Skip to main content
SpringerLink
Log in

Gas injection from the surface of a triangular plate in a hypersonic flow

  • Published:
Fluid Dynamics Aims and scope Submit manuscript

Abstract

The flow formed as a result of gas injection through the permeable surface of a triangular plate is investigated in the regime of strong viscous-inviscid interaction between the hypersonic flow and the laminar boundary layer. The features of the flow past strongly cooled surfaces with the formation of supercritical and subcritical flow regions in the boundary layer are studied. The injected gas distribution ensuring the existence of self-similar solutions in the supercritical flow regions is obtained.

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. G. N. Dudin and D. O. Lyzhin, “A method of calculating the strong viscous interaction on a delta wing,”Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 4, 119 (1983).

  2. V. Ya. Neiland, “Gas injection into a hypersonic flow,”Uch. Zap. TsAGI,3, No. 6, 29 (1972).

    Google Scholar 

  3. V. Ya. Neiland, “Theory of interaction of a hypersonic flow with a boundary layer for two- and three-dimensional separation flows. Part 1. Three-dimensional flows,”Uch. Zap. TsAGI,5, No. 2, 70 (1974).

    Google Scholar 

  4. G. N. Dudin and I. I. Lipatov, “Supercritical regime of hypersonic flow past a delta wing,”Zh. Prikl. Mekh. Tekhn. Fiz., No. 3, 100 (1985).

    Google Scholar 

  5. G. N. Dudin, “Influence of intense surface cooling on hypersonic viscous flow past a delta wing,”Izv. Ross. Akad. Nauk, Mekh. Zhidk. Gaza, No. 4, 57 (1998).

    Google Scholar 

  6. W. D. Hayes and R. F. Probstein,Hypersonic Flow Theory, Academic Press, New York (1966).

    MATH  Google Scholar 

  7. G. N. Dudin, “Hypersonic boundary layer flow on bodies of power-law shape in the presence of mass transfer,”Zh. Prikl. Mekh. Tekhn. Fiz., No. 5, 73 (1979).

  8. G. N. Dudin, “On the existence of self-similar solutions in the supercritical region on a delta wing in a hypersonic flow,”Izv. Ross. Akad. Nauk, Mekh. Zhidk. Gaza, No. 2, 156 (1997).

Download references

Authors
  1. G. N. Dudin
    View author publications

    You can also search for this author in PubMed Google Scholar

Additional information

Moscow. Translated from Izvestiya Rossiiskoi Akademii Nauk, Mekhanika Zhidkosti i Gaza, No. 1, pp. 125–133, January–February, 2000.

The study was carried out with the support of the Russian Foundation for Basic Research (project No. 96-01-01391).

Rights and permissions

Reprints and permissions

About this article

Cite this article

Dudin, G.N. Gas injection from the surface of a triangular plate in a hypersonic flow. Fluid Dyn 35, 101–107 (2000). https://doi.org/10.1007/BF02698794

Download citation

  • Received:

  • Issue Date:

  • DOI: https://doi.org/10.1007/BF02698794

Keywords

Search

Navigation