Skip to main content
SpringerLink
Log in

Formation of laminar lateral separation caused by a sustainer engine jet

  • Published:
Fluid Dynamics Aims and scope Submit manuscript

Abstract

The early stage of separation flow formation on a cylindrical surface immediately after the onset of jet exhaust from the base is investigated numerically for various values of the jet-to-ambient pressure ratio on the basis of the complete time-dependent Navier-Stokes equations, the energy equation and the equations for the transfer and diffusion of the exhaust gas concentration. The time dependence of the geometrical and gasdynamic parameters in the separation flow region is obtained for various flow regimes. It is found that the process is periodic with transition from the flow regime with an open separation zone to that with a closed zone, and vice versa, until the final flow regime is attained, which may be open, closed, or periodic.

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. P. Carrier and M. Sirieix, “Effets aérodynamiques de l'éclatement d'un jet de fusée,”Rech. Aéronaut., No. 89, 3 (1962).

    Google Scholar 

  2. L. J. Alpinieri and R. H. Adams, “Flow separation due to jet pluming,”AIAA J.,4, 1865 (1966).

    Google Scholar 

  3. R. H. Adams, “Wind tunnel testing techniques for gas-particle flows in rocket exhaust plumes,” AIAA Pap., No. 767 (1966).

  4. A. N. Shlyagun, “Interaction of a highly underexpanded supersonic jet with a hypersonic outer flow,”Uch. Zap. TsAGI,10, No. 3, 37 (1979).

    Google Scholar 

  5. A. C. H. Mace, N. C. Markatos, D. B. Spalding, and D. G. Tatchell, “Analysis of combustion in recirculating flow for rocket exhausts in supersonic streams,”J. Spacecr. Rockets,19, 557 (1982).

    Google Scholar 

  6. J. M. Klineberg, T. Kubota, and L. Lees, “Theory of exhaust-plume/boundary-layer interactions at supersonic speeds,”AIAA J.,10, 581 (1972).

    Google Scholar 

  7. E. V. Myshenkov and V. I. Myshenkov, “Regimes of laminar lateral flow separation due to jet exhaust,”Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 1, 132 (1994).

  8. B. Engquist and S. Osher, “One-sided difference approximation for non-linear conservation laws,”Math. Comput.,36, 321 (1981).

    Google Scholar 

  9. P. K. Sweby, “High resolution schemes using flux limiters for hyperbolic conservation laws,”SIAM J. Numer. Anal.,21, 995 (1984).

    Google Scholar 

Download references

Authors
  1. V. I. Myshenkov
    View author publications

    You can also search for this author in PubMed Google Scholar

  2. E. V. Myshenkov
    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. 4, pp. 122–130, July–August, 1995.

Rights and permissions

Reprints and permissions

About this article

Cite this article

Myshenkov, V.I., Myshenkov, E.V. Formation of laminar lateral separation caused by a sustainer engine jet. Fluid Dyn 30, 592–598 (1995). https://doi.org/10.1007/BF02030336

Download citation

  • Received:

  • Issue Date:

  • DOI: https://doi.org/10.1007/BF02030336

Keywords

Search

Navigation