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Development of disturbances generated by an electric discharge in the shock wave / boundary layer interaction zone

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Thermophysics and Aeromechanics Aims and scope

Abstract

The paper presents the results of experimental study of disturbances generated by an electric discharge. Observations are carried out in the zone of interaction of a shock wave and a boundary layer (the incident shock wave has the Mach number M = 1.43). Experiments were carried out in a supersonic wind tunnel with the unit Reynolds number Re1 = 11·106 1/m. The flow velocity was measured using the PIV method and hot-wire method. The artificial disturbances are generated by a periodic pulsed electric discharge; the discharge is allocated at the model surface upstream of the interaction zone. The discharge time is less than 100 ns: this enables creating a broadband disturbance inside the boundary layer. The method of phase-locked measurement with the ensemble averaging of realizations produces the spatial and temporal characteristics of disturbances generated in the interaction zone. The major growth of initial disturbances occurs in the shear layer behind the shock wave/boundary layer interaction zone (here the flow becomes turbulent).

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References

  1. P. Doerffer, C. Hirsch, J.-P. Dussauge, H. Babinsky, and G. Barakos, Unsteady effects of shock wave induced separation. N.Y.: Springer Science & Business Media, 2010, Vol. 114.

    Google Scholar 

  2. P.A. Polivanov, A.A. Sidorenko, and A.A. Maslov, Correlations study in shock wave/turbulent boundary layer interaction, Techn. Phys. Letters, 2010, Vol. 36, P. 104–107.

    Article  ADS  Google Scholar 

  3. P.A. Polivanov, A.A. Sidorenko, and A.A. Maslov, The influence of the laminar–turbulent transition on the interaction between the shock wave and boundary layer at a low supersonic Mach number, Techn. Phys. Letters, 2015, Vol. 41, P. 933–937.

    Article  ADS  Google Scholar 

  4. J.-P. Dussauge, R. Bur, T. Davidson, H. Babinsky, M. Bernardini, S. Pirozzoli, P. Dupont, S. Piponniau, L. Larchevêque, R. Giepman, F. Schrijer, B. Oudheusden, P. Polivanov, A. Sidorenko, D. Szubert, M. Braza, I. Asproulias, N. Simiriotis, J.-B. Tô, Y. Hoarau, A. Sansica, and N. Sandham, Wp-1 reference cases of laminar and turbulent interactions, Transition Location Effect on Shock Wave Boundary Layer Interaction: Experimental and Numerical Findings from the TFAST Project. 2021, Vol. 144, P. 25–127.

    Article  Google Scholar 

  5. H. Babinsky, P. Dupont, P. Polivanov, A. Sidorenko, R. Bur, R. Giepman, F. Schrijer, B. Oudheusden, A. Sansica, N. Sandham, M. Bernardini, S. Pirozzoli, T. Kwiatkowski, and J. Sznajder, Wp-2 basic investigation of transition effect, Transition Location Effect on Shock Wave Boundary Layer Interaction: Experimental and Numerical Findings from the TFAST Project. 2021, Vol. 144, P. 129–225.

    Article  Google Scholar 

  6. P.A. Polivanov, A.A. Sidorenko, and A.A. Maslov, Transition effect on shock wave/boundary layer interaction at M = 1.47, in: 53rd AIAA Aerospace Sci. Meeting. 2015 (Kissimmee, Florida, USA, 5–9 Jan. 2015): Conf. Papers. S. l, 2015, Vol. 18, P. 15299–15309.

    Google Scholar 

  7. A.A. Sidorenko, A.D. Budovsky, P.A. Polivanov, O.I. Vishnyakov, V.G. Sudakov, and V.N. Ischenko, Suppression of transonic buffet with plasma vortex generators, Thermophysics and Aeromechanics, 2019, Vol. 26, No. 4, P. 465–480.

    Article  ADS  Google Scholar 

  8. P.A. Polivanov and A.A. Sidorenko, Suppressing a laminar flow separation zone by spark discharge at Mach number M = 1.43, Techn. Phys. Letters, 2018, Vol. 44, P. 833–836.

    Article  ADS  Google Scholar 

  9. S.A. Gaponov and A.A. Maslov, Disturbances Developing in Compressible Flows, Nauka, Novosibirsk 1980.

    Google Scholar 

  10. A.A. Yatskikh, Yu.G. Ermolaev, A.D. Kosinov, and N.V. Semionov, Evolution of wave packets in supersonic flat-plate boundary layer, Thermophysics and Aeromechanics, 2015, Vol. 22, No. 1, P. 17–27.

    Article  ADS  Google Scholar 

  11. G.L. Kolosov, A.D. Kosinov, A.N. Semenov, and A.A. Yatskikh, Experimental and numerical investigation of controlled disturbances development from two sources in supersonic boundary layer, Adv. Aerodynamics, 2019, Vol. 1, No. 1, P. 1–13.

    Article  Google Scholar 

  12. I. Moralev, I. Selivonin, and M. Ustinov, On the stochastic forcing of the boundary layer by plasma actuators, Exp. Fluids, 2019, Vol. 60, P. 1–9.

    Article  Google Scholar 

  13. O.I. Vishnyakov and P.A. Polivanov, Evolution of artificial disturbances in separation area of laminar boundary layer for M = 1.43, AIP Conf. Proc. XX Inter. Conf. on the Methods of Aerophys. Res. (ICMAR-2020) (Novosibirsk, 1–7 Nov. 2020). S. l.: AIP Publ. LLC, 2021. Vol. 2351, No. 1, P. 030019-1–030019-7.

    Google Scholar 

  14. O.I. Vishnyakov, P.A. Polivanov, and A.A. Sidorenko, On the problem of using particle image velocimetry for measurements in high-velocity thin shear layers, J. Appl. Mech. Techn. Phys., 2020, Vol. 61, P. 748–756.

    Article  ADS  Google Scholar 

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Authors and Affiliations

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

    O. I. Vishnyakov, P. A. Polivanov, A. A. Sidorenko & A. D. Budovsky

Authors
  1. O. I. Vishnyakov
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  2. P. A. Polivanov
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  3. A. A. Sidorenko
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  4. A. D. Budovsky
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Corresponding author

Correspondence to O. I. Vishnyakov.

Additional information

Experimental research was performed under the state assignment for ITAM SB RAS. The methodology of introducing the artificial disturbances was supported by the grant from the Russian Science Foundation (grant 18-19-00547). Research was performed using equipment for Core Facilities Center “Mechanics” of I TAM SB RAS.

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Vishnyakov, O.I., Polivanov, P.A., Sidorenko, A.A. et al. Development of disturbances generated by an electric discharge in the shock wave / boundary layer interaction zone. Thermophys. Aeromech. 30, 673–681 (2023). https://doi.org/10.1134/S0869864323040078

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  • DOI: https://doi.org/10.1134/S0869864323040078

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