Skip to main content
SpringerLink
Log in

Laminarization of boundary layer flow on a vibrating wing

  • Published:
Fluid Dynamics Aims and scope Submit manuscript

Abstract

A new type of Tollmien-Schlichting wave excitation, experimentally detected in [6] in investigating the unsteady perturbation field downstream from roughness on the surface of a vibrating wing, is studied. It is shown that the generation mechanism consists in the nonlinear interaction between the unsteady disturbance produced by the vibrations of the smooth wall and the steady nonuniformity of the boundary layer above the roughness.

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. Yu. S. Kachanov, V. V. Kozlov, and V. Ya. Levchenko,Onset of Boundary Layer Turbulence [in Russian], Nauka, Novosibirsk (1982).

    Google Scholar 

  2. E. D. Terent'ev, “Linear problem of a harmonic vibrator vibrating at supercritical frequencies in the subsonic boundary layer,”Prikl. Mat. Mekh.,48, 264 (1984).

    Google Scholar 

  3. A. V. Fedorov, “Excitation of Tollmien-Schlichting waves in a boundary layer by a periodic external source localized on the body surface,”Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 6, 36 (1984).

    Google Scholar 

  4. S. V. Manuilovich, “Sensitivity of subsonic flow to oscillations localized at the base of the boundary layer,”Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 4, 63 (1988).

    Google Scholar 

  5. A. A. Pilipenko and G. K. Shapovalov, “Effect of the vibration of the model on laminar-turbulent boundary layer transition,”Uch. Zap. TsACI,17, 41 (1986).

    Google Scholar 

  6. I. A. Belov and V. M. Litvinov, “Possibility of suppressing Tollmien-Schlichting waves and delaying laminar-turbulent transition on a vibrating surface,” Preprint No. 30 [in Russian], Central Aerohydrodynamic Institute, Moscow (1991).

    Google Scholar 

  7. S. V. Manuilovich, “Possibility of suppressing acoustically generated Tollmien-Schlichting waves,”Dokl. Akad. Nauk SSSR,313, 280 (1990).

    Google Scholar 

  8. V. S. Kosorygin and N. F. Polyakov, “Self-destruction of unstable laminar boundary layer waves,” Preprint No. 11 [in Russian], Institute of Theoretical and Applied Mechanics, Siberian Division of the USSR Academy of Sciences, Novosibirsk (1990).

    Google Scholar 

  9. L. D. Landau and E. M. Lifshitz,Hydrodynamics [in Russian], Nauka, Moscow (1986).

    Google Scholar 

  10. E. V. Bogdanova and O. S. Ryzhov, “Disturbances generated by oscillators in a viscous flow at supercritical frequencies,”Zh. Prikl. Mekh. Tekh. Fiz., No. 4, 65 (1982).

    Google Scholar 

  11. S. V. Manuilovich, “A method of laminarizing the boundary layer on a vibrating wing,”Dokl. Akad. Nauk SSSR,322, 52 (1992).

    Google Scholar 

Download references

Author information

Authors and Affiliations

  1. Moscow

    S. V. Manuilovich

Authors
  1. S. V. Manuilovich
    View author publications

    You can also search for this author in PubMed Google Scholar

Additional information

Translated from Izvestiya Rossiiskoi Akademii Nauk, Mekhanika Zhidkosti i Gaza, No.2, pp. 26–34, March–April, 1993.

Rights and permissions

Reprints and permissions

About this article

Cite this article

Manuilovich, S.V. Laminarization of boundary layer flow on a vibrating wing. Fluid Dyn 28, 177–183 (1993). https://doi.org/10.1007/BF01051204

Download citation

  • Received:

  • Issue Date:

  • DOI: https://doi.org/10.1007/BF01051204

Keywords

Search

Navigation