Egorov Ivan Vladimirovich

Publications in Math-Net.Ru

1. Численное моделирование взаимодействия волны Маха и пограничного слоя на плоской пластине
   
   TVT, 61:5 (2023),  752–759
2. Numerical simulation of turbulent spots evolution in supersonic boundary layer over a plate
   
   Matem. Mod., 34:7 (2022),  63–72
3. Simulation of the laminar–turbulent transition by applying hybrid difference schemes
   
   Zh. Vychisl. Mat. Mat. Fiz., 62:4 (2022),  677–693
4. Simulation of the laminar–turbulent transition by applying dissipative numerical schemes
   
   Zh. Vychisl. Mat. Mat. Fiz., 61:2 (2021),  268–280
5. Numerical simulation of the flow over a segment-conical body on the basis of Reynolds equations
   
   Zh. Vychisl. Mat. Mat. Fiz., 58:1 (2018),  123–135
6. Effect of small bluntness on the formation of Görtler vortices in a supersonic flow around a compression corner
   
   Prikl. Mekh. Tekh. Fiz., 58:6 (2017),  23–40
7. Direct numerical simulation of the laminar-turbulent transition at hypersonic flow speeds on a supercomputer
   
   Zh. Vychisl. Mat. Mat. Fiz., 57:8 (2017),  1347–1373
8. Circular cyllinder in a transonic flow at high Reynolds numbers: Thermal problem
   
   TVT, 54:4 (2016),  576–583
9. The interaction of shock waves with a boundary layer on a sharp plate and a blunted plate
   
   TVT, 54:3 (2016),  379–392
10. Direct numerical simulation of laminar-turbulent flow over a flat plate at hypersonic flow speeds
    
    Zh. Vychisl. Mat. Mat. Fiz., 56:6 (2016),  1064–1081
11. The effect of spatial perturbations of a supersonic flow on heat flow to the surface of blunt bodies
    
    TVT, 53:5 (2015),  713–726
12. Numerical investigation of the flow field and heat transfer in the circuit of a high-temperature wind-tunnel facility
    
    TVT, 46:5 (2008),  771–783
13. Numerical simulation of stabilization of the boundary layer on a surface with a porous coating in a supersonic separated flow
    
    Prikl. Mekh. Tekh. Fiz., 48:2 (2007),  39–47
14. Aerodynamic Heating of a Thin Sharp-Nose Circular Cone in Supersonic Flow
    
    TVT, 43:5 (2005),  732–744
15. Evolution of the flow field around a circular cylinder and a sphere upon instantaneous start with a supersonic velocity
    
    Prikl. Mekh. Tekh. Fiz., 45:3 (2004),  44–49
16. Three-dimensional laminar streamlining of axially symmetric bodies by supersonic gas flow
    
    Zh. Vychisl. Mat. Mat. Fiz., 42:12 (2002),  1864–1874
17. Effect of the temperature drop between the isothermic walls of a channel on the structure of supersonic flow and on the aerodynamic properties
    
    TVT, 39:4 (2001),  581–588
18. Supersonic flow of viscous gas in a flat channel at high values of the Reynolds number
    
    TVT, 39:1 (2001),  115–122
19. Development of a flow field structure in the vicinity of a circular cylinder in the presence of a laminar-turbulent transition
    
    TVT, 38:5 (2000),  759–768
20. Hypersonic flow in an MHD-acceleration facility and under full-scale conditions
    
    Prikl. Mekh. Tekh. Fiz., 39:2 (1998),  91–102
21. Application of Newton's method in simulation of unsteady separated flows
    
    Zh. Vychisl. Mat. Mat. Fiz., 38:3 (1998),  504–509
22. Simulation of the flow with nonequilibrium chemical reactions in a channel of various crossection
    
    Matem. Mod., 9:11 (1997),  85–100
23. Application of the Newton method to the calculation of internal supersonic separated flows
    
    Prikl. Mekh. Tekh. Fiz., 38:1 (1997),  30–42
24. Simulation of confined separated flows in chemical nonequilibrium
    
    Zh. Vychisl. Mat. Mat. Fiz., 37:6 (1997),  751–758
25. The use of fully implicit monotone schemes to model plane internal flows
    
    Zh. Vychisl. Mat. Mat. Fiz., 36:12 (1996),  91–107
26. Numerical solution of the Navier-Stokes equations using variational iteration methods
    
    Zh. Vychisl. Mat. Mat. Fiz., 34:11 (1994),  1693–1703
27. An approach to the numerical solution of the bidimensional Navier–Stokes equations using the direct calculation method
    
    Zh. Vychisl. Mat. Mat. Fiz., 31:2 (1991),  286–299