Journal of Engineering Physics and Thermophysics

, Volume 85, Issue 6, pp 1372–1377

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

Authors

    • S. A. Khristianovich Institute of Theoretical and Applied MechanicsSiberian Branch of the Russian Academy of Sciences
  • V. P. Zamuraev
    • S. A. Khristianovich Institute of Theoretical and Applied MechanicsSiberian Branch of the Russian Academy of Sciences
  • A. P. Kalinina
    • S. A. Khristianovich Institute of Theoretical and Applied MechanicsSiberian Branch of the Russian Academy of Sciences
Article

DOI: 10.1007/s10891-012-0784-9

Cite this article as:
Aul’chenko, S.M., Zamuraev, V.P. & Kalinina, A.P. J Eng Phys Thermophy (2012) 85: 1372. doi:10.1007/s10891-012-0784-9
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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.

Keywords

transonic flowbody of revolutionpulsed energy supplyEuler equations
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© Springer Science+Business Media New York 2012