Skip to main content
SpringerLink
Log in

Interference of a Bow Shock with an Oblique Shock and an Isentropic Compression Wave

  • Published:
Fluid Dynamics Aims and scope Submit manuscript

Abstract

The features of the flow in the zone of interaction between a plane bow shock and an oblique shock or an isentropic compression wave are studied. The limiting interaction regimes are considered analytically, the similarity conditions are formulated, and the limiting values of the flow parameters are determined for the high-pressure compressed gas jet formed in the interference and for the body surface. On the basis of a numerical solution of the Euler equations the flow specifics in the neighborhood of the spreading line on the body are determined and ways of reducing the dynamic and thermal loadings on this line are proposed.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Log in via an institution

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Institutional subscriptions

Similar content being viewed by others

REFERENCES

  1. B. Edney, "Anomalous heat transfer and pressure distributions on blunt bodies at hypersonic speeds in the presence of an impinging shock," K. T. H. Abhandl. No. 239. Medd. Flugtekn. Forsok.-Anstalt., Report 115, Stockholm (1968).

  2. V.Ya. Borovoi, Gas Flow and Heat Transfer in the Zones of Interaction between Shock Waves and a Boundary Layer [in Russian], Mashinostroenie, Moscow (1983).

    Google Scholar 

  3. V. N. Gusev, "Limiting regimes of interaction between an external shock and the bow shock ahead of a body," Uch. Zap. TsAGI, 32, No. 1–2, 3 (2001).

    Google Scholar 

  4. S.K. Godunov, A.V. Zabrodin, and M.Ya. Ivanov et al., Numerical Solution of Multidimensional Gas Dynamic Problems [in Russian], Nauka, Moscow (1976).

    Google Scholar 

  5. V. P. Kolgan, "Application of the minimum derivative principle to construction of finite-difference schemes for calculating discontinuous gas dynamic solutions," Uch. Zap. TsAGI, 3, No. 6, 68 (1972).

    Google Scholar 

  6. V.Ya. Borovoi, A.Yu. Chinilov, V.N. Gusev, I.V. Struminskaya, J. Delery, and B. Chanetz, "Interference between a cylindrical bow shock and a plane oblique shock," AIAA Journal, 35, 1721 (1997).

    Google Scholar 

  7. W. Hayes and R. Probstein, Hypersonic Flow Theory, Academic Press, New York (1959).

    Google Scholar 

Download references

Authors
  1. V. N. Gusev
    View author publications

    You can also search for this author in PubMed Google Scholar

  2. A. Yu. Chinilov
    View author publications

    You can also search for this author in PubMed Google Scholar

Rights and permissions

Reprints and permissions

About this article

Cite this article

Gusev, V.N., Chinilov, A.Y. Interference of a Bow Shock with an Oblique Shock and an Isentropic Compression Wave. Fluid Dynamics 38, 612–619 (2003). https://doi.org/10.1023/A:1026334113926

Download citation

  • Issue Date:

  • DOI: https://doi.org/10.1023/A:1026334113926

Search

Navigation