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Hypersonic Boundary Layers with Special Reference to Heat Transfer

Published online by Cambridge University Press:  04 July 2016

L. F. Crabtree
L. F. Crabtree*
Affiliation:
Aerodynamics Department, Royal Aircraft Establishment
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Extract

On the face of it boundary layer problems at hypersonic speed present enormous difficulties. However some aspects have turned out to be somewhat simpler than was visualised some years ago, and with the aid of certain simplifying assumptions many problems have been solved, at least to a good design approximation, and inaccuracies in the results are due not so much to the approximations involved, but to our lack of knowledge of the physical properties of air such as viscosity and Lewis number.

Type
Hypersonic Flow
Information
The Aeronautical Journal , Volume 63 , Issue 585 , September 1959 , pp. 513 - 516
Copyright
Copyright © Royal Aeronautical Society 1959

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References

1.Creager, M. O. (1957). Effects of Leading-Edge Blunting on the Local Heat Transfer and Pressure Distributions Over Flat Plates in Supersonic Flow. N.A.C.A. T.N. 4142, December 1957.Google Scholar
2.Bertram, M. H. and Henderson, A. (1958). Effects of Boundary-Layer Displacement and Leading-Edge Bluntness on Pressure Distribution, Skin Friction and Heat Transfer of Bodies at Hypersonic Speeds. N.A.C.A. T.N. 4301, July 1958.Google Scholar
3.Lees, Lester (1956). Laminar Heat Transfer Over Blunt-Nosed Bodies at Hypersonic Flight Speeds. Jet Propulsion, Vol. 26, No. 4, pp. 259–269, April 1956.CrossRefGoogle Scholar
4.Kemp, N. H., Detra, R. W. and Riddell, F. R. (1957). Addendum to “ Heat Transfer to Satellite Vehicles Re-entering the Atmosphere.” Jet Propulsion, Vol. 27, No. 12, pp. 1256-7, December 1957.CrossRefGoogle Scholar
5.Kemp, N. H., Rose, P. H. and Detra, R. W. (1958). Laminar Heat Transfer Around Blunt Bodies in Dissociated Air. Research Report 15, A.V.C.O. Research Laboratory, Everett, Mass., May 1958.Google Scholar
6.Rose, P. H., Probstein, R. F. and Adams, M. C. (1958). Turbulent Heat Transfer Through a Highly Cooled Partially Dissociated Boundary Layer. Research Report 14, A.V.C.O. Research Laboratory, January 1958.CrossRefGoogle Scholar
7.Libby, P. A. and Cresci, R. J.Evaluation of Several Hypersonic Turbulent Heat Transfer Analyses by Comparison with experimental data. W.A.D.C. T.N. 57-72. (Astia Document No. A.D. 118093). Polytechnic Institute of Brooklyn.Google Scholar
8.Eckert, E. R. G. (1954). Survey on Heat Transfer at High Speeds. W.A.D.C. Technical Report 54-70, April 1954.Google Scholar
9.Monaghan, R. J. Formulae and approximations for Aerodynamic Heating Rates in High Speed Flight. Unpublished Ministry of Supply Report.Google Scholar
10.Monaghan, R. J., Crabtree, L. F. and Woods, B. A. 1958). Features of Hypersonic Heat Transfer. The First International Congress of the Aeronautical Sciences, Madrid, 1958, Pergamon Press, 1959.Google Scholar
11.Gadd, G. E.To be published.Google Scholar
12.Naysmith, A. Heat Transfer and Boundary Layer Measurements in a Region of Supersonic Flow Separation and Reattachment. Unpublished Ministry of Supply Report.Google Scholar
13.Dorrance, W. H. and Dore, F. J. (1954). The Effect of Mass Transfer on the Compressible Turbulent Boundary Layer Skin Friction and Heat Transfer. Journal of the Aeronautical Sciences, Vol. 21, No. 6, pp. 404–410, June 1954.CrossRefGoogle Scholar
14.Leadon, B. M. and Scott, C. J. (1956). Transpiration Cooling Experiments in a Turbulent Boundary Layer at M = 3. Journal of the Aeronautical Sciences, Vol. 23, No. 8, pp. 798–799, August 1956.Google Scholar