Aerodynamics of slot-film cooling: theory and experiment

Author:

Fitt A. D.,Ockendon J. R.,Jones T. V.

Abstract

A simple model is proposed for the two-dimensional injection of irrotational inviscid fluid from a slot into a free stream. In a certain range of values of the ratio of free-stream to injection total heads, the film thickness satisfies a nonlinear integral equation whose solution enables the mass flow in the film to be found. Some experiments are described which both agree with this theory when it is relevant and indicate its deficiencies at other values of the total head ratio.

Publisher

Cambridge University Press (CUP)

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics

Reference13 articles.

1. Smith, F. T. & Stewartson, K. 1973 On slot injection into a supersonic laminar boundary layer.Proc. R. Soc. Lond. A332,1–22.

2. Ting, L. & Ruger, C. J. 1965 Oblique injection of a jet into a stream.AIAA J. 3,534–576.

3. Goldstein, R. J. 1971 Film cooling.Adv. Heat Transfer 7,321–379.

4. Schlichting, H. 1979 Boundary Layer Theory.McGraw-Hill.

5. Barry, B. 1976 The aerodynamic penalties associated with blade cooling. InTurbine Blade Cooling; VKI LS 83.

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