32 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 a three-dimensional flow in a channel with interaction of a plane shock wave and a longitudinally ribbed surface
6. Supersonic flow in the rectangular duct of an air inlet with the separation-induced interaction of the boundary layer with shock waves
7. Flow turbulization in a pseudo-shock forming in an axisymmetric duct with a frontal inlet
8. Numerical Investigation of the Influence of the Configuration Parameters of a Supersonic Passenger Aircraft on the Intensity of Sonic Boom
9. On the question of starting conditions for frontal axisymmetric inlets tested in hot-shot wind tunnels
10. Numerical simulation of the side pylon effect on the aerodynamic characteristics of models at their wind tunnel tests
11. Numerical simulation of the influence of the control surfaces deflection on the aerodynamics of a slender axisymmetric configuration
12. Numerical modeling of the conditions for realization of flow regimes in supersonic axisymmetric conical inlets of internal compression
13. Supersonic flow over paired compression wedges of different sweep installed on the pre-compression surface
14. Numerical investigation of supersonic flow breakdown at the inlet duct throttling
15. Numerical investigation of flow past a system of two sweptback compression wedges
16. Flow field study in the T-313 wind-tunnel test section for M = 7
17. Numerical investigation of flow over two sweepback wedges at M = 4 and 6
18. Supersonic flow past a system of two swept wedges mounted on a preliminary compression surface
19. Experimental characteristics of a supersonic three-dimensional air inlet with adjustable throat
20. Gasdynamic design of a two-dimensional supersonic inlet with the increased flow rate factor
21. Design of supersonic three-dimensional inlets using two-dimensional isentropic compression flow
22. Off-design regimes of flow past waveriders based on isentropic compression flows
23. Analysis of possible improvement of acceleration of a high-velocity air-breathing flying vehicle
24. Numerical investigation of off-design regimes of flow past waveriders on the basis of axisymmetric conical flows
25. Comparative analysis of aerodynamics of waveriders designed on the basis of conical and planar flows
26. Carrying bodies with an adverse longitudinal pressure gradient
27. Aerodynamics of re-entry vehicles at real values of Reynolds numbers
28. Characteristics of the AT-303 hypersonic wind tunnel. Part 2. Aerodynamics of the HB-2 reference model
29. Numerical Investigation of Off-Design Regimes of Flow Past Power-Law Waveriders Based on the Flows Behind Plane Shocks
30. Distinctive Features of the Lateral Flow for a Convergent Air-Intake with a Convergent Nose Compression Surface
31. Numerical Investigation of Supersonic Flows Around Hyperelliptic Cones
32. Gasdynamics of a Convergent Air-Intake with a Nose Compression Surface
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