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Publications in Math-Net.Ru |
Citations |
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2019 |
1. |
V. N. Golubkin, G. B. Sizykh, “Generalization of the Crocco invariant for 3D gas flows behind detached bow shock wave”, Izv. Vyssh. Uchebn. Zaved. Mat., 2019, no. 12, 52–56 ; Russian Math. (Iz. VUZ), 63:12 (2019), 45–48 |
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2018 |
2. |
V. N. Golubkin, I. S. Manuilovich, V. V. Markov, “Пятый инвариант линий тока для осесимметричных закрученных течений газа”, Proceedings of MIPT, 10:2 (2018), 131–135 |
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2015 |
3. |
V. N. Golubkin, V. V. Markov, G. B. Sizykh, “The integral invariant of the equations of viscous gas flow”, Prikl. Mat. Mekh., 79:6 (2015), 808–816 ; J. Appl. Math. Mech., 79:6 (2015), 566–571 |
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1998 |
4. |
V. N. Golubkin, D. S. Emelin, “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 ; Comput. Math. Math. Phys., 38:9 (1998), 1527–1535 |
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1997 |
5. |
V. N. Golubkin, D. S. Emelin, “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 ; Comput. Math. Math. Phys., 37:10 (1997), 1197–1205 |
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1995 |
6. |
V. N. Golubkin, A. V. Baranov, “Hypersonic flow around V-shaped wings with a detached shock wave”, Zh. Vychisl. Mat. Mat. Fiz., 35:11 (1995), 1705–1714 ; Comput. Math. Math. Phys., 35:11 (1995), 1373–1380 |
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1994 |
7. |
V. N. Golubkin, V. V. Negoda, “Optimizing hypersonic wings”, Zh. Vychisl. Mat. Mat. Fiz., 34:3 (1994), 446–460 ; Comput. Math. Math. Phys., 34:3 (1994), 377–388 |
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1993 |
8. |
V. N. Golubkin, V. V. Negoda, “Optimum wing shapes in a hypersonic nonequilibrium flow”, Prikl. Mekh. Tekh. Fiz., 34:2 (1993), 66–72 ; J. Appl. Mech. Tech. Phys., 34:2 (1993), 212–218 |
9. |
V. N. Golubkin, “The hypersonic flow of gas with heat input about airfoil”, TVT, 31:2 (1993), 252–256 ; High Temperature, 31:2 (1993), 215–219 |
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1991 |
10. |
V. N. Golubkin, V. V. Negoda, “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 ; U.S.S.R. Comput. Math. Math. Phys., 31:12 (1991), 70–79 |
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1989 |
11. |
V. N. Golubkin, V. V. Negoda, “Calculation of the flow past a delta wing in the thin shock layer approximation”, Zh. Vychisl. Mat. Mat. Fiz., 29:10 (1989), 1530–1537 ; U.S.S.R. Comput. Math. Math. Phys., 29:5 (1989), 195–200 |
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1988 |
12. |
V. N. Golubkin, V. V. Negoda, “Nonstationary flow around delta wings by a stream behind shocks”, Prikl. Mekh. Tekh. Fiz., 29:5 (1988), 40–46 ; J. Appl. Mech. Tech. Phys., 29:5 (1988), 637–642 |
13. |
V. N. Golubkin, V. V. Negoda, “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 ; U.S.S.R. Comput. Math. Math. Phys., 28:5 (1988), 202–208 |
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1987 |
14. |
V. N. Golubkin, “Three-dimensional flow of a hypersonic dusty gas over a wing”, Prikl. Mekh. Tekh. Fiz., 28:1 (1987), 15–20 ; J. Appl. Mech. Tech. Phys., 28:1 (1987), 13–18 |
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1985 |
15. |
V. N. Golubkin, V. V. Negoda, “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 ; U.S.S.R. Comput. Math. Math. Phys., 25:2 (1985), 176–182 |
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1984 |
16. |
V. N. Golubkin, “Supersonic flow over a wing at high attack angles”, Prikl. Mekh. Tekh. Fiz., 25:4 (1984), 65–70 ; J. Appl. Mech. Tech. Phys., 25:4 (1984), 556–562 |
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1983 |
17. |
A. I. Golubinskii, V. N. Golubkin, “Hypersonic three-dimensional radiating gas flow around a wing”, Prikl. Mekh. Tekh. Fiz., 24:6 (1983), 71–78 ; J. Appl. Mech. Tech. Phys., 24:6 (1983), 828–835 |
18. |
M. A. Galakhov, V. N. Golubkin, “Elastothermo-hydrodynamic problems in the theory of lubrication”, Prikl. Mekh. Tekh. Fiz., 24:3 (1983), 52–60 ; J. Appl. Mech. Tech. Phys., 24:3 (1983), 329–337 |
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1981 |
19. |
A. I. Golubinskii, V. N. Golubkin, “Theory of three-dimensional hypersonic flow around a body”, Dokl. Akad. Nauk SSSR, 258:1 (1981), 42–44 |
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1977 |
20. |
A. I. Golubinskii, V. N. Golubkin, “Three dimensional flow of hypersonic gas past a thin airfoil”, Dokl. Akad. Nauk SSSR, 234:5 (1977), 1032–1034 |
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1976 |
21. |
A. I. Golubinskii, V. N. Golubkin, “Delta wing in a hypersonic gas flow”, Dokl. Akad. Nauk SSSR, 226:4 (1976), 789–790 |
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Organisations |
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