Hostname: page-component-7479d7b7d-rvbq7 Total loading time: 0 Render date: 2024-07-12T12:43:01.769Z Has data issue: false hasContentIssue false
  • English
  • Français

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
Get access Rights & Permissions [Opens in a new window]

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

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