Skip to main content
SpringerLink
Log in

Design of multimode axisymmetric hypersonic nozzles with the use of optimization methods

  • Hydrogasdynamics in Technological Processes
  • Published:
Journal of Engineering Physics and Thermophysics Aims and scope

On the basis of the solution of direct problems with the use of various medium models and numerical methods of integration of gas flow equations, methods for designing super- and hypersonic nozzles have been developed. Multimode nozzles in the ranges of Mach numbers 8–14 and 14–20 satisfying given conditions have been designed.

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. O. N. Katskova, Calculation of Equilibrium Gas Flows in Supersonic Nozzles [in Russian], VTs AN SSSR, Moscow (1964).

    Google Scholar 

  2. A. P. Byrkin and V. P. Verkhovskii, Supersonic Axisymmetric Contoured Nozzle of a Wind Tunnel, Patent 1528116 of the Russian Federation. Published 08.02.93.

  3. Yu. S. Volkov and V. M. Galkin, On the choice of approximations in direct problems of nozzle design, Zh. Vych. Mat. Mat. Fiz., 47, No. 5, 923–936 (2007).

    MathSciNet  Google Scholar 

  4. Yu. S. Volkov and V. M. Galkin, Optimization of a multimode wind tunnel, in: Proc. of the Conf. "Fundamental and Applied Problems of Modern Mechanics" [in Russian], Izd. Tomsk. Univ., Tomsk (2006), pp. 356–357.

  5. S. M. Aulchenko and V. P. Zamuraev, Design of a multi-regime nozzle by means of a direct method of numerical optimization, Proc. 12th Int. Conf. on the Methods of Aerophysical Research, Pt. 1, Novosibirsk (2004), pp. 15–18.

  6. J. Korte, Aerodynamic design of axisymmetric hypersonic wind-tunnel nozzle using a least-squares/parabolized Navier-Stokes procedure, J. Spacecraft Rockets, 29, No. 5, 685–691 (1992).

    Article  Google Scholar 

  7. S. M. Aulchenko, V. M. Galkin, V. I. Zveginzev, and A. N. Shiplyk, Design of a multimode axisymmetric nozzle for a hypersonic wind tunnel by methods of numerical optimization, 14 Int. Conf. on the Methods of Aerophysical Research, 30 June–6 July 2008, Abstracts, Pt. 2, Novosibirsk (2008), pp. 221–222.

  8. A. M. Kharitonov, V. I. Zvegintsev, L. G. Vasenev, et al., Investigation of the characteristics of the AT-303 hypersonic wind tunnel, Pt. 1. Velocity Fields, Teplofiz. Aéromekh., 13, No. 1, 1–17 (2006).

    Google Scholar 

Download references

Author information

Authors and Affiliations

  1. S. A. Khristianovich Institute of Theoretical and Applied Mechanics, 4/1 Institutskaya Str., Novosibirsk, 630090, Russia

    S. M. Aulchenko, V. I. Zvegintsev & A. N. Shiplyuk

  2. Tomsk Polytechnical University, 30 Lenin Ave., Tomsk, 634050, Russia

    V. M. Galkin

Authors
  1. S. M. Aulchenko
    View author publications

    You can also search for this author in PubMed Google Scholar

  2. V. M. Galkin
    View author publications

    You can also search for this author in PubMed Google Scholar

  3. V. I. Zvegintsev
    View author publications

    You can also search for this author in PubMed Google Scholar

  4. A. N. Shiplyuk
    View author publications

    You can also search for this author in PubMed Google Scholar

Corresponding author

Correspondence to S. M. Aulchenko.

Additional information

Translated from Inzhenerno-Fizicheskii Zhurnal, Vol. 82, No. 6, pp. 1109–1112, November–December, 2009.

Rights and permissions

Reprints and permissions

About this article

Cite this article

Aulchenko, S.M., Galkin, V.M., Zvegintsev, V.I. et al. Design of multimode axisymmetric hypersonic nozzles with the use of optimization methods. J Eng Phys Thermophy 82, 1127–1131 (2009). https://doi.org/10.1007/s10891-010-0306-6

Download citation

  • Received:

  • Revised:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s10891-010-0306-6

Keywords

Search

Navigation