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Simulation of the Laminar–Turbulent Transition by Applying Dissipative Numerical Schemes

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Abstract

The applicability of a low-order monotone shock-capturing scheme to the simulation of the laminar–turbulent transition is demonstrated. The laminar–turbulent transition is simulated in a supersonic boundary layer over a flat plate at a Mach number of 3. The numerical results are compared with results of other authors based on low-dissipative schemes. The spectral characteristics of disturbances in the linear and nonlinear development regions, the structure of the transient flow, and averaged boundary layer characteristics are compared.

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Funding

This work was performed at the Moscow Institute of Physics and Technology and was supported by the Russian Science Foundation (project no. 19-79-10132) with the use of computing resources of the federal collective use center Complex for Simulation and Data Processing for Mega-science Facilities at NRC “Kurchatov Institute,” http://ckp.nrcki.ru/.

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Authors and Affiliations

  1. Moscow Institute of Physics and Technology (National Research University), 141701, Dolgoprudnyi, Moscow oblast, Russia

    I. V. Egorov, N. C. Nguyen & P. V. Chuvakhov

  2. Central Aerohydrodynamic Institute (TsAGI), National Research Center “Zhukovsky Institute”, 140180, Zhukovskii, Moscow oblast, Russia

    I. V. Egorov & P. V. Chuvakhov

  3. Hanoi Industrial University, Hanoi, Vietnam

    T. S. Nguyen

Authors
  1. I. V. Egorov
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  2. N. C. Nguyen
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  3. T. S. Nguyen
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  4. P. V. Chuvakhov
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Corresponding author

Correspondence to N. C. Nguyen.

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Translated by I. Ruzanova

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Egorov, I.V., Nguyen, N.C., Nguyen, T.S. et al. Simulation of the Laminar–Turbulent Transition by Applying Dissipative Numerical Schemes. Comput. Math. and Math. Phys. 61, 254–266 (2021). https://doi.org/10.1134/S0965542521020081

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  • DOI: https://doi.org/10.1134/S0965542521020081

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