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The Effect of Admixture of Non-Evaporating Droplets on the Flow Structure and Adiabatic Wall Temperature in a Compressible Two-Phase Boundary Layer
Golubkina I.V., Osiptsov A.N.
Problem of Optimal Control of the Turbulent Boundary Layer on a Permeable Surface in Supersonic Gas Flow
Garaev K.G., Mukhametzyanov I.R.
Turbulent thermal boundary layer on a plate. Reynolds analogy and heat transfer law over the entire range of prandtl numbers
Vigdorovich I.I.
Global Stability Analysis of Spatially Developing Boundary Layer: Effect of Streamwise Pressure Gradients
Bhoraniya R., Narayanan V.
Experimental Investigation of the Weak Shock Wave Influence on the Boundary Layer of a Flat Blunt Plate at the Mach Number 2.5
Ermolaev Y.G., Kosinov A.D., Kocharin V.L., Semenov N.V., Yatskikh A.A.
Disturbance Propagation in Boundary Layers under the Conditions of Weak Hypersonic Interaction
Lipatov I.I., Ngo Q.N.
The effect of fine evaporating droplets on the adiabatic-wall temperature in a compressible two-phase boundary layer
Azanov G.M., Osiptsov A.N.
Numerical Simulation of the Interaction of Unsteady Surface Blowing (Suction) with Turbulent Near-Wall Flow
Aleksin V.A.
Inviscid vortex structures in the shock layers of conical flows around V wings
Zubin M.A., Maksimov F.A., Ostapenko N.A.
Temperature Factor Effect on the Disturbance Propagation in Hypersonic Flow past a Yawed Flat Plate
Dudin G.N., Neiland V.Y.
Status of the Navier–Stokes Equations in Gas Dynamics. A Review
Galkin V.S., Rusakov S.V.
Effect of a dielectric barrier discharge on laminar-turbulent transition on a flat plate in a disturbed external flow
Vatazhin A.B., Kholshchevnikova E.K.
Numerical Modeling of the Interaction between a Supersonic Boundary Layer and an Acoustic Wave
Gaponov S.A., Semenov A.N.
Generation of Three-Dimensional Disturbances in a Boundary Layer on Strong Interaction with a Hypersonic Flow
Dudin G.N., Neiland V.Y.
Application of the method of near-wall boundary conditions to an investigation of turbulent flows with longitudinal pressure gradients
Aleksin V.A.
Distinctive Features of Flow in the Hypersonic Boundary Layer in the Vicinity of the Plane of Symmetry of a Planar Wing Having a Bend of the Leading Edge
Dudin G.N., Ledovskii A.V.
Modelling of the Interaction of Unsteady High-Intensity Turbulence Flow with Heat- and Mass-Transfer in the Boundary Layer on the Surface
Aleksin V.A.
Asymptotic Analysis of Viscous Fluctuations in Turbulent Boundary Layers
Gorbushin A.R., Zametaev V.B.
Excitation of controllable perturbations in the three-dimensional boundary layer using plasma actuators
Kiselev A.F., Kuryachii A.P., Chernyshev S.L.
Joint effect of heat and mass transfer on the compressible boundary layer stability
Gaponov S.A., Terekhova N.M.
Mach Wave Effect on Laminar-Turbulent Transition in Supersonic Flow over a Flat Plate
Din Q.H., Egorov I.V., Fedorov A.V.
Flutter of infinite elastic plates in the boundary-layer flow at finite Reynolds numbers
Bondarev V.O., Vedeneev V.V.
Local modeling of the aerodynamic heating of the blunt body surface in subsonic high-enthalpy air flow. Theory and experiment on a high-frequency plasmatron
Vasil’evskii S.A., Gordeev A.N., Kolesnikov A.F.
Propagation of a Shock Wave through a Viscous Heat-Conducting Gas in a Long Microchannel
Azarova O.A., Shakhov E.M.
Investigation of the effect of heavy gas injection into a supersonic boundary layer on laminar-turbulent transition
Gaponov S.A., Ermolaev Y.G., Zubkov N.N., Kosinov A.D., Lysenko V.I., Smorodskii B.V., Yatskikh A.A.
1 - 25 of 25 Items

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