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Publications in Math-Net.Ru |
Citations |
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1996 |
1. |
V. V. Negoda, K. G. Sayadyan, “The use of transonic slender-body theory to calculate the spatial flow over a wing–fuselage configuration”, Zh. Vychisl. Mat. Mat. Fiz., 36:9 (1996), 134–154 ; Comput. Math. Math. Phys., 36:9 (1996), 1277–1293 |
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1994 |
2. |
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 |
3. |
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 |
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1991 |
4. |
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 |
5. |
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 |
6. |
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 |
7. |
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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1985 |
8. |
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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