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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

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