Combustor liner cooling technology in scope of reduced pollutant formation and rising thermal efficiencies

Annals of the New York Academy of Sciences

Volumn 934, Issue , 2001, Pages 135-146

  Schulz, A ^a  

^a UNIVERSITY OF KARLSRUHE   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTION; CONFERENCE PAPER; COOLING; DENSITY; POLLUTANT; TECHNIQUE; TECHNOLOGY; TEMPERATURE; THERMAL ANALYSIS;

EID: 0034960713     PISSN: 00778923     EISSN: None     Source Type: Book Series    
DOI: 10.1111/j.1749-6632.2001.tb05848.x     Document Type: Conference Paper

References (29)

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4. Full-coverage film cooling Part 1: Comparison of heat transfer data for three injection angles
5. A model for correlating flat plate film cooling effectiveness for rows of round holes
6. Film effectiveness over a flat surface, with air CO2 injection through compound angle holes using a transient liquid crystal image method
7. Heat transfer coefficients over a flat surface with air CO2 injection through compound angle holes using a transient liquid crystal image method
8. Mass transfer in the neighborhood of jets entering a crossflow
9. Velocity distribution. Temperature distribution. Effectiveness and heat transfer in cooling of a surface with pressure gradient
10. Adiabatic effectiveness. Thermal fields, and velocity fields for film cooling with large angle ejection
11. Experiments on transpiration cooling: Discrete hole injection as it means of transpiration cooling: An experimental study
12. Experimental study on the flow characteristic of streamwise inclined jets in crossflow on flat plate
13. Effectiveness and heat transfer with full-coverage film cooling
14. Multihole cooling film effectiveness and heat transfer
15. Hydrodynamic measurements of jets in crossflow for gas turbine film cooling applications
16. Film cooling of an adiabatic flat plate in zero pressure gradient in the presence of a hot mainstream and a cold tangential secondary injection
17. Effusion cooled combustor liners of gas turbines - An assessment of the contributions of convective, impingement, and film cooling
18. Flow field measurements for film cooling holes with expanded exits
19. Hot air discharge for Dc-Icing