Bashkin Vyacheslav Antonovich

Publications in Math-Net.Ru

1. Circular cyllinder in a transonic flow at high Reynolds numbers: Thermal problem
   
   TVT, 54:4 (2016),  576–583
2. The interaction of shock waves with a boundary layer on a sharp plate and a blunted plate
   
   TVT, 54:3 (2016),  379–392
3. 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
4. Aerodynamic Heating of a Thin Sharp-Nose Circular Cone in Supersonic Flow
   
   TVT, 43:5 (2005),  732–744
5. 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
6. Three-dimensional laminar streamlining of axially symmetric bodies by supersonic gas flow
   
   Zh. Vychisl. Mat. Mat. Fiz., 42:12 (2002),  1864–1874
7. 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
8. Supersonic flow of viscous gas in a flat channel at high values of the Reynolds number
   
   TVT, 39:1 (2001),  115–122
9. 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
10. Application of the Newton method to the calculation of internal supersonic separated flows
    
    Prikl. Mekh. Tekh. Fiz., 38:1 (1997),  30–42
11. Numerical solution of the Navier-Stokes equations using variational iteration methods
    
    Zh. Vychisl. Mat. Mat. Fiz., 34:11 (1994),  1693–1703
12. Calculation of self-similar three-dimensional laminar boundary layer equations by a quasilinear method
    
    Zh. Vychisl. Mat. Mat. Fiz., 11:5 (1971),  1338–1344
13. Numerical integration of the equations of the three-dimensional laminar boundary layer on lines of divergence
    
    Zh. Vychisl. Mat. Mat. Fiz., 10:6 (1970),  1491–1502
14. Calculation of laminar boundary layer on sharp elliptic cones in supersonic flow at the angle of attack equal to zero
    
    Zh. Vychisl. Mat. Mat. Fiz., 10:1 (1970),  255–259
15. Calculation of the equations of a laminar boundary space layer by the method of integral relations
    
    Zh. Vychisl. Mat. Mat. Fiz., 8:6 (1968),  1280–1290
16. A spatial laminar boundary layer on a streamline in conical external flow of a uniform gas in the absence of sources and sinks
    
    Prikl. Mekh. Tekh. Fiz., 8:2 (1967),  97–103