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Supersonic Cone with Surface Blowing

Published online by Cambridge University Press:  07 June 2016

E Carafoli  and
C Berbente
E Carafoli
Affiliation:
Polytechnic Institute of Bucharest
C Berbente
Affiliation:
Polytechnic Institute of Bucharest
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Summary

The velocity field around a circular cone in supersonic flow is determined by considering fluid injection and suction through the porous wall of the body. By using a new method of linearisation of the equations of motion, analytical formulae are obtained which yield almost exact results, as compared with numerical calculations. In addition, the method proposed suggests new problems related to fluid injection and suction which are important for practical applications.

Information

Type
Research Article
Information
Aeronautical Quarterly , Volume 27 , Issue 4 , November 1976 , pp. 243 - 256
Copyright
Copyright © Royal Aeronautical Society. 1976

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References

1 Aroesty, J Davis, S H Inviscid cone flows with surface mass transfer, AIAA Journal, Vol 4, p 1830, 1966.CrossRefGoogle Scholar
2 Emanuel, G Blowing from a porous cone or wedge when the contact surface is straight, AIAA Journal, Vol 5, p 534, 1967.CrossRefGoogle Scholar
3 Kalinin, EM Aerodynamics of the porous cone, Mechanics of Liquids and Gases (in Russian), No 1, 1969.Google Scholar
4 Carafoli, E Berbente, C Supersonic-hypersonic motion part a circular porous cone, l’Aeronautica, Missili e Spazio, Vol 5, p 309, 1972.Google Scholar
5 Carafoli, E High Speed Aerodynamics, Ed.Technica, , Bucuresti, and Pergamon Press, 1956.Google Scholar
6 Carafoli, E Berbente, C The supersonic-hypersonic flow around a circular cone with normal blowing or suction through the surface. Mechanics Research Communications, Vol 1, pp 239–244, 1974.Google Scholar
7 Kubardin, Yu A et al Atlas of Gasdynamic Functions under High Speeds and Temperatures of the Flow (in Russian). Gosudarst.Energ.Izd. Moskva/Leningrad, 1961.Google Scholar
8 Langefeld, W, Uberschall-Umströmung von spitzen und Strumpfen Kegelcörpern im Anstellwinkelbereich von 0° bis 45°, Report, Technische Hochschule, Aachen, 20.07.1971.Google Scholar
9 Hantsche, W Wendt, H Cones in supersonic flow (Mit Uberschallgeschwindigkeit angeblasene Kegelspitzen). Jahrbuch 1942 der deutschen Luftfahrtforschung, pp 180–190.Google Scholar
10 Hantsche, W Wendt, H Tables for Supersonic Flow around Right Circular Cones at Zero Angle of Attack. NASA Special Publication 300 4, 1964.Google Scholar
11 Taylor, G I Maccoll, J W Proc. Roy. Soc. Series A, Vol 139, p 278, 1933.Google Scholar