CONTROLLING OF THE STREAMLINE OF ELEMENTS OF THE AIRPLANE BY MEANS OF THE EXTERNAL ENERGY SUPPLY

Sergey M. Aulchenko
1. Khristianovich Institute of Theoretical and Applied Mechanics SB RAS Novosibirsk, Russian Federation
aultch@itam.nsc.ru
Vladimir P. Zamuraev
1. Khristianovich Institute of Theoretical and Applied Mechanics SB RAS Novosibirsk, Russian Federation
2. Novosibirsk State University Novosibirsk, Russian Federation
zamuraev@itam.nsc.ru
Anna P. Kalinina
1. Khristianovich Institute of Theoretical and Applied Mechanics SB RAS Novosibirsk, Russian Federation
2. Novosibirsk State University Novosibirsk, Russian Federation
a_p_kalinina@mail.ru
The material was received by the Editorial Board: 08.02.2012
The studies of acting of pulsed-periodic energy supply on the transonic flow regimes of streamline of the body of revolution were performed for different models of the energy source. The possibility of a significant restructuring of the flow, which can serve as a basis for effective control of streamline of as a whole aircraft and its components was demonstrated.

Keywords:
transonic flow, the body of revolution, pulse energy supply, the Euler equations. 
УДК 533.6.011

CONTROLLING OF THE STREAMLINE OF ELEMENTS OF THE AIRPLANE BY MEANS OF THE EXTERNAL ENERGY SUPPLY
References: Aulchenko S. M., Zamuraev V. P., Kalinina A. P. CONTROLLING OF THE STREAMLINE OF ELEMENTS OF THE AIRPLANE BY MEANS OF THE EXTERNAL ENERGY SUPPLY. Vestnik NSU. Series: Physics. 2012, vol. 7, no. 3. P. 57–61 (in Russ.). DOI: 10.54362/1818-7919-2012-7-3-57-61