Skip to main content
SpringerLink
Log in

Numerical modeling of the pressure distribution on the axisymmetric body surface at the supersonic freestream interaction with a transversely blown gas jet

  • Published:
Thermophysics and Aeromechanics Aims and scope

Abstract

The results of numerical investigation of the interaction of a supersonic free stream with the Mach number of 3.85 with a transverse gas jet blown from the surface of an axisymmetric model located at zero angle of attack with respect to the flow are presented. The numerical modeling was conducted using the averaged Navier-Stokes equations employing the k-ω SST turbulence model. The investigation of the influence of the gas jet blowing on pressure redistribution over the axisymmetric model surface and on the formation of an additional transverse force and moment has also been conducted. The shift of the blowing orifice along the model length leads to a significant variation of arising forces and moments. A fundamental difference in the distribution of pressures over the surface at the jet blowing from the axisymmetric body and from a flat plate is shown.

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. I. I. Mazhul, V. F. Volkov, V. I. Zvegintsev, and I. V. Ivanov, Numerical simulation of the influence of the control surfaces deflection on the aerodynamics of a slender axisymmetric configuration, Thermophysics and Aeromechanics, 2016, Vol. 23, No. 1, P. 49–58.

    Article  ADS  Google Scholar 

  2. Physical Foundations of the Design and Functioning of Shooting and Cannon Artillery and Rocket Arms. Part II. Physical Foundations of the Design and Functioning of Rocket Arms: Textbook for Higher Schools, V. V. Vetrov and V. P. Strogalev (Eds.), Tula State Univ., Tula, 2007.

    Google Scholar 

  3. N. I. Sidnyaev, Computation of the parameters of a planar jet blown from a sublimating plate into the carrying away supersonic flow, Nauka i obrazovanie: electronnoe nauchnoe izdanie, Bauman Moscow State Techn. Univ., 2011, No. 11, P. 66–85.

    Google Scholar 

  4. V. I. Kornilov, Implementation of air injection into the turbulent boundary layer of aircraft wing using external pressurized flow, Thermophysics and Aeromechanics, 2017, Vol. 24, No. 2, P. 175–185.

    Article  ADS  Google Scholar 

  5. A. O. Beketaeva, Ye.S. Moisseyeva, and A.Zh. Naimanova, Numerical simulations of shock-wave interaction with a boundary layer in the plane supersonic flows with jet injection, Thermophysics and Aeromechanics, 2016, Vol. 23, No. 2, P. 173–183.

    Article  ADS  Google Scholar 

  6. J. Zhang, Y. D. Cui, J. Cai, and H. Dou, Numerical investigation of lateral jets over body of revolution in supersonic crossflow, J. Propulsion and Power, 2012, Vol. 28, No. 1, P. 33–45.

    Article  Google Scholar 

  7. D. Chai, Y. W. Fang, W. S. Peng, and P. F. Yang, Numerical investigation of lateral jet interaction effects on the hypersonic quasi-waverider vehicle, J. Aerospace Engng, 2015, Vol. 229, No. 14, P. 2671–2680.

    Google Scholar 

  8. A. Yu. Lutsenko, E. G. Stolyarova, and P. A. Chernuha, Jet control of flow parameters nearby flying vehicles of various purposes, Civil Aviation High Technologies, 2015, No. 212, P. 38–44.

    Google Scholar 

  9. J. Brandeis and J. Gill, Experimental investigation of super- and hypersonic jet interaction on missile configurations, J. Spacecraft and Rockets, 1998, Vol. 35, No. 3, P. 296–302.

    Article  ADS  Google Scholar 

  10. B. Stahl, H. Esch, and A. Gülhan, Experimental investigation of side jet interaction with a supersonic cross flow, Aerospace Sci. Technol., 2008, Vol. 12, No. 4, P. 269–275.

    Article  Google Scholar 

  11. V. Viti, R. Neel, and J. Schetz, Detailed flow physics of the supersonic jet interaction flow field, Phys. Fluids, 2009, P. 046101-1–046101-16.

    Google Scholar 

  12. R. Adeli and F. Seiler, Numerical flow visualisation of side jet/cross flow interaction, in: ISFV15 — 15th Int. Symp. on Flow Visualization, June 25–28, 2012, Minsk, Belarus.

    Google Scholar 

  13. P. Gnemmi, R. Adeli, and J. Longo, Computational comparisons of the interaction of a lateral jet on a supersonic generic missile, AIAA Paper, 2008, No. 2008-6883.

    Google Scholar 

  14. V. A. Kislovskiy and V. I. Zvegintsev, Redistribution of pressure along the surface of axisymmetric vehicle as a result of transverse gas jet blowing, in: Proc. XXV Conf. on High Energy Processes in Condensed Matter 2017: AIP Conference Proc., 2017, Vol. 1893, P. 030028-1–030028-5.

    Google Scholar 

Download references

Author information

Authors and Affiliations

  1. Khristianovich Institute of Theoretical and Applied Mechanics SB RAS, Novosibirsk, Russia

    V. A. Kislovskiy & V. I. Zvegintsev

Authors
  1. V. A. Kislovskiy
    View author publications

    You can also search for this author in PubMed Google Scholar

  2. V. I. Zvegintsev
    View author publications

    You can also search for this author in PubMed Google Scholar

Corresponding author

Correspondence to V. A. Kislovskiy.

Rights and permissions

Reprints and permissions

About this article

Check for updates. Verify currency and authenticity via CrossMark

Cite this article

Kislovskiy, V.A., Zvegintsev, V.I. Numerical modeling of the pressure distribution on the axisymmetric body surface at the supersonic freestream interaction with a transversely blown gas jet. Thermophys. Aeromech. 26, 19–26 (2019). https://doi.org/10.1134/S0869864319010037

Download citation

  • Received:

  • Revised:

  • Accepted:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1134/S0869864319010037

Key words

Search

Navigation