22 results on '"Mazhul', I. I."'
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2. Numerical simulation of gas dynamics of the inflow into a channel located behind a conical or plane shock wave
3. Asymmetry of a Flow Which is Due to the Interaction of a Compression Shock with the Boundary Layer on a Longitudinally Ribbed Surface
4. Numerical simulation of starting conditions for a supersonic air intake with a rectangular duct and partial release of the captured air stream through longitudinal slots
5. Numerical simulation of gas dynamics of the inflow into a channel located behind a conical or plane shock wave
6. Numerical simulation of a three-dimensional flow in a channel with interaction of a plane shock wave and a longitudinally ribbed surface
7. Supersonic flow in the rectangular duct of an air inlet with the separation-induced interaction of the boundary layer with shock waves
8. Flow turbulization in a pseudo-shock forming in an axisymmetric duct with a frontal inlet
9. Numerical Investigation of the Influence of the Configuration Parameters of a Supersonic Passenger Aircraft on the Intensity of Sonic Boom
10. Asymmetry of a Flow Which is Due to the Interaction of a Compression Shock with the Boundary Layer on a Longitudinally Ribbed Surface.
11. On the question of starting conditions for frontal axisymmetric inlets tested in hot-shot wind tunnels
12. Numerical simulation of the side pylon effect on the aerodynamic characteristics of models at their wind tunnel tests
13. Numerical simulation of the influence of the control surfaces deflection on the aerodynamics of a slender axisymmetric configuration
14. Numerical modeling of the conditions for realization of flow regimes in supersonic axisymmetric conical inlets of internal compression
15. Supersonic flow over paired compression wedges of different sweep installed on the pre-compression surface
16. SUPERSONIC INTAKE WITH LONGITUDINAL AIR BLEED SLOTS FACILITATING ITS STARTING
17. Numerical modeling of three-dimensional separated flow at the initial section of a rectangular air inlet
18. Numerical modeling of three-dimensional separated flow at the initial section of a rectangular air inlet.
19. Numerical simulation of the flow with a pseudo-shock in an axisymmetric expanding duct with a frontal inlet
20. Gasdynamic and turbulent features of flows with a pseudo-shock wave in axisymmetric ducts
21. Gasdynamic and Turbulent Features of Flows with a Pseudo-Shock Wave in Axisymmetric Ducts.
22. An investigation of starting processes and flow patterns occurring in hypersonic axisymmetric inlets of internal compression
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