Design approaches and flow analysis techniques currently employed by aircraft engine manufacturers are assessed. Studies were performed to define the characteristics of aircraft and engines for civil missions of the 1990's and beyond. These studies, coupled with experience in recent years, identified the critical technologies needed to meet long range goals in fuel economy and other operating costs. Study results, recent and current research and development programs, and an estimate of future design and analytic capabilities are discussed
Turbine aerodynamic and cooling requirements for turbojet powered Mach 3 transport using methane fue
Cost/benefit studies were conducted on ten advanced material technologies applicable to small aircra...
Radial turbines have been used extensively in many applications including small ground based electri...
The design of a single stage axial-flow turbine with a tip diameter of 11.15 cm is presented. The de...
The design practices for the gas turbine are traced throughout history with particular emphasis on t...
Turbomachinery system component research to advance the technology of aviation turbofan and turbojet...
A cursory review is presented of some of the recent work that has been done in turbine aerodynamic r...
A brief description of the radial turbine and its analysis needs is followed by discussions of five ...
The advancement of small, cooled, radial inflow turbine technology in the area of operation at highe...
PaperPg. 90-104.The transformation between work and other forms of energy is accomplished in turboma...
The advancement of aeropropulsion systems continues to provide technology to various portions of the...
Technology areas related to gas turbine propulsion systems with potential for application to the aut...
A procedure for computing the rotor temperature and stress distributions in a cooled radial turbine ...
Experiments to determine the available increase in turbine horsepower achieved by increasing turbine...
A 74.5 kW(100 hp) advanced automotive gas turbine engine is described. A design iteration to improve...
Turbine aerodynamic and cooling requirements for turbojet powered Mach 3 transport using methane fue
Cost/benefit studies were conducted on ten advanced material technologies applicable to small aircra...
Radial turbines have been used extensively in many applications including small ground based electri...
The design of a single stage axial-flow turbine with a tip diameter of 11.15 cm is presented. The de...
The design practices for the gas turbine are traced throughout history with particular emphasis on t...
Turbomachinery system component research to advance the technology of aviation turbofan and turbojet...
A cursory review is presented of some of the recent work that has been done in turbine aerodynamic r...
A brief description of the radial turbine and its analysis needs is followed by discussions of five ...
The advancement of small, cooled, radial inflow turbine technology in the area of operation at highe...
PaperPg. 90-104.The transformation between work and other forms of energy is accomplished in turboma...
The advancement of aeropropulsion systems continues to provide technology to various portions of the...
Technology areas related to gas turbine propulsion systems with potential for application to the aut...
A procedure for computing the rotor temperature and stress distributions in a cooled radial turbine ...
Experiments to determine the available increase in turbine horsepower achieved by increasing turbine...
A 74.5 kW(100 hp) advanced automotive gas turbine engine is described. A design iteration to improve...
Turbine aerodynamic and cooling requirements for turbojet powered Mach 3 transport using methane fue
Cost/benefit studies were conducted on ten advanced material technologies applicable to small aircra...
Radial turbines have been used extensively in many applications including small ground based electri...