Control of transonic flow past aircraft elements using different external energy sources
First Online: 25 November 2012 Received: 12 April 2012 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
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
Translated from Inzhenerno-Fizicheskii Zhurnal, Vol. 85, No. 6, pp. 1268–1272, November–December, 2012.
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