Yermolaev, Yuriy Gennadievich
Senior Research Scientist, Ph.D. in Physics and MathematicsKhristianovich Institute of Theoretical and Applied Mechanics of SB RAS
http://www.itam.nsc.ru
Russia, 630090, Novosibirsk, 4/1, Institutskaya Str.
Phone: +7(383) 330-85-34, Fax: +7(383) 330-72-68
Reports list
- Lysenko V.I.*, Smorodsky B.V.*, Yermolaev Y.G.*, Гапонов С.А.*, Zubkov N.**, Kosinov A.D.*
Experimental Investigation of influence of heavy gas blowing into the supersonic boundary layer on its laminar-turbulent transition
*Khristianovich Institute of Theoretical and Applied Mechanics of SB RAS (Novosibirsk), Russia
**МВТУ им.Баумана (Moscow), Russia - Kolosov G.*, Kosinov A.D.*, Semionov N.*, Yermolaev Y.G.*
Linear and nonlinear development of controlled stationary and travelling disturbances in the supersonic boundary layer on a swept wing at Mach 2 and 2.5
*Khristianovich Institute of Theoretical and Applied Mechanics of SB RAS (Novosibirsk), Russia - Panina A.V.*, Kosinov A.D.*, Semionov N.*, Yermolaev Y.G.*
On the oblique breakdown mechanism in a supersonic boundary layer on a swept wing at Mach 2
*Khristianovich Institute of Theoretical and Applied Mechanics of SB RAS (Novosibirsk), Russia - Yatskikh A.*, Kosinov A.D.*, Yermolaev Y.G.*, Semionov N.*, Kolosov G.*, Panina A.V.*
The laminar-turbulent transition diagrams of a two-dimensional supersonic boundary layer at Mach number M = 2.5
*Khristianovich Institute of Theoretical and Applied Mechanics of SB RAS (Novosibirsk), Russia - Yermolaev Y.G.*, Yatskikh A.*, Kosinov A.D.*, Semionov N.*
Распространение волнового пакета в пограничном слое скользящего крыла при числе Маха 2
*Khristianovich Institute of Theoretical and Applied Mechanics of SB RAS (Novosibirsk), Russia