Article

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

  • S. M. Aul’chenkoAffiliated withS. A. Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch of the Russian Academy of Sciences Email author 
  • , V. P. ZamuraevAffiliated withS. A. Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch of the Russian Academy of Sciences
  • , A. P. KalininaAffiliated withS. A. Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch of the Russian Academy of Sciences

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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 flow body of revolution pulsed energy supply Euler equations