Fluid Dynamics

, Volume 21, Issue 5, pp 789–794 | Cite as

Numerical simulation of shock wave intersections

  • Yu. M. Lipnitskii
  • A. V. Panasenko
Article
  • 48 Downloads

Abstract

A large number of papers, generalized and classified in [1, 2], have been devoted to unsteady gas flows arising in shock wave interaction. Experimental results [3–5] and theoretical analysis [6–9] indicate that the most interesting and least studied types of interaction arise in cases when there are several shock waves. At the same time, nonlinear effects, which depend largely on the nature of the shock wave intersections, become appreciable. Regions of existence of different types, of plane shock wave intersections have been analyzed in [10–13]. It has been shown that in a number of cases the simultaneous existence of different types of intersections is possible. The aim of the present paper is to study unsteady shock wave intersections in the framework of a numerical solution of the axisymmetric boundary-value problem that arises in the diffraction of a plane shock wave on a cone in a supersonic gas flow. Flow regimes that augment the experimental data of [3–5] and the theoretical analysis of [9] are considered.

Keywords

Experimental Data Shock Wave Theoretical Analysis Flow Regime Nonlinear Effect 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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Copyright information

© Plenum Publishing Corporation 1987

Authors and Affiliations

  • Yu. M. Lipnitskii
    • 1
  • A. V. Panasenko
    • 1
  1. 1.Moscow

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