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Features of Hypersonic Flow Past a Yawed Plate

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Abstract

Flow past a yawed plate in the strong interaction mode is considered in the case when the pressure at its trailing edge varies along the transverse coordinate instead of being constant. It is shown that the form of the expansion of the stream functions in the vicinity of the leading edge significantly changes in the case of the appearance of large transverse gradients of induced pressure, and the third term of the expansions should be taken into account.

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Funding

This study was supported by the Russian Foundation for Basic Research, project no. 18-01-00211.

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Authors and Affiliations

  1. Zhukovskii Central Institute of Aerohydrodynamics, 140160, Zhukovskii, Moscow oblast, Russia

    G. N. Dudin &  V. Ya. Neyland

Authors
  1. G. N. Dudin
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  2. V. Ya. Neyland
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Corresponding author

Correspondence to G. N. Dudin.

Additional information

Translated by V. Bukhanov

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Dudin, G.N., Neyland, V.Y. Features of Hypersonic Flow Past a Yawed Plate. Dokl. Phys. 64, 289–292 (2019). https://doi.org/10.1134/S1028335819070012

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  • DOI: https://doi.org/10.1134/S1028335819070012

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