Yermolaev, Yuriy Gennadievich

Senior Research Scientist, Ph.D. in Physics and Mathematics

Khristianovich 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

  1. 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
  2. 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
  3. 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
  4. 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
  5. 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

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