Turbine Nozzle Endwall film cooling study using pressure-sensitive paint

Journal of Turbomachinery

Volumn 123, Issue 4, 2001, Pages 730-738

  Zhang, L J ^a   Jaiswal, R S ^a  

^a SOLAR TURBINES INCORPORATED   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ANEMOMETERS; COOLING; JETS; MASS TRANSFER; NOZZLES; OXYGEN; REYNOLDS NUMBER; TURBULENT FLOW;

PRESSURE-SENSITIVE PAINTS (PSP);

TURBINES;

COOLING; FLOW MEASUREMENT; GAS TURBINE; NOZZLE; PAINT;

EID: 0035483150     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1400113     Document Type: Article

References (19)

1. An experimental study of heat transfer and film cooling on low aspect ratio turbine nozzles
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3. Film cooling research on the endwall of a turbine nozzle guide vane in a short duration cascade part 1: Experimental technique and results
4. Film cooling research on the endwall of a turbine nozzle guide vane in a short duration cascade part 2: Analysis and correlation of results
5. Distribution of film cooling effectiveness on a turbine endwall measured using the ammonia and diazo technique
6. Aerodynamic aspect of endwall film cooling
7. The design of an improved endwall film cooling configuration
8. Film cooling of the gas turbine endwall by discrete-hole injection
9. Experimental contribution on the significance and the control by transverse injection of the horseshoe vortex
10. Effects of slot bleed injection over a contoured endwall on nozzle guide vane cooling performance: Part I - Flow field measurements
11. Aerodynamic investigation of endwall film-cooling in an axial turbine cascade part I: Experimental investigation
12. Aerodynamic investigation of endwall film-cooling in an axial turbine cascade. Part II: Numerical investigation
13. Effects of slot bleed injection over a contoured endwall on nozzle guide vane cooling performance: Part II - Thermal measurements
14. Measurements in a turbine cascade over a contoured endwall: Discrete hole injection of bleed flow
15. Flat plate film cooling measurement using PSP and gas chromatography techniques
16. Turbine nozzle film cooling study using the pressure sensitive paint (PSP) technique
17. Turbine nozzle leading edge film cooling study in a high speed wind tunnel
18. The effect of injection angle and hole exit shape on turbine nozzle pressure side film cooling
19. Describing uncertainties in single sample experiments