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The Mechanism and Application of Effusion Cooling

Published online by Cambridge University Press:  04 July 2016

L. Green Jr*
Affiliation:
Aerojet-General Corp., Azusa, California

Extract

In his excellent review of the “state of the art” of effusion cooling (p. 73, February Journal, 1959), Dr. P. Grootenhuis clearly distinguishes the two mechanisms which contribute to the cooling effectiveness; namely, efficient abstraction of heat from the porous wall material by internal transfer to the effusing coolant, and reduction of the rate of external transfer of heat from the stream to the wall as a result of boundary layer injection. An observation that deserves emphasis, however, is that the first of these mechanisms is the predominant one. This fact is illustrated by the good agreement between the theory assuming laminar flow conditions (i.e. involving integration of the Navier-Stokes equations and the use of a one-parameter velocity-profile expression proposed by Schlich-ting for the laminar boundary layer with injection) and the various experiments, all of which involved turbulent stream conditions. This observed agreement indicates that the surface temperature is primarily controlled by the internal heat transfer within the porous wall and is relatively insensitive to the external heat-transfer conditions.

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society 1959

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References

1.Green, L. Jr. and Nall, K. L. (1959). Experiments on Porous-Wall Cooling and Flow Separation Control in a Supersonic Nozzle. I.A.S. Report No. 59-38, January 1959.Google Scholar
2.Saunders, O. A. and Calder, P. H. (1952). Heat Transfer in Nozzles at Supersonic Speeds. Engineering, pp. 281284, 29th August 1952.Google Scholar
3.Rubesin, M. W. (1954). An Analytical Estimation of the Effect of Transpiration Cooling on the Heat-Transfer and Skin-Friction Characteristics of a Compressible, Turbulent Boundary Layer. N.A.C.A. T.N. 3341, December 1954.Google Scholar