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Numerical Simulation of the Interaction of a Mach Wave and a Boundary Layer on a Flat Plate

  • HEAT AND MASS TRANSFER AND PHYSICAL GASDYNAMICS
  • Published:
High Temperature Aims and scope

Abstract

Using direct numerical simulation, a problem of the interaction of a Mach wave with a boundary layer on a flat plate, streamlined by a supersonic perfect gas flow at the Mach number M = 2.5 is considered. The influence of the intensity of the incident Mach wave on the laminar-turbulent transition (LTT) is studied. It is shown that the incidence of a Mach wave with an amplitude of 5%, simulating the relative thickness of the roughness on the side wall of the wind tunnel, on the boundary layer leads to the formation of a turbulent wedge in the boundary layer on a flat plate.

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Funding

This study was carried out at Moscow Institute of Physics and Technology with financial support from the Russian Science Foundation (project code 21-19-00307).

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Authors and Affiliations

  1. Moscow Institute of Physics and Technology (National Research University), Dolgoprudny, Russia

    I. V. Egorov, N. K. Nguyen & N. V. Pal’chekovskaya

  2. Central Aerohydrodynamic Institute, Zhukovsky, Russia

    I. V. Egorov & N. V. Pal’chekovskaya

Authors
  1. I. V. Egorov
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  2. N. K. Nguyen
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  3. N. V. Pal’chekovskaya
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Correspondence to N. V. Pal’chekovskaya.

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Egorov, I.V., Nguyen, N.K. & Pal’chekovskaya, N.V. Numerical Simulation of the Interaction of a Mach Wave and a Boundary Layer on a Flat Plate. High Temp 61, 689–696 (2023). https://doi.org/10.1134/S0018151X23050036

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  • DOI: https://doi.org/10.1134/S0018151X23050036

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