Hostname: page-component-cd9895bd7-hc48f Total loading time: 0 Render date: 2024-12-18T16:00:04.416Z Has data issue: false hasContentIssue false
  • English
  • Français

The steady two-dimensional reflexion of an oblique partly dispersed shock wave from a plane wall

Published online by Cambridge University Press:  29 March 2006

H. Buggisch
H. Buggisch
Affiliation:
Fachbereich Mechanik, Technische Hochschule, Darmstadt, Germany
Get access Rights & Permissions [Opens in a new window]

Abstract

The steady two-dimensional problem of reflexion of an oblique partly dispersed plane shock wave from a plane wall is studied analytically. Viscosity, diffusion and heat conduction are neglected. The thermodynamic state of the gas is assumed to be determined by the instantaneous values of the specific entropy s, pressure p and a finite number of internal state variables. Results for the flow field behind the reflected shock are obtained by a perturbation method which is based on the assumption that the influence of relaxation is relatively weak.

Type
Research Article
Information
Journal of Fluid Mechanics , Volume 61 , Issue 1 , 23 October 1973 , pp. 159 - 172
Copyright
© 1973 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

Baganoff, D. 1965 Experiments on the wall-pressure history in shock-reflexion processes. J. Fluid Mech. 23, 209–228.Google Scholar
Becker, E. 1972 Chemically reacting flows. Ann. Rev. Fluid Mech. 4, 155–193.Google Scholar
Becker, E. & Böhme, G. 1969 Gasdynamics, a Series of Monographs (ed. P. P. Wegener), vol. 1. Non-Equilibrium Flows, part 1. Marcel Dekker.
Buggisch, H. 1969 Analytische Untersuchungen zur Reflexion von Verdichtungsstößen in relaxierenden Gasen. Dissertation D 17, Darmstadt.
Buggisch, H. 1970 Analytische Untersuchung zur Reflexion teildispergierter Wellen in relaxierenden Gasen. Z. angew. Math. Mech. 50, 169–170.Google Scholar
Chu, B. T. 1952 On weak interaction of strong shock and Mach waves generated downstream of the shock. J. Aero. Sci. 19, 433–446.Google Scholar
Johannesen, N. H., Bird, G. A. & Zienkiewicz, H. K. 1967 Theoretical and experimental investigation of the reflexion of normal shock waves with vibrational relaxation. J. Fluid Mech. 30, 51–65.Google Scholar
Lighthill, M. J. 1949 The flow behind a stationary shock. Phil. Mag. 40, 214–220.Google Scholar
Ockendon, H. & Spence, D. A. 1969 Non-linear wave propagation in a relaxing gas. J. Fluid Mech. 39, 329–345.Google Scholar
Smith, J. A. 1968 Experimentally determined structure of the shock reflection process in ionizing xenon. Phys. Fluids, 11, 2150–2161.Google Scholar
Spence, D. A. 1961 Unsteady shock propagation in a relaxing gas. Proc. Roy. Soc. A 264, 221.Google Scholar