Modelling of local heating/cooling effect on laminar-turbulent transition in supersonic flows with engineering correlations and Reynolds averaged Navier-Stokes equations
R.V. Kovalev, V.V. Kudryavtsev and D.A. Churakov
Experimental investigation of effect of ultrasonically absorptive coating locations on second mode disturbances in hypersonic boundary layer
S. Lukashevich, S. Morozov and A. Shiplyuk
On the origin high level pulsations in vicinity of lateral edge of blunted triangular plate in supersonic flow
A.D. Kosinov, N.V. Semionov, Y.G. Yermolaev and A.V. Vaganov
Experimental study of receptivity of supersonic boundary layer on swept wing
N.V. Semionov, A.D. Kosinov and Yu.G. Yermolaev
Effect of the local wall cooling/heating on the hypersonic boundary layer stability and transition
A. Sidorenko, P. Polivanov, Y. Gromyko, D. Bountin and A. Maslov
Influence of external disturbances on nonlinear processes of three-dimensional supersonic boundary layer
N.V. Semionov, A.D. Kosinov and Y.G. Yermolaev
Research of formation and development of stationary vortices and its secondary instability after the roughness element on the leading edge of the oblique wing
S.N. Tolkachev, V.N. Gorev and V.V. Kozlov
Laminar-turbulent transition structure on classical and wavy wing at low Reynolds number.
I.D. Zverkov, V.V. Kozlov, A.V. Kryukov, A.V. Boiko and S. Hein
|
