25 results on '"Mazhul', I. I."'
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2. 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
3. Numerical simulation of a three-dimensional flow in a channel with interaction of a plane shock wave and a longitudinally ribbed surface
4. Supersonic flow in the rectangular duct of an air inlet with the separation-induced interaction of the boundary layer with shock waves
5. Flow turbulization in a pseudo-shock forming in an axisymmetric duct with a frontal inlet
6. Numerical simulation of the flow with a pseudo-shock in an axisymmetric expanding duct with a frontal inlet
7. On the question of starting conditions for frontal axisymmetric inlets tested in hot-shot wind tunnels
8. Numerical simulation of the side pylon effect on the aerodynamic characteristics of models at their wind tunnel tests
9. Numerical simulation of the influence of the control surfaces deflection on the aerodynamics of a slender axisymmetric configuration
10. Numerical modeling of the conditions for realization of flow regimes in supersonic axisymmetric conical inlets of internal compression
11. Supersonic flow over paired compression wedges of different sweep installed on the pre-compression surface
12. Numerical investigation of supersonic flow breakdown at the inlet duct throttling
13. Numerical investigation of flow past a system of two sweptback compression wedges
14. Flow field study in the T-313 wind-tunnel test section for M = 7
15. Numerical investigation of flow over two sweepback wedges at M = 4 and 6
16. Supersonic flow past a system of two swept wedges mounted on a preliminary compression surface
17. Experimental characteristics of a supersonic three-dimensional air inlet with adjustable throat
18. Gasdynamic design of a two-dimensional supersonic inlet with the increased flow rate factor
19. Design of supersonic three-dimensional inlets using two-dimensional isentropic compression flow
20. Off-design regimes of flow past waveriders based on isentropic compression flows
21. Analysis of possible improvement of acceleration of a high-velocity air-breathing flying vehicle
22. Numerical investigation of off-design regimes of flow past waveriders on the basis of axisymmetric conical flows
23. Comparative analysis of aerodynamics of waveriders designed on the basis of conical and planar flows
24. Aerodynamics of re-entry vehicles at real values of Reynolds numbers
25. Characteristics of the AT-303 hypersonic wind tunnel. Part 2. Aerodynamics of the HB-2 reference model
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