Infrared Low-Temperature Turbine Vane Rough Surface Heat Transfer Measurements

[+] Author and Article Information
R. J. Boyle, C. M. Spuckler, B. L. Lucci, W. P. Camperchioli

NASA Glenn Research Center, Cleveland, OH 44135

J. Turbomach 123(1), 168-177 (Feb 01, 2000) (10 pages) doi:10.1115/1.1333693 History: Received February 01, 2000
Copyright © 2001 by ASME
Your Session has timed out. Please sign back in to continue.


Dunn,  M. G., Kim,  J., Civinskas,  K. C., and Boyle,  R. J., 1994, “Time-Averaged Heat Transfer and Pressure Measurements and Comparison With Prediction for a Two-Stage Turbine,” ASME J. Turbomach., 116, pp. 14–22.
Blair,  M. F., 1994, “An Experimental Study of Heat Transfer in a Large-Scale Turbine Rotor Passage,” ASME J. Turbomach., 116, pp. 1–13.
Tarada, F., 1987, “Heat Transfer to Rough Turbine Blading,” PhD thesis, University of Sussex, England.
Tarada, F., and Suzuki, M., 1993, “External Heat Transfer Enhancement to Turbine Blading Due to Surface Roughness,” ASME Paper No. 93-GT-74.
Abuaf,  N., Bunker,  R. S., and Lee,  C. P., 1998, “Effects of Surface Roughness on Heat Transfer and Aerodynamic Performance of Turbine Airfoils,” ASME J. Turbomach., 120, pp. 522–529.
Sargent,  S. R., Hedlund,  C. R., and Ligrani,  P. M., 1998, “An Infrared Thermography Imaging System for Convective Heat Transfer Measurements in Complex Flows,” Meas. Sci. Technol., 9, pp. 1974–1981.
Baldauf, S., Schulz, A., and Witting, S., 1999, “High Resolution Measurements of Local Heat Transfer Coefficients by Discrete Hole Film Cooling,” ASME Paper No. 99-GT-43.
Johnston, C. A., Bogard, D. G., and McWaters, M. A., 1999, “Highly Turbulent Mainstream Effects on Film Cooling of a Simulated Airfoil Leading Edge,” ASME Paper No. 99-GT-261.
Sweeney,  P. C., and Rhodes,  J. F., 2000, “An Infrared Technique for Evaluating Turbine Airfoil Cooling Designs,” ASME J. Turbomach., 122, pp. 171–178.
Boyle, R. J., Spuckler, C. M., and Lucci, B. L., 2000, “Comparison of Predicted and Measured Vane Rough Surface Heat Transfer,” ASME Paper No. 2000-GT-0217.
Boyle, R. J., Lucci, B. L., Verhoff, V. G., Camperchioli, W. P., and La, H., 1998, “Aerodynamics of a Transitioning Turbine Stator Over a Range of Reynolds Numbers,” ASME Paper No. 98-GT-285.
Banks, B. A., and Rutledge, S. K., 1982, “Ion Beam Sputter Deposited Diamondlike Films,” NASA TM 82873.
Dagnall, H., 1986, Exploring Surface Texture, 2nd ed., Rank Taylor Hobson Ltd., Leicester, England, p. 158.
Kind,  R. J., Serjak,  P. J., and Abbott,  M. W. P., 1998, “Measurements and Prediction of the Effects of Surface Roughness on Profile Losses and Deviation in a Turbine Cascade,” ASME J. Turbomach., 120, pp. 20–27.
Bammert,  K., and Stanstede,  H., 1972, “Measurements Concerning the Influence of Surface Roughness and Profile Changes on the Performance of Gas Turbines,” ASME J. Eng. Power, 94, pp. 207–213.
Bammert,  K., and Stanstede,  H., 1976, “Influences of Manufacturing Tolerances and Surface Roughness of Blades on the Performance of Turbines,” ASME J. Eng. Power, 98, pp. 29–36.
Boynton,  J. L., Tabibzadeh,  R., and Hudson,  S. T., 1992, “Investigation of Rotor Blade Roughness Effects on Turbine Performance,” ASME J. Turbomach., 115, pp. 614–620.
Boyle,  R. J., and Giel,  P. W., 1995, “Three-Dimensional Navier–Stokes Heat Transfer Predictions for Turbine Blade Rows,” J. Propul. Power, 11, No. 6, pp. 1179–1186.
Kays, W. M., and Crawford, M. E., 1980, Convective Heat and Mass Transfer, 2nd ed., McGraw-Hill, New York, p. 327.
Chima,  R. V., 1996, “Application of the k–ω Turbulence Model to Quasi-Three-Dimensional Turbomachinery Flows,” J. Propul. Power, 12, No. 6, pp. 1176–1179.
Burmeister, L. C., 1983, Convective Heat Transfer, Wiley, New York, p. 544.
Hodge,  B. K., Taylor,  R. P., and Coleman,  H. W., 1986, “An Investigation of Surface Roughness Effects on Adiabatic Wall Temperature,” AIAA J., 24, No. 9, pp. 1560–1561.
Van Fossen,  G. J., Simoneau,  R. J., and Ching,  C. Y., 1995, “Influence of Turbulence Parameters, Reynolds Number, and Body Shape on Stagnation Region Heat Transfer,” ASME J. Heat Transfer, 117, pp. 597–603.
Pimenta, M. M., Moffatt, R. J., and Kays, W. M., 1995, “The Turbulent Boundary Layer: An Experimental Study of the Transport of Momentum and Heat With the Effect of Roughness,” Rep. HMT-21, Dept. of Mechanical Engineering, Stanford Univ., CA.


Grahic Jump Location
Overall view of test section
Grahic Jump Location
Construction of heat transfer vane
Grahic Jump Location
Estimated maximum equivalent roughness height, hEQ+
Grahic Jump Location
Temperatures recorded by infrared camera, °C
Grahic Jump Location
Calculated surface temperatures, °C
Grahic Jump Location
Nusselt number, uniform heat flux
Grahic Jump Location
Nusselt number, nonuniform heat flux
Grahic Jump Location
Midspan Nusselt numbers
Grahic Jump Location
Frossling number at vane stagnation point
Grahic Jump Location
Stanton number at s/Cx=2.5
Grahic Jump Location
Effect of emissivity variation, Re2=0.394×106,M2=0.7, grid



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