Hostname: page-component-586b7cd67f-r5fsc Total loading time: 0 Render date: 2024-11-22T05:10:15.617Z Has data issue: false hasContentIssue false
  • English
  • Français

Inversion of the Prandtl-Meyer relation

Published online by Cambridge University Press:  04 July 2016

I. M. Hall
I. M. Hall*
Affiliation:
Department of the Mechanics of Fluids, University of Manchester
Get access Rights & Permissions [Opens in a new window]

Summary

A simple rational fraction is derived which gives the Mach number with an error of less than 0·05 per cent for a given value of the Prandtl-Meyer function.

Type
Technical note
Information
The Aeronautical Journal , Volume 79 , Issue 777 , September 1975 , pp. 417 - 418
Copyright
Copyright © Royal Aeronautical Society 1975 

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. Fraser, S. M. Calculation of Mach number from given turning angle in supersonic isentropic flow. The Aeronautical Journal, Vol 79, No 770, pp 95–96, February 1975.Google Scholar