Published May 7, 2018 | Version v1

Design, Development and Validation of University of Cincinnati (UC) Film Cooling Research Facility

  • 1. University of Cincinnati, USA

Description

Film cooling effectiveness can be measured by thermal and mass transfer analysis. We have designed and developed a flat plate adiabatic wind tunnel facility to study film cooling effectiveness of selected film hole geometries by mass transfer analysis using a heavy gas (CO2 ) as a substitute for the coolant, measuring the mixing by both gas sampling and full field measurements by an optical measurement technique using pressure/oxygen sensitive paint .

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References

  • ABERNETHY, R., BENEDICT, R. and DOWDELL, R., 1985. ASME measurement uncertainty. Journal of Fluids Engineering, 107 (2), pp. 161 - 164.
  • BALDAUF, S., SCHULZ, A., WITTIG, S. and SCHLEURLEN, M., 1997. An overall correlation of film cooling effectiveness from one row of holes. ASME paper, (97 - GT), pp. 079.
  • BALDAUF, S.A., SCHEURLEN, M., SCHULZ, A. and WITTIG, S., 2002. Correlation of film - cooling effectiveness from thermographic measurements at engine like conditions. TRANSACTIONS - AMERICAN SOCIETY OF MECHANICAL ENGINEERS JOURNAL OF TURBOMACHINERY, 124 (4), pp. 686 - 698.
  • BRADLEY, A. and WREN, J., 2010. Comparison of Correlations and Experiments for Prediction of Vane Film Cooling in Gas Turbines. Linköping University Electronic Press.
  • BROWN, A. and SALUJA, C., 1979. Film cooling from a single hole and a row of holes of variable pitch to diameter ratio. International Journal of Heat and Mass Transfer, 22 (4), pp. 525 - 534.
  • BUNKER, R., 2007. Turbine engine film cooling design and applications. LECTURE SERIES - VON KARMAN INSTITUTE FOR FLUID DYNAMICS, 6, pp. 1.
  • COLBAN, W.F., THOLE, K.A. and BOGARD, D., 2011. A film - cooling correlation for shaped holes on a flat - plate surface. Journal of Turbomachinery, 133 (1), pp. 011002.
  • ECKERT, E., ERIKSEN, V., GOLDSTEIN, R. and RAMSEY, J., 1970. Film cooling following injection through inclined circular tubes.
  • GOLDSTEIN, R.J., 1971. Film cooling. Advances in heat transfer, 7 (1), pp. 321 - 379.
  • GRITSCH, M., SCHULZ, A. and WITTIG, S., 1998. Adiabatic wall effectiveness measurements of film - cooling holes with expanded exits. TRANSACTIONS - AMERICAN SOCIETY OF MECHANICAL ENGINEERS JOURNAL OF TURBOMACHINERY, 120, pp. 549 - 556.
  • HAN, J., 1997. Film Effectiveness Over a Flat Surface with Air and C02 Injection Through Compound Angle Holes Using a Transient Liquid Crystal Image Method. Journal of Turbomachinery, 119, pp. 587.
  • L'ECUYER, M. and SOECHTING, F., 1985. A model for correlating flat plate film - cooling effectiveness for rows of round holes. AGARD Heat Transfer and Cooling in Gas Turbines 12p (SEE N86 - 29823 21 - 07) .
  • LUTUM, E. and JOHNSON, B.V., 1999. Influence of the hole length - to - diameter ratio on film cooling with cylindrical holes. ASME J. Turbomach, 121 (2), pp. 209 - 216.
  • MANDEL, J., 1972. Repeatability and reproducibility. Journal of Quality Technology, 4 (2).
  • PEDERSEN, D., ECKERT, E. and GOLDSTEIN, R., 1977. Film cooling with large density differences between the mainstream and the secondary fluid measured by the heat - mass transfer analogy. Journal of Heat Transfer, 99 (4), pp. 620 - 627.
  • SAUMWEBER, C. and SCHULZ, A., 2012. Free - stream effects on the cooling performance of cylindrical and fan - shaped cooling holes. Journal of Turbomachinery, 134 (6), pp. 061007.
  • SCHMIDT, D.L. and BOGARD, D.G., 1995. Pressure gradient effects on film cooling. ASME paper, (95 - GT), pp. 18.
  • SCHMIDT, D.L., SEN, B. and BOGARD, D.G., 1996a. Effects of Surface Roughness on Film Cooling. ASME paper, (96 - GT), pp. 299.
  • SCHMIDT, D.L., SEN, B. and BOGARD, D.G., 1996b. Film cooling with compound angle holes: adiabatic effectiveness. Journal of Turbomachinery, 118 (4), pp. 807 - 813.
  • SINHA, A., BOGARD, D. and C RAWFORD, M., 1991. Film - cooling effectiveness downstream of a single row of holes with variable density ratio. Journal of Turbomachinery, 113 (3), pp. 442 - 449.
  • WAYE, S.K. and BOGARD, D.G., 2007. High - resolution film cooling effectiveness measurements of axial holes embedded in a transverse trench with various trench configurations. Journal of Turbomachinery, 129 (2), pp. 294 - 302.
  • YUEN, C.H.N., 2000. Measurement of Local Heat Transfer Coefficient and Film Cooling Effectiveness in Film Cooling Geometrics. Diss. Department of Mechanical Engineering, Imperial College .