Add to ORKGA centrifugal compressor was designed for a gas turbine powered automobile as part of the Energy Research and Development Agency program to demonstrate emissions characteristics that meet 1978 standards with fuel economy and acceleration which are competitive with conventionally powered vehicles. A backswept impeller was designed for the compressor in order to attain the efficiency goal range required for the objectives of this program. Details of the design and method of flow analysis of the compressor are presented
Overall performance of 6-inch radial-bladed centrifugal compressor with various diffuser vane settin...
Report presents the results of an investigation conducted to determine the nature and the extent of ...
PaperPg. 123-150.Any performance gain in a turbomachinery system requires some advancements in a num...
The design of a single stage axial-flow turbine with a tip diameter of 11.15 cm is presented. The de...
A single stage axial-flow turbine having a tip diameter of 15.41 centimeters was designed. The desig...
A 74.5 kW(100 hp) advanced automotive gas turbine engine is described. A design iteration to improve...
The objective of the NASA Energy Efficient Engine program is to identify and verify the technology r...
LecturePg. 91-100The natural gas and chemical processing industries have historically and necessaril...
The aerodynamic performance of the inlet manifold and stator assembly of the compressor drive turbin...
A vehicle concept study has been made to meet the requirements of the Large Civil Tilt Rotorcraft ve...
Program uses one-dimensional mean streamline analysis conducted at fixed stagnation conditions. Seve...
As the nation’s top user of energy, the U.S. Department of Defense (DOD) has initiated ways to becom...
The transport sector is one of many markets facing new challenges in the pursuit of reduced greenhou...
The aerodynamic performance of a redesigned compressor drive turbine of the gas turbine engine is de...
General Aviation will benefit from turbine engines that are both fuel-efficient and reliable. Curren...
Overall performance of 6-inch radial-bladed centrifugal compressor with various diffuser vane settin...
Report presents the results of an investigation conducted to determine the nature and the extent of ...
PaperPg. 123-150.Any performance gain in a turbomachinery system requires some advancements in a num...
The design of a single stage axial-flow turbine with a tip diameter of 11.15 cm is presented. The de...
A single stage axial-flow turbine having a tip diameter of 15.41 centimeters was designed. The desig...
A 74.5 kW(100 hp) advanced automotive gas turbine engine is described. A design iteration to improve...
The objective of the NASA Energy Efficient Engine program is to identify and verify the technology r...
LecturePg. 91-100The natural gas and chemical processing industries have historically and necessaril...
The aerodynamic performance of the inlet manifold and stator assembly of the compressor drive turbin...
A vehicle concept study has been made to meet the requirements of the Large Civil Tilt Rotorcraft ve...
Program uses one-dimensional mean streamline analysis conducted at fixed stagnation conditions. Seve...
As the nation’s top user of energy, the U.S. Department of Defense (DOD) has initiated ways to becom...
The transport sector is one of many markets facing new challenges in the pursuit of reduced greenhou...
The aerodynamic performance of a redesigned compressor drive turbine of the gas turbine engine is de...
General Aviation will benefit from turbine engines that are both fuel-efficient and reliable. Curren...
Overall performance of 6-inch radial-bladed centrifugal compressor with various diffuser vane settin...
Report presents the results of an investigation conducted to determine the nature and the extent of ...
PaperPg. 123-150.Any performance gain in a turbomachinery system requires some advancements in a num...