Turbine nozzle film cooling study using the pressure sensitive paint (PSP) technique

Proceedings of the ASME Turbo Expo

Volumn 3, Issue , 1999, Pages

  Zhang, Luzeng ^a   Baltz, Michael ^a   Pudupatty, Ram ^a   Fox, Michael ^a  

^a SOLAR TURBINES INCORPORATED   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; COOLING; GAS TURBINES; HEAT TRANSFER; LUMINOUS PAINT; MACH NUMBER; MASS TRANSFER; NITROGEN; NOZZLES; PAINT; REYNOLDS NUMBER; SUPERSONIC AERODYNAMICS; WIND TUNNELS;

FILM COOLING EFFECTIVENESS; FREESTREAM CONDITIONS; FREESTREAM MACH NUMBER; HIGH-SPEED WIND TUNNEL; OXYGEN CONCENTRATIONS; PRESSURE SENSITIVE PAINT TECHNIQUE; PRESSURE SENSITIVE PAINTS; TURBULENCE INTENSITY;

TURBINE COMPONENTS;

EID: 84928473695     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/99-GT-196     Document Type: Conference Paper

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