Detailed Measurements of Local Heat Transfer Coefficient in the Entrance to Normal and Inclined Film Cooling Holes

Author:

Gillespie D. R. H.1,Byerley A. R.1,Ireland P. T.1,Wang Z.1,Jones T. V.1,Kohler S. T.2

Affiliation:

1. Department of Engineering Science, University of Oxford, Oxford, United Kingdom

2. Rolls Royce Bristol, United Kingdom

Abstract

The local heat transfer inside the entrance to large-scale models of film cooling holes has been measured using the transient heat transfer technique. The method employs temperature-sensitive liquid crystals to measure the surface temperature of large-scale perspex models. Full distributions of local Nusselt number were calculated based on the cooling passage centerline gas temperature ahead of the cooling hole. The circumferentially averaged Nusselt number was also calculated based on the local mixed bulk driving gas temperature to aid interpretation of the results, and to broaden the potential application of the data. Data are presented for a single film cooling hole inclined at 90 and 150 deg to the coolant duct wall. Both holes exhibited entry length heat transfer levels that were significantly lower than those predicted by entry length data in the presence of crossflow. The reasons for the comparative reduction are discussed in terms of the interpreted flow field.

Publisher

ASME International

Subject

Mechanical Engineering

Reference17 articles.

1. Baughn, J. W., and Yan, X., 1992, “Heat Transfer Measurements in Square Ducts With Transverse Ribs,” presented at the National Heat Transfer Conference, Aug.

2. Boelter, L. M. K., Young, G., and Iversen, H. W., 1948, “An Investigation of Aircraft Heaters XXVII: The Distribution of Heat Transfer Rate in the Entrance Region of a Circular Tube,” NACA TN1451, Washington, DC.

3. Byerley, A. R., Ireland, P. T., Jones, T. V., and Ashton, S. A., 1988, “Detailed Heat Transfer Measurements Near and Within the Entrance of a Film Cooling Hole,” ASME Paper No. 88-GT-155.

4. Byerley, A. R., Jones, T. V., and Ireland, P. T., 1992, “Internal Cooling Passage Heat Transfer Near the Entrance to a Film Cooling Hole: Experimental and Computational Results,” ASME Paper No. 92-GT-241.

5. Byerley, A. R., 1989, “Heat Transfer Near the Entrance to a Film Cooling Hole in a Gas Turbine Blade,” D. Phil Thesis, Department of Engineering Science, University of Oxford, United Kingdom.

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