Hostname: page-component-586b7cd67f-vdxz6 Total loading time: 0 Render date: 2024-11-22T06:14:20.960Z Has data issue: false hasContentIssue false

General Characteristics of Hypersonic Flow Fields

Published online by Cambridge University Press:  04 July 2016

R. N. Cox*
Affiliation:
A.R.D.E., Fort Hahtead

Summary

The object of this paper is to give a brief account of the development of the study of hypersonic flow over the past three decades, and to stress some of the ways in which hypersonic flow differs from supersonic flow. In some of the early work on the subject a wrong emphasis was given to the study of flows with attached shock waves and to the nature of the shock boundary layer interaction problem, and it is only quite recently, mainly as a result of experimental work, that it has become possible to obtain a balanced picture of the important features of hypersonic flow fields. In the present paper real gas effects are not taken into account; in general, the inclusion of these effects will not markedly alter the picture given.

Type
Hypersonic Flow
Copyright
Copyright © Royal Aeronautical Society 1959

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

1.Warren, C. H. E. and Young, A. D. (1958). The Definitions of Some Terms Relating to Various Flow Régimes of a Gas—Some Proposals. Journal of the Royal Aeronautical Society, pp. 801804, November 1958.Google Scholar
2.SirNewton, I. (1687). Mathematical Principles of Natural Philosophy, Section VII, 34th proposition, 1687.Google Scholar
3.Busemann, A. (1933). Flüssigkeits und Gasbewegungen. Handwörterbuch der Naturwissenschaft. 2nd Ed. Gustave Fischer, Jena, pp. 275277, 1933.Google Scholar
4.von Kármán, T. (1935). The Problem of Resistance in Compressible Fluids. Proc. 5th Volta Congress, Rome, pp. 210271, 1935.Google Scholar
5.Cox, R. N. and Winter, D. F. T. (1957). The Light Gas Hypersonic Gun Tunnel at A.R.D.E. Fort Halstead. A.G.A.R.D. Report 139, July 1957.Google Scholar
6.Lees, L. and Kubota, T. (1957). Inviscid Hypersonic Flow over Blunt-Nosed Slender Bodies. Journal of the Aeronautical Sciences, Vol. 24, No. 3, March 1957.Google Scholar
7.Tsien, H. S. (1946). Similarity Laws of Hypersonic Flows. Journ. Math, and Phys., Vol. 25, pp. 247251, 1946.Google Scholar
8.Oswatitsch, K. (1950). Similarity Laws for Hypersonic Flow. K.T.H. Aero. T.N. 16, Royal Inst. of Technology, Stockholm, 1950.Google Scholar
9.Hayes, W. D. (1947). On Hypersonic Similitude. Q. Appl. Math., Vol. 5, pp. 105106, 1947.Google Scholar
10.Taylor, G. I. (1950). The Formation of a Blast Wave by a Very Intense Explosion. Proc. Roy. Soc. (A) Vol. 201, No. 1065, pp. 159186, March 1950.Google Scholar
11.Lin, S. C. (1954). Cylindrical Shock Waves Produced by Instantaneous Energy Release. Journ. of Appl. Phys. Vol. 25, No. 1, pp. 5457, January 1954.Google Scholar
12.Sakurai, A. (1953). On the Propagation and Structure of the Blast Wave. Journ. of the Physical Soc. of Japan, Vol. 8, No. 5, September-October 1953.Google Scholar
13.Lees, L. (1956). Inviscid Hypersonic Flow over Blunt Nosed Slender Bodies. G.A.L.C.I.T. Hypersonic Research Project, Memo. No. 31, February 1956.Google Scholar
14.Cheng, H. K. (1957). Interim Report on Investigations Related to Hypersonic Flow and Boundary Layer Phenomena. Cornell Aero. Lab. Report No. A.F.-1180- A-l, November 1957.Google Scholar
15.Lees, L. (1954). Influence of the Leading Edge Shock Wave on the Laminar Boundary Layer at Hypersonic Speeds. G.A.L.C.I.T. Tech. Report No. 1, Contract No. DA-04-495-ORD-19, July 1954.Google Scholar
16.Probstein, R. F. (1955). Interacting Hypersonic Laminar Boundary Layer Flow Over a Cone. W.A.D.C. Technical Report A.F. 2798/1, March 1955.Google Scholar
17.Li, Ting-Yi and Nagamatsu, H. Y. (1955). Hypersonic Viscous Flow on Non-Insulated Flat Plate. Proc. 4th Midwest Conf. on Fluid Mech.. September 1955.Google Scholar
18.Shen, S. F. (1957). An Estimate of Viscosity Effect on the Hypersonic Flow Over an Insulated Wedge. J. Math, and Phys., Vol. 31, No. 3, pp. 192205, October 1957.Google Scholar
19.Stewartson, K. (1955). On the Motion of a Flat Plate at High Speed in a Viscous Incompressible Fluid. Proc. Camb. Phil. Soc., Vol. 51, Pt. I, p. 202, January 1955.Google Scholar
20.Bertram, M. H. (1954). Viscous and Leading Edge Thickness Effects on the Pressures on the Surface of a Flat Plate in Hypersonic Flow. Journal of the Aeronautical Sciences, Vol. 21, No. 6, pp. 430431, June 1954.Google Scholar
21.Kendall, James M. Jr. (1957). An Experimental Investigation of Leading-Edge Shock Wave Boundary-Layer Interaction at Mach 5·8. Journal of the Aeronautical Sciences, Vol. 24, No. 1, pp. 4756, January 1957.Google Scholar
22.Hammitt, A. G. and Bogdonoff, S. M. (1954). A Study of the Flow About Simple Bodies at Mach Numbers From 11-15. W.A.D.C. Technical Report 54-257, October 1954.Google Scholar
23.Lees, L. (1955). Hypersonic Flow. Fifth Int. Aero. Conf., Los Angeles, pp. 241276, 1955. Inst, of the Aero. Sciences, 1956.Google Scholar
24.Hammitt, A. G. and Bogdonoff, S. M. (1956). Hypersonic Studies of the Leading Edge Effect on the Flow Over a Flat Plate. Jet Propulsion, Vol. 26, No. 4, 1956.Google Scholar
25.Bertram, M. H. (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. Tech. Note 4301, July 1958.Google Scholar
26.Vas, I. E., Bogdonoff, S. M. and Hammitt, A. G. (1958). An Experimental Investigation of the Flow Over Simple Two-Dimensional and Axi-Symmetric Bodies at Hypersonic Speeds. Jet Propulsion, Vol. 28, No. 2, February 1958.Google Scholar
27.Kopal, Z. (1947). Tables of Supersonic Flow Around Cones. Centre of Analysis, M.I.T. Technical Report No. 1, 1947.Google Scholar