Add to ORKGA comparison was made of the heat transfer characteristics of three air cooled vanes. The vanes incorporated cooling schemes such as impingement cooling, film cooling, and convection cooling with and without extended surfaces. A redesign study was made for two vanes to improve the cooling effectiveness. An average impingement heat transfer coefficient was calculated on the bases of experimentally determined temperatures at the leading edge and a one dimensional heat transfer calculation. This heat transfer coefficient was compared with existing impingement heat transfer correlations
Progress in predictive design capabilities for external heat transfer to turbine vanes was summarize...
An effort was undertaken to understand the impact of different film cooling configurations in a true...
An effort was undertaken to understand the impact of different film cooling configurations in a true...
The heat-transfer characteristics of a chordwise-finned, impingement-cooled vane were investigated i...
The experimental temperature characteristics of two spanwise-finned, impingement-cooled vanes, one w...
The cooling effectiveness of three film-cooled vanes were compared to the cooling effectiveness of t...
Two air-cooled blades were tested to gas temperatures of 2568 F with coolant temperatures to 764 F. ...
The results of an experimental investigation of the aerodynamic performance of two geometrically sim...
Gas turbine engines are prevalent in the today’s aviation and power generation industries. The major...
An air-cooled turbine vane was tested in a four-vane cascade. Heat transfer characteristics of the i...
The aerodynamic performance of four different cooled vane configurations was experimentally determin...
Film-cooling-air ejection from the pressure surface of a turbine vane was investigated, and experime...
The first part of this dissertation experimentally studies the effect of transonic flow velocity on ...
Heat-transfer was investigated on an air-cooled turbine vane made from photoetched laminates that we...
The overall cooling performance of turbine nozzle guide vane, with the impingement-cutback structure...
Progress in predictive design capabilities for external heat transfer to turbine vanes was summarize...
An effort was undertaken to understand the impact of different film cooling configurations in a true...
An effort was undertaken to understand the impact of different film cooling configurations in a true...
The heat-transfer characteristics of a chordwise-finned, impingement-cooled vane were investigated i...
The experimental temperature characteristics of two spanwise-finned, impingement-cooled vanes, one w...
The cooling effectiveness of three film-cooled vanes were compared to the cooling effectiveness of t...
Two air-cooled blades were tested to gas temperatures of 2568 F with coolant temperatures to 764 F. ...
The results of an experimental investigation of the aerodynamic performance of two geometrically sim...
Gas turbine engines are prevalent in the today’s aviation and power generation industries. The major...
An air-cooled turbine vane was tested in a four-vane cascade. Heat transfer characteristics of the i...
The aerodynamic performance of four different cooled vane configurations was experimentally determin...
Film-cooling-air ejection from the pressure surface of a turbine vane was investigated, and experime...
The first part of this dissertation experimentally studies the effect of transonic flow velocity on ...
Heat-transfer was investigated on an air-cooled turbine vane made from photoetched laminates that we...
The overall cooling performance of turbine nozzle guide vane, with the impingement-cutback structure...
Progress in predictive design capabilities for external heat transfer to turbine vanes was summarize...
An effort was undertaken to understand the impact of different film cooling configurations in a true...
An effort was undertaken to understand the impact of different film cooling configurations in a true...