Add to ORKGThe design of a single stage axial-flow turbine with a tip diameter of 11.15 cm is presented. The design specifications are given, and the aerodynamic design procedure is described. The aerodynamic information includes the results of flow path, velocity diagram, and blade profile studies. Predicted off-design performance characteristics are also presented
A 74.5 kW(100 hp) advanced automotive gas turbine engine is described. A design iteration to improve...
An air cooled version of a single-stage, axial-flow turbine was investigated to determine aerodynami...
The turbine component of a gas turbine engine is the most costly component due to its complexity, an...
A single stage axial-flow turbine having a tip diameter of 15.41 centimeters was designed. The desig...
ABSTRACT An aerodynamic design study to configure a high efficiency industrial-size gas turbine comp...
A centrifugal compressor was designed for a gas turbine powered automobile as part of the Energy Res...
A single-stage axial-flow turbine was investigated to determine the effect of increased stator throa...
The aerodynamic performance of a redesigned compressor drive turbine of the gas turbine engine is de...
A vehicle concept study has been made to meet the requirements of the Large Civil Tilt Rotorcraft ve...
The aerodynamic design and rig test evaluation of a small counter-rotating turbine system is describ...
Design approaches and flow analysis techniques currently employed by aircraft engine manufacturers a...
In the operation of a mini-jet engine, the turbine plays a critical role of driving the compressor. ...
A solid blade version of a single-stage, axial-flow turbine was investigated to determine its perfor...
Results are presented for the design and development of an upgraded engine. The design incorporated ...
PaperPg. 90-104.The transformation between work and other forms of energy is accomplished in turboma...
A 74.5 kW(100 hp) advanced automotive gas turbine engine is described. A design iteration to improve...
An air cooled version of a single-stage, axial-flow turbine was investigated to determine aerodynami...
The turbine component of a gas turbine engine is the most costly component due to its complexity, an...
A single stage axial-flow turbine having a tip diameter of 15.41 centimeters was designed. The desig...
ABSTRACT An aerodynamic design study to configure a high efficiency industrial-size gas turbine comp...
A centrifugal compressor was designed for a gas turbine powered automobile as part of the Energy Res...
A single-stage axial-flow turbine was investigated to determine the effect of increased stator throa...
The aerodynamic performance of a redesigned compressor drive turbine of the gas turbine engine is de...
A vehicle concept study has been made to meet the requirements of the Large Civil Tilt Rotorcraft ve...
The aerodynamic design and rig test evaluation of a small counter-rotating turbine system is describ...
Design approaches and flow analysis techniques currently employed by aircraft engine manufacturers a...
In the operation of a mini-jet engine, the turbine plays a critical role of driving the compressor. ...
A solid blade version of a single-stage, axial-flow turbine was investigated to determine its perfor...
Results are presented for the design and development of an upgraded engine. The design incorporated ...
PaperPg. 90-104.The transformation between work and other forms of energy is accomplished in turboma...
A 74.5 kW(100 hp) advanced automotive gas turbine engine is described. A design iteration to improve...
An air cooled version of a single-stage, axial-flow turbine was investigated to determine aerodynami...
The turbine component of a gas turbine engine is the most costly component due to its complexity, an...