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Methods of Controlling Flows under the Strong Hypersonic Interaction Conditions

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Abstract—

The methods of the flow control in a laminar boundary layer at local surface cooling are studied. The dependence of the velocity of disturbance propagation upstream on the temperature factor of the body surface is obtained. The methods of controlling the boundary layer flow under the strong viscous-inviscid interaction conditions by means of suppressing the upstream disturbance propagation are investigated.

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Funding

The study is supported by the Ministry of Education and Science of the Russian Federation (contract 14.G39.31.0001 of February 13, 2017) and the Russian Foundation for Basic Research (project 17-01-00129 а).

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Authors and Affiliations

  1. Central Aerohydrodynamic Institute (TsAGI), ul. Zhukovskogo 1, 140180, Zhukovsky, Moscow oblast, Russia

    I. I. Lipatov

  2. Moscow Institute of Sciences and Technology, Institutski per. 9, 141701, Dolgoprudny, Moscow oblast, Russia

    I. I. Lipatov & V. K. Fam

Authors
  1. I. I. Lipatov
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  2. V. K. Fam
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Correspondence to I. I. Lipatov or V. K. Fam.

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The Authors declare no potential conflicts of interest with respect to the research, authorship, and/or publication of this article.

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Translated by M. Lebedev

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Lipatov, I.I., Fam, V.K. Methods of Controlling Flows under the Strong Hypersonic Interaction Conditions. Fluid Dyn 55, 220–230 (2020). https://doi.org/10.1134/S0015462820020093

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  • DOI: https://doi.org/10.1134/S0015462820020093

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