Aerodynamic measurements over a film cooled nozzle vane endwall

ETC 2005 - 6th Conference on Turbomachinery: Fluid Dynamics and Thermodynamics

Volumn , Issue , 2005, Pages

  Barigozzi, G ^a   Benzoni, G ^a   Franchini, G ^a   Perdichizzi, A ^a  

^a UNIVERSITY OF BERGAMO   (Italy)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; COOLANTS; FLOW FIELDS; FLOW OF FLUIDS; MACH NUMBER; NOZZLES; SECONDARY FLOW; THERMODYNAMICS;

AERO-DYNAMIC PERFORMANCE; AERODYNAMIC MEASUREMENTS; COOLANT INJECTION; ENDWALL COOLING; INJECTION RATES; LOW MACH NUMBERS; MASS FLOW RATIOS; NOZZLE VANE CASCADE;

COOLING;

EID: 84925423575     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (16)

1. Blair, M.F., 1974, "An Experimental Study of Heat Transfer and Film Cooling on Large-Scale Turbine Endwalls", ASME Journal of Heat Transfer, pp. 524-529.
2. Roy, R.P. et al., 2000, "Flow and Heat Transfer at the Hub Endwall of Inlet Vane Passages - Experiments and Simulations", ASME Paper 2000-GT-198.
3. Oke, R.A., Simon, 2002, "Film Cooling Experiments with Flow Introduced upstream of a First Stage Nozzle Guide Vane through Slots of Various Geometries", ASME paper GT-2002-30169.
4. Oke, R.A., Simon, T.W., Burd, S.W., Vahlberg, R., 2000, "Measurements in a Turbine Cascade over a Contoured Endwall: Discrete Hole Injection of Bleed Flow", ASME paper 2000-GT-214.
5. Jabbari, M.J., Marston, K.C., Eckert, E.R.G. Goldstein, R.J., 1996, "Film Cooling of the Gas Turbine Endwall by Discrete-Hole Injection", ASME Journal of Turbomachinery, Vol. 118, pp. 278-284.
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8. Friedrichs, S., Hodson, H.P., Dawes, W.N., 1999, "The Design of an Improved Endwall Film- Cooling Configuration", ASME Journal of Turbomachinery, Vol. 121, pp. 772-780.
9. Kost, F., Nicklas, M., 2001, "Film-Cooled Turbine Endwall in a Transonic Flow Field: Part I - Aero-dynamic Measurements", ASME paper 2001-GT-0145.
10. Nicklas, M., 2001, "Film-Cooled Turbine Endwall in a Transonic Flow Field: Part II - Heat Transfer and Film-Cooling Effectiveness", ASME Paper 2001-GT-0146.
11. Knost, D.G., Thole, K.A., 2004, "Adiabatic Effectiveness Measurements of Endwall Film- Cooling for a First Stage Vane", ASME Paper GT-2004-53326.
12. Zhang, L.J., Jaiswal, R.S., 2001, "Turbine Nozzle Endwall Film Cooling Study using Pressure Sensitive Paint", ASME Paper 2001-GT-0147.
13. Barigozzi, G., Benzoni, G., Perdichizzi, A., 2001, "Boundary Layer and Loss Analysis in a Film Cooled Vane", ASME Paper 2001-GT-0136.
14. Osnaghi, C., Perdichizzi, A., 1990, "Aerodynamic Measurements in Turbine Cascades at High Mach Number", Xth Symposium on Measuring Techniques for Transonic and Supersonic Flows in Cascades and Turbomachines, Von Karman Institute, Bruxelles, 17-18 September 1990
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16. Kost, F.H., Holmes, A.T., 1985, "Aerodynamic Effect of Coolant Ejection in the Rear Part of Transonic Rotor Blades", AGARD CP 390 "Heat Transfer and Cooling in Gas Turbines", Bergen (Norway), May 1985.