Hostname: page-component-cd9895bd7-7cvxr Total loading time: 0 Render date: 2024-12-28T04:42:00.594Z Has data issue: false hasContentIssue false
  • English
  • Français

The Speed of Sound and Mach Number Effects

Published online by Cambridge University Press:  04 July 2016

W. G. Watson
W. G. Watson*
Affiliation:
Scottish Aviation Ltd.
Get access Rights & Permissions [Opens in a new window]

Extract

Since I have not been concerned with matters thermo-dynamic for some years, I have hesitated to enter the lists on the recent discussions on “The Speed of Sound and Mach Number Effects,” but I cannot let the comments of Mr. Naylor (Journal, January 1964, p. 63) and the reply by Messrs. Bragg and Smith stand without further comment.

I am in agreement with Mr. Naylor in the specific circumstances with which he deals, but I believe his concentration upon the polytropic efficiency obscures the more fundamental approach.

Type
Technical notes
Information
The Aeronautical Journal , Volume 68 , Issue 643 , July 1964 , pp. 485 - 487
Copyright
Copyright © Royal Aeronautical Society 1964

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

Watson, W. G. Nozzle Flow with Heat Transfer and Friction, Aircraft Engineering, October 1955.Google Scholar