Timchenko Sergei Viktorovich

Publications in Math-Net.Ru

1. State of fullerene C$_{60}$ in a two-component gas mixture
   
   Vestn. Tomsk. Gos. Univ. Mat. Mekh., 2024, no. 87,  59–72
2. Numerical study of the aerodynamic characteristics of a “wing–fuselage–engine nacelle–pylon” three-dimensional layout of the engine for a wide-body long-range aircraft
   
   Vestn. Tomsk. Gos. Univ. Mat. Mekh., 2019, no. 62,  135–141
3. The stability of the optimal aerodynamic design of an isolated three-dimensional wing to its initial form
   
   Zhurnal Tekhnicheskoi Fiziki, 88:12 (2018),  1793–1800
4. Investigation of the stability of an unmanned aerial vehicle wing optimizing in terms of its initial shape
   
   Vestn. Tomsk. Gos. Univ. Mat. Mekh., 2018, no. 56,  120–127
5. Aerodynamic design for an isolated three-dimensional wing of an unmanned aerial vehicle
   
   Vestn. Tomsk. Gos. Univ. Mat. Mekh., 2018, no. 54,  118–130
6. An optimal aerodynamic design for the wing of a wide-body long-range aircraft
   
   Vestn. Tomsk. Gos. Univ. Mat. Mekh., 2018, no. 51,  117–129
7. An optimal design technology for aerodynamic configurations based on the numerical solutions of the full Navier–Stokes equations
   
   Vestn. Tomsk. Gos. Univ. Mat. Mekh., 2017, no. 50,  90–98
8. Effective implementation of nonlinear constraints in optimization of three-dimensional transonic wings
   
   Vestn. Tomsk. Gos. Univ. Mat. Mekh., 2015, no. 1(33),  72–81
9. Optimization of the Earth reentry trajectory of a blunted body by the integral heat flux
   
   Prikl. Mekh. Tekh. Fiz., 41:4 (2000),  112–123
10. Calculations for 3D boundary layer by high accuracy finite-difference method
    
    Mat. Model., 10:10 (1998),  79–86
11. Application of genetic algorithms for heat flux optimization problem
    
    Mat. Model., 10:9 (1998),  111–122
12. High accuracy finite-difference method for boundary layer equations
    
    Mat. Model., 10:4 (1998),  70–82
13. Solution of the equations of a nonequilibrium viscous shock layer for blunt bodies with catalytic surfaces
    
    Zh. Vychisl. Mat. Mat. Fiz., 38:5 (1998),  860–869
14. Calculation of three-dimensional turbulent boundary-layer flows on a network of different-power computers
    
    Zh. Vychisl. Mat. Mat. Fiz., 38:3 (1998),  510–519
15. Simulation of flow in threedimensional viscous shock layer on distributed memory multiprocessor system
    
    Mat. Model., 5:7 (1993),  41–48
16. Three-dimensional, nonuniform, hypersonic viscous gas flow around blunt bodies
    
    TVT, 30:1 (1992),  116–121
17. Spatial thin viscous shock layer in non-homogeneous gas flow in the absence of symmetry planes
    
    Mat. Model., 1:11 (1989),  51–57
18. Supersonic nonuniform gas flow around elongated axisymmetric bodies
    
    Prikl. Mekh. Tekh. Fiz., 30:5 (1989),  60–65