Vetlutskii Vitalii Nikolaevich

Publications in Math-Net.Ru

1. Air flow in the human nasal cavity
   
   Prikl. Mekh. Tekh. Fiz., 51:2 (2010),  107–115
2. Flow in a viscous jet escaping through a supersonic nozzle into a semi-infinite ambient space
   
   Prikl. Mekh. Tekh. Fiz., 50:6 (2009),  6–15
3. Investigation of a gas flow with solid particles in a supersonic nozzle
   
   Prikl. Mekh. Tekh. Fiz., 46:6 (2005),  65–77
4. Numerical investigation of three-dimensional super- and hypersonic boundary layers at large Reynolds numbers
   
   Sib. Zh. Ind. Mat., 7:1 (2004),  9–20
5. Investigation of a turbulent boundary layer on a hypersonic aircraft model
   
   Prikl. Mekh. Tekh. Fiz., 40:1 (1999),  115–125
6. Investigation of aerodynamic heating of a plate in a viscous hypersonic flow
   
   TVT, 37:3 (1999),  415–419
7. The effect of the angle of attack on hypersonic flow on a plate
   
   TVT, 36:5 (1998),  754–760
8. A numerical study of a viscous shock layer on a plate
   
   Prikl. Mekh. Tekh. Fiz., 38:2 (1997),  91–100
9. Calculation of flow in a chemical reactor for chloroorganic waste utilization
   
   Fizika Goreniya i Vzryva, 31:4 (1995),  44–53
10. Hypersonic flow on a flat plate. Experimental results and numerical modeling
    
    Prikl. Mekh. Tekh. Fiz., 36:6 (1995),  60–67
11. Computational analysis of a spatial compressed turbulent boundary layer on the upwind side of delta wings under supersonic flow
    
    Prikl. Mekh. Tekh. Fiz., 35:1 (1994),  68–74
12. Numerical calculation of a three-dimensional laminar compressible boundary layer on profiled triangular wings with supersonic front edges
    
    Prikl. Mekh. Tekh. Fiz., 34:5 (1993),  88–94
13. Computing the compressible laminar boundary layer on a sharp body of bielliptic section
    
    Prikl. Mekh. Tekh. Fiz., 32:1 (1991),  55–61
14. Calculation of a laminar boundary layer on the leeward side of a triangular plate with supersonic leading edges
    
    Prikl. Mekh. Tekh. Fiz., 30:1 (1989),  75–81
15. Compressible laminar boundary layer on a delta wing with attached shock wave
    
    Prikl. Mekh. Tekh. Fiz., 26:5 (1985),  23–29
16. Investigation of the supersonic flow around a pointed elliptical cone at an angle of attack
    
    Prikl. Mekh. Tekh. Fiz., 16:1 (1975),  114–120