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XI.—Application of Relaxation Methods to Compressible Flow past a Double Wedge*

Published online by Cambridge University Press:  14 February 2012

A. R. Mitchell  and
D. E. Rutherford
A. R. Mitchell
Affiliation:
United College, University of St Andrews.
D. E. Rutherford
Affiliation:
United College, University of St Andrews.
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Synopsis

The relaxation technique of R. V. Southwell is shown to be applicable in certain cases to transonic problems. For a uniform stream with a low subsonic velocity impinging on a symmetrical 2-dimensional double wedge, an asymmetrical supersonic region can be isolated in the neighbourhood of the corner of the wedge, and the streamlines and the values of the Mach number within this supersonic region can be determined with the aid of relaxation methods. Difficulties must be expected to occur in the neighbourhood of the sonic line, but in the present problem these have been surmounted.

Type
Research Article
Information
Proceedings of the Royal Society of Edinburgh Section A: Mathematics , Volume 63 , Issue 2 , 1951 , pp. 139 - 154
Copyright
Copyright © Royal Society of Edinburgh 1951

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References

REFERENCES TO LITERATURE

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