Skip to main content
SpringerLink
Log in

Change in the Aerodynamic Characteristics of an Aerofoil as a Result of the One-Sided Force Action of its Surface Segment on the Transonic Flow Around it

  • Published:
Journal of Engineering Physics and Thermophysics Aims and scope

Mathematical simulation of the forced vibrations of a surface segment on one side of an aerofoil on the shock wave formed in the transonic flow around it has been performed. The influence of the vibrations of this segment in a wide frequency range on the quantitative and qualitative characteristics of the wave drag and lift of the aerofoil were investigated for the case of maximum amplitude of oscillations of the velocity of movement of the vibrating segment of the aerofoil, close to the velocity of the incident flow. It is shown that an additional lifting force arises in this case.

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. A. M. Lipanov, I. I. Lipatov, and S. A. Karskanov, Mathematical simulation of a high-velocity flow of a viscous gas around an aerofoil, Tr. Inst. Mekh. UrO RAN "Problems of Mechanics and Material Science," Izhevsk (2015), pp. 164–179.

  2. I. I. Lipatov and F. T. Vin′, Numerical simulation of the processes causing a buffeting of an ONERA M6 aerofoil, Nauchn. Vestn. Moskovsk. Gos. Univ. Grazhd. Aviatsii, No. 200, 133–140 (2014).

  3. S. M. Aul′chenko, V. P. Zamuraev, and A. P. Kalinina, Control of a transonic flow with the use of a local energy action, Zh. Tekh. Fiz., 81, Issue 11, 13–22 (2011).

  4. S. M. Aul′chenko, V. P. Zamuraev, and A. P. Kalinina, Numerical and analytical study of nonlinear effects of transonic flow past a wing airfoil on oscillation of its surface element, J. Eng. Phys. Thermophys., 87, No. 3, 635–647 (2014).

  5. A. N. Bogdanov, V. N. Diesperov, V. I. Zhuk, and G. L. Korolev, Transonic transition: features, attendant effects, models, approaches, possibilities of control of flow, Proc. XI Vseros. S′ezd Fundam. Probl. Teor. Prikl. Mekh., 20–24 August 2015, Kazan (2015), pp. 485–486.

Download references

Author information

Authors and Affiliations

  1. S. A. Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch of the Russian Academy of Sciences, 4/1 Institutskaya Str., Novosibirsk, 630090, Russia

    V. P. Zamuraev & A. P. Kalinina

  2. Novosibirsk State University, 2 Pirogov Str., Novosibirsk, 630090, Russia

    V. P. Zamuraev & A. P. Kalinina

Authors
  1. V. P. Zamuraev
    View author publications

    You can also search for this author in PubMed Google Scholar

  2. A. P. Kalinina
    View author publications

    You can also search for this author in PubMed Google Scholar

Corresponding author

Correspondence to V. P. Zamuraev.

Additional information

Translated from Inzhenerno-Fizicheskii Zhurnal, Vol. 90, No. 3, pp. 599–602, May–June, 2017.

Rights and permissions

Reprints and permissions

About this article

Check for updates. Verify currency and authenticity via CrossMark

Cite this article

Zamuraev, V.P., Kalinina, A.P. Change in the Aerodynamic Characteristics of an Aerofoil as a Result of the One-Sided Force Action of its Surface Segment on the Transonic Flow Around it. J Eng Phys Thermophy 90, 564–567 (2017). https://doi.org/10.1007/s10891-017-1601-2

Download citation

  • Received:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s10891-017-1601-2

Keywords

Search

Navigation