Hostname: page-component-5c6d5d7d68-thh2z Total loading time: 0 Render date: 2024-08-19T00:52:20.087Z Has data issue: false hasContentIssue false

An experimental-numerical method for transient infrared measurement of film cooling effectiveness and heat transfer coefficient in a single test

Published online by Cambridge University Press:  05 August 2019

Nicholas E. Holgate*
Affiliation:
The University of Oxford Department of Engineering Science Oxford, United Kingdom
Peter T. Ireland
Affiliation:
The University of Oxford Department of Engineering Science Oxford, United Kingdom
Eduardo Romero
Affiliation:
Rolls-Royce plc Aerothermal Bristol, United Kingdom

Abstract

An experimental technique for assessing film cooling performance is proposed which can determine both film effectiveness and heat transfer coefficient distributions from a single infrared experiment. First, the film effectiveness is determined in the experiment’s steady-state phase on a series of film-cooled nozzle guide vane leading edge geometries made of a low thermal conductivity foam. Then, the effectiveness is used to calculate the distribution of the transient phase driving gas temperatures, which is applied to a finite element conduction model. Heat transfer coefficients are guessed and iteratively refined until the surface temperature histories predicted by the finite element model match those which were experimentally observed. Unlike conventional methods based on one-dimensional analytical heat transfer solutions, this approach does not require assumptions about the material thickness underlying the test surface or the uniformity with depth of its initial temperature distribution. This relieves certain experimental constraints and reduces uncertainty in results.

Type
Research Article
Copyright
© Royal Aeronautical Society 2019 

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

Footnotes

A version of this paper was presented at the 24th ISABE Conference in Canberra, Australia, September 2019.

References

REFERENCES

Metzger, D.E. and Larson, D.E. Use of melting point surface coatings for local convection heat transfer measurements in rectangular channel flows with 90-deg turns, J Heat Transfer, 1986, 108, (1), pp 4854.CrossRefGoogle Scholar
Ireland, P.T. and Jones, T.V. Liquid crystal measurements of heat transfer and surface shear stress, Measurement Science and Technology, 2000, 11, (7), pp 969986.CrossRefGoogle Scholar
Vedula, R.P. and Metzger, D.E. A method for the simultaneous determination of local effectiveness and heat transfer distributions in three temperature convection situations, 1991, ASME International Gas Turbine & Aeroengine Congress & Exposition.Google Scholar
Du, H., Han, J.C. and Ekkad, S.V. Effect of unsteady wake on detailed heat transfer coefficient and film effectiveness distributions for a gas turbine blade, J Turbomachinery, 1998, 120, (4), pp 808817.CrossRefGoogle Scholar
Licu, D.N., Findlay, M.J., Gartshore, I.S. and Salcudean, M. Transient heat transfer measurements using a single wide-band liquid crystal test, J Turbomachinery, 2000, 122, (3), pp 546552.CrossRefGoogle Scholar
Chyu, M.K. and Hsing, Y.C. Use of a thermographic phosphor fluorescence imaging system for simultaneous measurement of film cooling effectiveness and heat transfer coefficient, 1996, ASME International Gas Turbine & Aeroengine Congress & Exhibition.CrossRefGoogle Scholar
Ekkad, S.V., Ou, S. and Rivir, R.B. A transient infrared thermography method for simultaneous film cooling effectiveness and heat transfer coefficient measurements from a single test, J Turbomachinery, 2004, 126, (4), pp. 597603.Google Scholar
Chen, S.P., Chyu, M.K. and Shih, T.I.P. Effects of upstream ramp on the performance of film cooling, International Journal of Thermal Sciences, 2011, 50, (6), pp. 10851094.Google Scholar
Hayes, S.A., Nix, A.C., Nestor, C.M., Billups, D.T. and Haught, S.M. Experimental investigation of the influence of freestream turbulence on an anti-vortex film cooling hole, Experimental Thermal and Fluid Science, 2017, 81, pp 314326.CrossRefGoogle Scholar
Cresci, I. High pressure nozzle guide vane cooling system flow characteristics, D. Phil. thesis, The University of Oxford, 2015.Google Scholar
Cresci, I., Ireland, P.T., Bacic, M., Tibbott, I. and Rawlinson, A. Realistic velocity and turbulence intensity profiles at the combustor-turbine interaction plane in a nozzle guide vane test facility, 2015, European Turbomachinery Conference.Google Scholar
Cresci, I., Ireland, P.T., Bacic, M., Tibbott, I. and Rawlinson, A. Velocity and turbulence intensity profiles downstream of a long reach endwall double row of film cooling holes in a gas turbine combustor representative environment, 2015, ASME Turbomachinery Technical Conference & Exposition.CrossRefGoogle Scholar
Drost, U. and Bölcs, A. Investigation of detailed film cooling effectiveness and heat transfer distributions on a gas turbine airfoil, J Turbomachinery, 1999, 121, (2), pp 233242CrossRefGoogle Scholar
Pietrzyk, J.R., Bogard, D.G. and Crawford, M.E. Effects of density ratio on the hydrodynamics of film cooling, J Turbomachinery, 1990, 112, (3), pp 437443.CrossRefGoogle Scholar
Holgate, N.E., Ireland, P.T. and Self, K.P. Nozzle guide vane film cooling effectiveness for radial showerheads with restricted cooling hole surface angles, 2017, ASME Turbomachinery Technical Conference & Exposition.Google Scholar
Holgate, N.E., Ireland, P.T. and Romero, E. The effects of combustor cooling features on nozzle guide vane film cooling experiments, J Turbomachinery, 2019, 141, (1), pp 011005.Google Scholar
Coletti, F., Scialanga, M. and Arts, T. Experimental investigation of conjugate heat transfer in a rib-roughened trailing edge channel with crossing-jets, J Turbomachinery, 2011, 134, (4), pp 041046.Google Scholar
Ryley, J.C., Mcgilvray, M. and Gillespie, D.R.H. Calculation of heat transfer coefficient distribution on 3D geometries from transient liquid crystal experiments, 2014, ASME Turbomachinery Technical Conference & Exposition.CrossRefGoogle Scholar
Moffat, R.J. Describing the uncertainties in experimental results, Experimental Thermal and Fluid Science, 1988, 1, (1), pp 317.Google Scholar
Chambers, A.C., Gillespie, D.R.H., Ireland, P.T. and Dailey, G.M. A novel transient liquid crystal technique to determine heat transfer coefficient distributions and adiabatic wall temperature in a three-temperature problem, J Turbomachinery, 2003, 125, (3), pp 538546.CrossRefGoogle Scholar
Ekkad, S.V., Han, J.C. and Du, H. Detailed film cooling measurements on a cylindrical leading edge model: effect of free-stream turbulence and coolant density, J Turbomachinery, 1998, 120, (4), pp 799807.CrossRefGoogle Scholar
Mick, W.J. and Mayle, R.E. Stagnation film cooling and heat transfer including its effect within the hole pattern, J Turbomachinery, 1988, 110, pp 6672.CrossRefGoogle Scholar
Sen, B., Schmidt, D. and Bogard, D. Film cooling with compound angle holes: heat transfer, J Turbomachinery, 1996, 118, (4), pp 800806.CrossRefGoogle Scholar
Mouzon, B.D., Terrell, E.J., Albert, J.E. and Bogard, D.G. Net heat flux reduction and overall effectiveness for a turbine blade leading edge, 2005, ASME Turbo Expo, vol 3A, pp 825832.Google Scholar