Hostname: page-component-78c5997874-fbnjt Total loading time: 0 Render date: 2024-11-13T01:26:15.300Z Has data issue: false hasContentIssue false
  • English
  • Français

Extreme temperatures in shock-wave interactions with rarefaction waves

Published online by Cambridge University Press:  28 March 2006

G. A. Bird
G. A. Bird
Affiliation:
Department of Aeronautical Engineering, The University of Sydney, Sydney, Australia
Get access Rights & Permissions [Opens in a new window]

Abstract

The method of characteristics is used to calculate numerical solutions for the head-on collision of a shock wave with a centred rarefaction wave in the onedimensional unsteady flow of a perfect gas. It is found that, for sufficiently strong shock waves, the rate of increase in the strength of the shock as it propagates through the rarefaction is so great that the temperature behind the shock reaches extreme values.

Type
Research Article
Information
Journal of Fluid Mechanics , Volume 15 , Issue 2 , February 1963 , pp. 282 - 288
Copyright
© 1963 Cambridge University Press

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

Bird, G. A. 1961 J. Fluid Mech. 11, 180.
Courant, R. & Friedrichs, K. O. 1948 Supersonic Flow and Shock Waves. New York: Interscience.
Gould, D. G. 1952 Inst. of Aerophysics, UTIA Rep. no. 17.
Greenspan, H. P. & Butler, D. S. 1962 J. Fluid Mech. 13, 101.
Rosciszewski, J. 1960 J. Fluid Mech. 8, 337.
Whitham, G. B. 1958 J. Fluid Mech. 4, 337.