Improved turbine durability and performance and reduced development cost will all result from impoved methods of predicting turbine metal temperatures. Better metal temperature prediction methods require improvements in the methods of predicting the hot gas flow over the turbine airfoils and the cooling air flow inside the airfoil and in the methods of predicting the heat transfer rates on both the hot gas side and coolant side of the airfoil. The overall HOST Turbine Heat Transfer effort is directed at improving all four of these areas of concern
NASA is sponsoring the Turbine Engine Hot Section Technology (HOST) Project to address the need for ...
The efficiency and power output of the gas turbine is impacted directly by the maximum gas temperatu...
This work is motivated by the need to accurately predict heat transfer in turbomachinery. For effici...
Improvements in methods for predicting heat transfer rates on the hot gas side of turbine airfoils a...
The objectives of the NASA Hot Section Technology (HOST) Turbine Heat Transfer subproject were to ob...
The thermal design of the combustor and turbine of a gas turbine engine poses a number of difficult ...
Increased attention to fuel economy and increased thrust requirements have increased the demand for ...
In current and advanced gas turbine engines, increased speeds, pressures and temperatures are used t...
The experimental part of the turbine heat transfer subproject consists of six large experiments, whi...
A two-day workshop on the research and plans for turbine engine hot section durability problems was ...
The objectives of the HOST Turbine Heat Transfer subproject were to obtain a better understanding of...
Higher operating temperatures increase the efficiency of aircraft gas turbine engines, but can also ...
Includes bibliographical references (leaf 17)A blowdown turbine facility and an experimental program...
Clearances between gas turbine casings and rotating blades is of quite importance on turbo machines ...
A program sponsored by NASA for the investigation of the heat transfer in the transition region of t...
NASA is sponsoring the Turbine Engine Hot Section Technology (HOST) Project to address the need for ...
The efficiency and power output of the gas turbine is impacted directly by the maximum gas temperatu...
This work is motivated by the need to accurately predict heat transfer in turbomachinery. For effici...
Improvements in methods for predicting heat transfer rates on the hot gas side of turbine airfoils a...
The objectives of the NASA Hot Section Technology (HOST) Turbine Heat Transfer subproject were to ob...
The thermal design of the combustor and turbine of a gas turbine engine poses a number of difficult ...
Increased attention to fuel economy and increased thrust requirements have increased the demand for ...
In current and advanced gas turbine engines, increased speeds, pressures and temperatures are used t...
The experimental part of the turbine heat transfer subproject consists of six large experiments, whi...
A two-day workshop on the research and plans for turbine engine hot section durability problems was ...
The objectives of the HOST Turbine Heat Transfer subproject were to obtain a better understanding of...
Higher operating temperatures increase the efficiency of aircraft gas turbine engines, but can also ...
Includes bibliographical references (leaf 17)A blowdown turbine facility and an experimental program...
Clearances between gas turbine casings and rotating blades is of quite importance on turbo machines ...
A program sponsored by NASA for the investigation of the heat transfer in the transition region of t...
NASA is sponsoring the Turbine Engine Hot Section Technology (HOST) Project to address the need for ...
The efficiency and power output of the gas turbine is impacted directly by the maximum gas temperatu...
This work is motivated by the need to accurately predict heat transfer in turbomachinery. For effici...