Golubkin Valeriy Nikolayevich

Publications in Math-Net.Ru

1. Generalization of the Crocco invariant for 3D gas flows behind detached bow shock wave
   
   Izv. Vyssh. Uchebn. Zaved. Mat., 2019, no. 12,  52–56
2. Пятый инвариант линий тока для осесимметричных закрученных течений газа
   
   Proceedings of MIPT, 10:2 (2018),  131–135
3. The integral invariant of the equations of viscous gas flow
   
   Prikl. Mat. Mekh., 79:6 (2015),  808–816
4. Optimization of a short-span wing in a hypersonic gas flow with boundary-layer transition
   
   Zh. Vychisl. Mat. Mat. Fiz., 38:9 (1998),  1592–1601
5. Calculation of the maximum hypersonic fineness ratio and optimal configuration of short-span wings with laminar and turbulent boundary layers
   
   Zh. Vychisl. Mat. Mat. Fiz., 37:10 (1997),  1237–1245
6. Hypersonic flow around V-shaped wings with a detached shock wave
   
   Zh. Vychisl. Mat. Mat. Fiz., 35:11 (1995),  1705–1714
7. Optimizing hypersonic wings
   
   Zh. Vychisl. Mat. Mat. Fiz., 34:3 (1994),  446–460
8. Optimum wing shapes in a hypersonic nonequilibrium flow
   
   Prikl. Mekh. Tekh. Fiz., 34:2 (1993),  66–72
9. The hypersonic flow of gas with heat input about airfoil
   
   TVT, 31:2 (1993),  252–256
10. Optimization of the spatial shape of load-carrying bodies of small elongation at hypersonic velocities
    
    Zh. Vychisl. Mat. Mat. Fiz., 31:12 (1991),  1858–1870
11. Calculation of the flow past a delta wing in the thin shock layer approximation
    
    Zh. Vychisl. Mat. Mat. Fiz., 29:10 (1989),  1530–1537
12. Nonstationary flow around delta wings by a stream behind shocks
    
    Prikl. Mekh. Tekh. Fiz., 29:5 (1988),  40–46
13. Calculation of supersonic flow past the weather side of a wing of small aspect ratio at large angles of attack
    
    Zh. Vychisl. Mat. Mat. Fiz., 28:10 (1988),  1586–1594
14. Three-dimensional flow of a hypersonic dusty gas over a wing
    
    Prikl. Mekh. Tekh. Fiz., 28:1 (1987),  15–20
15. Numerical computation of nonequilibrium flow around a wing in the approximation of a thin shock layer
    
    Zh. Vychisl. Mat. Mat. Fiz., 25:4 (1985),  599–608
16. Supersonic flow over a wing at high attack angles
    
    Prikl. Mekh. Tekh. Fiz., 25:4 (1984),  65–70
17. Hypersonic three-dimensional radiating gas flow around a wing
    
    Prikl. Mekh. Tekh. Fiz., 24:6 (1983),  71–78
18. Elastothermo-hydrodynamic problems in the theory of lubrication
    
    Prikl. Mekh. Tekh. Fiz., 24:3 (1983),  52–60
19. Theory of three-dimensional hypersonic flow around a body
    
    Dokl. Akad. Nauk SSSR, 258:1 (1981),  42–44
20. Three dimensional flow of hypersonic gas past a thin airfoil
    
    Dokl. Akad. Nauk SSSR, 234:5 (1977),  1032–1034
21. Delta wing in a hypersonic gas flow
    
    Dokl. Akad. Nauk SSSR, 226:4 (1976),  789–790