Convective Heat Transfer with Film Cooling Around a Rotor Blade

Author:

Arts T.

Publisher

Springer New York

Reference35 articles.

1. Adams, E.W., and Johnston, J.P., 1984, “A Mixing Length Model for the Prediction of Convex Curvature Effects on Turbulent Boundary Layers,” J. Engrg for Gas Turbines & Power,1061, Jan., 142–148.

2. Arts, T., 1982, “Cascade Flow Calculation Using a Finite Volume Method,” “Numerical Methods for Flows in Turbomachinery, VKI LS 1982–05.

3. Arts, T., and Bourguignon, A.E., 1989, “Behaviour of a Two Rows of Holes Coolant Film Along the Pressure Side of a High Pressure Nozzle Guide Vane,” ASME 34th Int. Gas Turbine and Aero-Engine Congress and Exposition, Toronto, Canada, June.

4. Arts, T., and Graham, C.G., 1985, “External Heat Transfer Study on a HP Turbine Rotor Blade,”Heat Transfer and Cooling in Gas Turbines, AGARD CP 390, Paper 5.

5. Buyuktur, A.R., Kestin, J., and Maeder, P.F.,1964, “Influence of Combined Pressure Gradient and Turbulence on the Transfer of Heat From a Plate,”Int. J. of Heat & Mass Transfer 7 11Nov.,1175–1186.

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