Time-Averaged and Time-Resolved Heat Flux Measurements on a Turbine Stator Blade Using Two-Layered Thin-Film Gauges

[+] Author and Article Information
V. Iliopoulou, R. Dénos, N. Billiard, T. Arts

von Karman Institute for Fluid Dynamics, Turbomachinery & Propulsion Department, Chaussée de Waterloo, 72 1640 Rhode Saint Genèse, Belgium

J. Turbomach 126(4), 570-577 (Dec 29, 2004) (8 pages) doi:10.1115/1.1791647 History: Received October 01, 2003; Revised March 01, 2004; Online December 29, 2004
Copyright © 2004 by ASME
Your Session has timed out. Please sign back in to continue.


Epstein,  A. H., Guenette,  G. R., Norton,  R. J. G., and Yuzhang,  C., 1986, “High-Frequency Response Heat-Flux Gauge,” Rev. Sci. Instrum., 57(4), pp. 639–649.
Doorly,  J. E., and Oldfield,  M. L. G., 1986, “New Heat Transfer Gages for Use on Multilayered Substrates,” ASME J. Turbomach., 108, pp. 153–160.
Abhari,  R. S., Guenette,  G. R., Epstein,  A. H., and Giles,  M. B., 1992, “Comparison of Time-Resolved Turbine Rotor Blade Heat Transfer Measurements and Numerical Calculations,” ASME J. Turbomach., 114, pp. 818–827.
Piccini,  E., Guo,  S. M., and Jones,  T. V., 2000, “The Development of a New Direct-Heat-Flux Gauge for Heat-Transfer Facilities,” Meas. Sci. Technol., 11, pp. 342–349.
Doorly,  J. E., and Oldfield,  M. L. G., 1987, “The Theory of Advanced Multi-Layer Thin Film Heat Transfer Gauges,” J. Heat Mass Transfer,30(6), pp. 1159–1168.
Schultz, D. L., and Jones, T. V., 1973, “Heat Transfer Measurements in Short Duration Facilities,” AGARDograph no. 165.
Guo, S. M., Spencer, M. C., Lock, G. D., Jones, T. V., and Harvey, N. W., 1995, “The Applications of Thin Film Gauges on Flexible Plastic Substrates to the Gas Turbine Situation,” ASME paper No. 95-GT-357.
Arts, T., Lambert de Rouvroit, M., and Rutherford, A. W., 1990, “Aero-Thermal Investigation of a Highly Loaded Transonic Linear Turbine Guide Vane Cascade (A Test Case for Inviscid and Viscous Flow Computations),” VKI TN 174.
Didier,  F., Dénos,  R., and Arts,  T., 2002, “Unsteady Rotor Heat Transfer in a Transonic Turbine Stage,” ASME J. Turbomach., 124(4), pp. 614–622.
Dénos, R., 1996, “Aerothermal Investigation of the Unsteady Flow in the Rotor of a Transonic Turbine Stage,” Ph.D. thesis, University of Poitiers, France, December 1996.
Paniagua, G., Dénos, R., and Oropesa, M., 2002, “Thermocouple Probes for Accurate Temperature Measurements in Short Duration Facilities,” Proceedings, ASME 2002, Amsterdam, GT-2002-30043.
Billiard, N., Iliopoulou, V., Ferrara, F., and Dénos, R., 2002, “Data Reduction and Thermal Product Determination for Single and Multilayered Substrates Thin-Film Gauges,” Proceedings, 16th Symposium on Measuring Techniques, Cambridge University, Cambridge, UK.
Hirsch, C., 1988, “Fundamentals of Numerical Discretization,” Numerical Computation of Internal and External Flows, Wiley, Great Britain, pp. 425–431.
Diller,  T. E., 1993, “Advances in Heat Flux Measurements,” Adv. Heat Transfer, 23, pp. 279–368.
Buchlin, J. M., and Laperches, M., 1998, “Detailed Investigation of Aerothermal Behavior of Confined Impinging Jet,” Quantitative Infrared Themography QIRT 98, D. Balageas, G. Busse, and G. M. Carlomagno, eds., S. A. Lodart, Lodz, Poland, pp. 258–264.
Miller, C. G., 1981, “Comparison of Thin-Film Resistance Heat Transfer Gauges With Thin-Skin Transient Calorimeter Gages in Conventional Hypersonic Wind Tunnels,” NASA Technical Memorandum 83197.
Sieverding, C. H., and Arts, T., 1992, “The VKI Compression Tube Annular Cascade Facility CT3,” ASME paper No. 92-GT-336.
Kestin,  J., and Wood,  R., 1971, “The Influence of Turbulence on Mass Transfer From Cylinders,” J. Heat Transfer, 93C, pp. 321–327.
Ainsworth,  R. W., Allen,  J. L., Davies,  M. R. D., Doorly,  J. E., Forth,  C. J. P., Hilditch,  M. A., Oldfield,  M. L. G., and Sheard,  A. G., 1989, “Developments in Instrumentation and Processing for Transient Heat Transfer Measurement in a Full-Stage Model Turbine,” ASME J. Turbomach., 111, pp. 20–27.


Grahic Jump Location
“Senflex” two-layered substrate thin-film gauge
Grahic Jump Location
Linearization of the wall temperature evolution for a gauge submitted to a constant wall heat flux
Grahic Jump Location
Calculated surface heat flux (10 800 W/m2 ) with the Crank-Nicholson scheme
Grahic Jump Location
Aerothermal conditions of the jet
Grahic Jump Location
Nusselt-Reynolds correlation obtained with single-layered thin-film gauge
Grahic Jump Location
Surface temperature and heat flux for the time-averaged component
Grahic Jump Location
Blade initial temperature distributions prior to blowdown from single and two-layered gauges
Grahic Jump Location
Surface temperature, heat flux, and Nusselt distribution for the two-layered gauges during the blowdown
Grahic Jump Location
Surface temperature, heat flux, and Nusselt distribution for the single-layered gauges during the blowdown
Grahic Jump Location
Comparison of the repeatability of the Nusselt distribution between the single- and two-layered gauges
Grahic Jump Location
Unsteady Nusselt number traces of two gauges of four different measurements for the two-layered gauges
Grahic Jump Location
Min-max envelope, mean RMS, and correlation coefficient of the Nusselt number obtained with single and two-layered gauges
Grahic Jump Location
Comparison of the unsteady Nusselt traces between the single- (in grey) and the two-layered gauges (in black)




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