Flow field simulations of a gas turbine combustor

Journal of Turbomachinery

Volumn 124, Issue 3, 2002, Pages 508-516

  Barringer, M D ^a   Richard, O T ^a   Walter, J P ^a   Stitzel, S M ^a   Thole, K A ^a  

^a State University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; COMPUTER SIMULATION; COOLING; GAS TURBINES; JETS; NOZZLES; TURBULENCE; WIND TUNNELS;

DILUTION JETS;

COMBUSTORS;

COMBUSTOR; FLOW FIELD; FLOW MODELING; GAS TURBINE;

EID: 0036648835     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1475742     Document Type: Article

References (21)

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3. On the multiplicity of steady gas flows having the same streamline pattern
4. Analysis of hot streak effects on turbine rotor heat load
5. Effect of inlet profiles on endwall secondary flows
6. Redistribution of an inlet temperature distortion in an axial flow turbine stage
7. The influence of inlet temperature distortion on rotor heat transfer in a transonic turbine
8. Performance of a high-work low aspect ratio turbine tested with a realistic inlet radial temperature profile
9. Effects of slot bleed injection over a contoured endwall on nozzle guide vane cooling performance: Part I - Flow field measurements
10. Effects of slot bleed injection over a contoured endwall on nozzle guide vane cooling performance: Part II - Thermal measurements
11. Heat transfer and flowfield measurements in the leading edge region of a stator vane endwall
12. Highly turbulent flowfield measurements around a stator vane
13. High freestream turbulence effects in the endwall leading edge region
14. Measurements of discharge coefficients in film cooling
15. Describing the uncertainties in experimental results
16. Computational design and experimental evaluation of a leading edge fillet on a gas turbine vane