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Publications in Math-Net.Ru
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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
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Optimizing hypersonic wings
Zh. Vychisl. Mat. Mat. Fiz., 34:3 (1994), 446–460
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Optimum wing shapes in a hypersonic nonequilibrium flow
Prikl. Mekh. Tekh. Fiz., 34:2 (1993), 66–72
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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
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Calculation of the flow past a delta wing in the thin shock layer approximation
Zh. Vychisl. Mat. Mat. Fiz., 29:10 (1989), 1530–1537
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Nonstationary flow around delta wings by a stream behind shocks
Prikl. Mekh. Tekh. Fiz., 29:5 (1988), 40–46
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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
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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
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