Effects of flow turning, flow acceleration, and supersonic flow on film cooling were determined experimentally and correlated in terms of an entrainment film cooling model. Experiments were conducted using thin walled metal test sections, hot nitrogen mainstream gas, and ambient hydrogen or nitrogen as film coolants. The entrainment film cooling model relates film cooling effectiveness to the amount of mainstream gases entrained with the film coolant in a mixing layer. The experimental apparatus and the analytical model used are described in detail and correlations for the entrainment fraction and film coolant-to-wall heat transfer coefficient are presented
Heat-transfer coefficients were obtained on a thrust chamber which simulated the geometry of the NER...
Film cooling is generally considered as a promising active cooling technology for developing thermal...
Various parts of aircraft propulsion engines that are in contact with hot gases often require coolin...
Small scale nozzle tests using heated nitrogen were run to obtain effectiveness and wall heat transf...
The effects of: (1) a reactive environment on film cooling effectiveness, and (2) film cooling on ro...
This thesis reports the results of an experimental investigation of film cooling in a supersonic env...
Experimental investigations have been carried out to examine film cooling effectiveness of an accele...
Liquid film cooling is an important method for cooling the walls of a liquid rocket engine. Mass tra...
The effectiveness of slot film cooling of a flat plate in a Mach 6.4 flow with and without incident ...
Topics include: upper stage engine key requirements and design drivers; Calspan "stage 1" results, H...
Film cooling has been selected for the thermal protection of the composite nozzle extension of the J...
Film cooling is a technique used in gas turbine engines, and blades and rocket nozzles to protect cr...
Design Criteria, Experimental Studies of Supersonic Shock Wave Interaction with Film Cooling, and Hi...
Data were taken with a film-cooled test plate placed in the exhaust stream of a rectangular combusto...
Design Criteria, Experimental Studies of Supersonic Shock Wave Interaction with Film Cooling, and Hi...
Heat-transfer coefficients were obtained on a thrust chamber which simulated the geometry of the NER...
Film cooling is generally considered as a promising active cooling technology for developing thermal...
Various parts of aircraft propulsion engines that are in contact with hot gases often require coolin...
Small scale nozzle tests using heated nitrogen were run to obtain effectiveness and wall heat transf...
The effects of: (1) a reactive environment on film cooling effectiveness, and (2) film cooling on ro...
This thesis reports the results of an experimental investigation of film cooling in a supersonic env...
Experimental investigations have been carried out to examine film cooling effectiveness of an accele...
Liquid film cooling is an important method for cooling the walls of a liquid rocket engine. Mass tra...
The effectiveness of slot film cooling of a flat plate in a Mach 6.4 flow with and without incident ...
Topics include: upper stage engine key requirements and design drivers; Calspan "stage 1" results, H...
Film cooling has been selected for the thermal protection of the composite nozzle extension of the J...
Film cooling is a technique used in gas turbine engines, and blades and rocket nozzles to protect cr...
Design Criteria, Experimental Studies of Supersonic Shock Wave Interaction with Film Cooling, and Hi...
Data were taken with a film-cooled test plate placed in the exhaust stream of a rectangular combusto...
Design Criteria, Experimental Studies of Supersonic Shock Wave Interaction with Film Cooling, and Hi...
Heat-transfer coefficients were obtained on a thrust chamber which simulated the geometry of the NER...
Film cooling is generally considered as a promising active cooling technology for developing thermal...
Various parts of aircraft propulsion engines that are in contact with hot gases often require coolin...