0
TECHNICAL PAPERS: Gas Turbines: Heat Transfer

Experimental and Numerical Study of Heat Transfer in a Gas Turbine Combustor Liner

[+] Author and Article Information
J. C. Bailey, N. V. Nirmalan, R. S. Bunker

GE Corporate Research and Development, Niskayuna, NY 12309

J. Intile, T. F. Fric

GE Power Systems, Greenville, SC 29602

A. K. Tolpadi

GE Power Systems, Schenectady, NY 12345

J. Eng. Gas Turbines Power 125(4), 994-1002 (Nov 18, 2003) (9 pages) doi:10.1115/1.1615256 History: Received December 01, 2001; Revised March 01, 2002; Online November 18, 2003
Copyright © 2003 by ASME
Your Session has timed out. Please sign back in to continue.

References

Chin,  J., Skirvin,  S., Hayes,  L., and Burggraf,  F., 1961, “Film Cooling With Multiple Slots and Louvers—Part 1: Multiple Continuous Slots,” ASME J. Heat Transfer, 83, pp. 281–286.
Crawford,  M., Kays,  W., and Moffat,  R., 1980, “Full-Coverage Film Cooling Part 1: Comparison of Heat Transfer Data for Three Injection Angles,” ASME J. Eng. Power, 102, pp. 1000–1005.
Metzger,  D. E., Takeuchi,  D., and Kuenstler,  P., 1973, “Effectiveness and Heat Transfer With Full-Coverage Film Cooling,” ASME J. Eng. Power, 95, pp. 180–184.
Andrews, G. E., Al Dabagh, A. M., Asere, A. A., Bazdidi-Tehrani, F., Mkpadi, M. C., and Nazari, A., 1992, “Impingement/Effusion Cooling,” AGARD CP-527, Heat Transfer and Cooling in Gas Turbines, Paper Number 30.
Andrews, G. E., Khalifa, I. M., Asere, A. A., and Bazdidi-Tehrani, F., 1995, “Full Coverage Effusion Film Cooling With Inclined Holes,” ASME Paper 95-GT-274.
Al Dabagh,  A. M., Andrews,  G. E., Abdul Husain,  R. A. A., Husain,  C. I., Nazari,  A., and Wu,  J., 1990, “Impingement/Effusion Cooling: The Influence of the Number of Impingement Holes and Pressure Loss on the Heat Transfer Coefficient,” ASME J. Turbomach., 112, pp. 467–476.
Martiny, M., Schulz, A., and Wittig, S., 1995, “Full-Coverage Film Cooling Investigations: Adiabatic Wall Temperatures and Flow Visualization,” ASME Paper 95-WA/HT-4.
Martiny, M., Schulz, A., and Wittig, S., 1997, “Mathematical Model Describing the Coupled Heat Transfer in Effusion Cooled Combustor Walls,” ASME Paper 97-GT-329.
Fric, T. F., Campbell, R. P., and Rettig, M. G., 1997, “Quantitative Visualization of Full-Coverage Discrete-Hole Film Cooling,” ASME Paper 97-GT-328.
Schulz,  A., 2001, “Combustor Liner Cooling Technology in Scope of Reduced Pollutant Formation and Rising Thermal Efficiencies,” Heat Transfer in Gas Turbine Systems, Ann. NY. Acad. Sci., 934, pp. 135–146.
Martin, H., 1977, “Heat and Mass Transfer Between Impinging Gas Jets and Solid Surfaces,” Advances in Heat Transfer, 13 , Academic Press, San Diego, CA, pp. 1–60.
Metzger,  D., and Korstad,  R., 1972, “Effects of Crossflow on Impingement Heat Transfer,” ASME J. Eng. Power, 94, pp. 35–41.
Kercher,  D., and Tabakoff,  W., 1970, “Heat Transfer by a Square Array of Round Air Jets Impinging Perpendicular to a Flat Surface Including the Effect of Spent Air,” ASME J. Eng. Power, 92, pp. 73–82.
Florschuetz,  L., Truman,  C., and Metzger,  D., 1981, “Streamwise Flow and Heat Transfer Distributions for Jet Array Impingement With Crossflow,” ASME J. Heat Transfer, 103, pp. 337–342.
Florschuetz,  L., Berry,  R., and Metzger,  D., 1980, “Periodic Streamwise Variations of Heat Transfer Coefficients for Inline and Staggered Arrays of Circular Jets With Crossflow of Spent Air,” ASME J. Heat Transfer, 102, pp. 132–137.
Florschuetz,  L., Metzger,  D., and Su,  C., 1984, “Heat Transfer Characteristics for Jet Array Impingement With Initial Crossflow,” ASME J. Heat Transfer, 106, pp. 34–41.
Webb,  R. L., Eckert,  E. R. G., and Goldstein,  R. J., 1971, “Heat Transfer and Friction in Tubes With Repeated-Rib Roughness,” Int. J. Heat Mass Transfer, 14, pp. 601–617.
Burggraf, F., 1970, “Experimental Heat Transfer and Pressure Drop With Two-Dimensional Turbulence Promoter Applied to Two Opposite Walls of a Square Tube,” Augmentation of Convective Heat and Mass Transfer, Bergles and Webb, eds., ASME, New York, pp. 70–79.
Han,  J. C., Glicksman,  L. R., and Rohsenow,  W. M., 1978, “An Investigation of Heat Transfer and Friction for Rib-Roughened Surfaces,” Int. J. Heat Mass Transfer, 21, pp. 1143–1156.
Han, J. C., Park, J. S., and Lei, C. K., 1984, “Heat Transfer Enhancement in Channels With Turbulence Promoters,” ASME Paper 84-WA/HT-72.
Ferrara, G., Innocenti, L., Migliorini, G., Facchini, B., and Dean, A. J., 2000, “Heat Transfer Analysis in a Modern DLN Combustor,” ASME Paper 2000-GT-254.
Smith, K., and Fahme, A., 1999, “Backside Cooled Combustor Liner for Lean-Premixed Combustion,” ASME Paper 99-GT-239.
Vandervort,  C. L., 2001, “9 ppm NOx/CO Combustion System for “F” Class Industrial Gas Turbines,” ASME J. Eng. Gas Turbines Power, 123, pp. 317–323.
Farina,  D. J., Hacker,  J. M., Moffat,  R. J., and Eaton,  J. K., 1994, “Illuminant Invariant Calibration of Thermochromic Liquid Crystals,” Exp. Therm. Fluid Sci., 9, pp. 1–9.
Kline, S. J., and McClintock, F. A., “Describing Uncertainties in Single-Sample Experiments,” Mech. Eng. (Am. Soc. Mech. Eng.), Jan.
Launder,  B. E., and Spalding,  D. B., 1974, “The Numerical Computation of Turbulent Flows,” Comput. Methods Appl. Mech. Eng., 3, pp. 269–289.
Norris, L. H., and Reynolds, W. C., 1975, “Turbulent Channel Flow With a Moving Wavy Boundary,” Report No. FM-10, Department of Mechanical Engineering, Stanford University, Stanford, CA.
STARCD, 2001, Version 3.1B manual.
Perry,  K. P., 1954, “Heat Transfer by Convection From a Hot Gas Jet to a Plane Surface,” Proc. Inst. Mech. Eng., 168, pp. 775–780.

Figures

Grahic Jump Location
Cross-section of typical “F” class combustor system per 23
Grahic Jump Location
Parallel plate test section module
Grahic Jump Location
Flow cross-section and detailed surface construction
Grahic Jump Location
Test rig pressure vessel (left) and internal test section (right, jets inactive)
Grahic Jump Location
Wall-function discretization scheme
Grahic Jump Location
Two-layer discretization scheme
Grahic Jump Location
Impingement heat transfer data with bare surface heater
Grahic Jump Location
Comparison of circumferentially averaged test data for varying geometries
Grahic Jump Location
(a) Computed velocities for impingement region (m/s); (b) Computed velocities for flow past a turbulator (m/s)
Grahic Jump Location
Comparison of liner pressure drop for experimental data and CFD predictions
Grahic Jump Location
Comparison of liner heat transfer for experimental data and CFD predictions
Grahic Jump Location
Relative error in heat transfer coefficients between test data and CFD predictions
Grahic Jump Location
Comparison of circumferentially averaged heat transfer coefficient across liner

Tables

Errata

Discussions

Some tools below are only available to our subscribers or users with an online account.

Related Content

Customize your page view by dragging and repositioning the boxes below.

Related Journal Articles
Related eBook Content
Topic Collections

Sorry! You do not have access to this content. For assistance or to subscribe, please contact us:

  • TELEPHONE: 1-800-843-2763 (Toll-free in the USA)
  • EMAIL: asmedigitalcollection@asme.org
Sign In