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Control of transonic flow past aircraft elements using different external energy sources

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Journal of Engineering Physics and Thermophysics Aims and scope

A study has been made of the influence of pulsed-periodic energy supply on transonic regimes of flow past a body of revolution for different source models. The possibility of restructuring significantly the flow has been shown, which can serve as a basis for efficient control of flow past the entire aircraft and its elements alike.

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Authors and Affiliations

  1. S. A. Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch of the Russian Academy of Sciences, 4/1 Institutskaya Str., Novosibirsk, 630058, Russia

    S. M. Aul’chenko, V. P. Zamuraev & A. P. Kalinina

Authors
  1. S. M. Aul’chenko
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  2. V. P. Zamuraev
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  3. A. P. Kalinina
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Corresponding author

Correspondence to S. M. Aul’chenko.

Additional information

Translated from Inzhenerno-Fizicheskii Zhurnal, Vol. 85, No. 6, pp. 1268–1272, November–December, 2012.

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Aul’chenko, S.M., Zamuraev, V.P. & Kalinina, A.P. Control of transonic flow past aircraft elements using different external energy sources. J Eng Phys Thermophy 85, 1372–1377 (2012). https://doi.org/10.1007/s10891-012-0784-9

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  • DOI: https://doi.org/10.1007/s10891-012-0784-9

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