...
An investigation was conducted to evaluate the operational characteristics of a 3000 pound thrust ax...
An investigation has been conducted in the NACA Cleveland altitude wind tunnel to evaluate the perfo...
A wind tunnel investigation was conducted to determine the performance of a turbine operating as an ...
Temperature and pressure distributions for an original and modified 3000 pound thrust axial flow tur...
The results of altitude-wind-tunnel tests conducted to determine the performance of an axial-flow-ty...
As part of an investigation of the performance and operational characteristics of the axial-flow gas...
An investigation was conducted in the Cleveland altitude wind tunnel to determine the operational ch...
Performance characteristics of the turbine of a 4000-pound-thrust axial-flow turbojet engine was det...
An investigation to determine the performance and operational characteristics of an axial-flow gas t...
A preliminary investigation of an axial-flow gas turbine-propeller engine was conduxted. Performance...
Performance properties and operational characteristics of an axial-flow gas turbine-propeller engine...