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Iterative Solutions of the Equations Jor Plane Oblique Shock Waves

Published online by Cambridge University Press:  04 July 2016

A. R. Collar
A. R. Collar*
Affiliation:
Department of Aeronautical Engineering, University of Bristol
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Extract

If a plane oblique shock wave, inclined to the free stream at the angle ε, is produced in two-dimensional supersonic flow of Mach number M by (for example) a wedge which deflects the flow through an angle δ, the equation connecting these quantities may be written

In this form, δ is given explicitly when M, ε are fixed. Similarly, we may obtain M explicitly when ε, δ are fixed; equation (1) may be written (see, for example, Liepmann and Puckett, Equation 4.27)

Type
Technical Notes
Information
The Aeronautical Journal , Volume 63 , Issue 587 , November 1959 , pp. 669 - 672
Copyright
Copyright © Royal Aeronautical Society 1959

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References

1.Liepmann, H. W. and Puckett, A. E. (1947). Introduction to Aerodynamics of a Compressible Fluid. Wiley and Sons, New York, 1947.Google Scholar