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Asymptotic boundary conditions for computing the position of laminar-turbulent transition by the eN-method
Boiko A.V., Demyanko K.V., Nechepurenko Y.M.
Asymmetric self-similar flows of a viscous incompressible fluid along a right-angle corner
Boiko A.V., Nechepurenko Y.M.
Numerical simulation of the evolution of unstable disturbances of various modes and initial stages of the laminar-turbulent transition in the boundary layer at the freestream Mach number М = 6
Khotyanovsky D.V., Kudryavtsev A.N.
Heat and mass transfer at adiabatic evaporation of binary zeotropic solutions
Makarov M.S., Makarova S.N.
Stability of space-periodic flow with separation of a laminar boundary layer
Boiko A.V., Dovgal A.V., Sorokin A.M.
Modification of turbulent airfoil section flow using a combined control action
Kornilov V.I., Kavun I.N., Popkov A.N.
Stability of supersonic boundary layer under the influence of heavy gas injection: experimental study
Ermolaev Y.G., Kosinov A.D., Lysenko V.I., Smorodsky B.V.
Turbulent circulation above the surface heat source in a stably stratified environment
Kurbatskii A.F., Kurbatskaya L.I.
Turbulization of a wake behind the double roughness elements in a hypersonic boundary layer
Polivanov P.A., Gromyko Y.V., Maslov A.A.
Investigation of the impulse action of a membrane on the straight wing boundary layer
Katasonov M.M., Pavlenko A.M., Kozlov V.V.
Control of turbulent boundary layer on a wing section by combined blowing/suction
Kornilov V.
Effect of the surface roughness of blunt cone forebody on the position of laminar-turbulent transition
Bountin D.A., Gromyko Y.V., Maslov A.A., Polivanov P.A., Sidorenko A.A.
The impact of weak shock waves on the flow in the boundary layer of a flat plate with a variable sweep angle of the leading edge
Kocharin V.L., Kosinov A.D., Yatskikh A.A., Ermolaev Y.G., Semionov N.V., Piterimova M.V., Shevelkov S.G., Minin O.P.
Experimental study of the influence of small angles of attack and cone nose bluntness on the stabilization of hypersonic boundary layer with passive porous coating
Morozov S.O., Lukashevich S.V., Soudakov V.G., Shiplyuk A.N.
Unsteady boundary layer flow of a nanofluid over a stretching sheet with variable fluid properties in the presence of thermal radiation
Daba M., Devaraj P.
Influence of flow conditions over the forebody of a hypersonic air inlet on the flow of air in a boundary-layer bleed channel
Goldfeld M.A., Korotaeva T.A., Obodovskaya E.A., Turchinovich A.O.
Effectiveness of blowing for improving the high-speed trains aerodynamics
Shkvar E.O., Jamea A., E S., Cai J., Kryzhanovskyi A.S.
The use of wavelet transform for the correlation analysis of boundary-layer pulsations
Polivanov P.A., Gromyko Y.V., Bountin D.A., Maslov A.A., Sidorenko A.A.
Effect of unit Reynolds number on the laminar-turbulent transition on a swept wing in supersonic flow
Ermolaev Y.G., Kosinov A.D., Semenov A.N., Semionov N.V., Yatskikh A.A.
An explicit algebraic model of the planetary boundary layer turbulence: test computation of the neutrally stratified atmospheric boundary layer
Kurbatskii A.F., Kurbatskaya L.I.
Laminar-turbulent transition of supersonic boundary layer in the presence of external disturbances
Gaponov S.A.
Numerical investigation of thermal protection of hypersonic flying vehicles
Zinchenko V.I., Gol’din V.D., Zverev V.G.
Numerical simulations of shock-wave interaction with a boundary layer in the plane supersonic flows with jet injection
Beketaeva A.O., Moisseyeva Y.S., Naimanova A.Z.
Investigation of a stable boundary layer using an explicit algebraic model of turbulence
Kurbatskii A.F., Kurbatskaya L.I.
Microwave heating of liquid at the forced flow around a flat plate under the conditions of non-stationary radiation-convection heat transfer
Salomatov V.V., Puzyrev E.M., Salomatov A.V.
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