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- W2028821384 abstract "An improved method is presented for coupling a boundary layer code with an unsteady inviscid transonic computer code in a quasi-steady fashion. At each fixed time step, the boundary layer and inviscid equations are successively solved until the process converges. An explicit coupling of the equations is described which greatly accelerates the convergence process. Computer times for converged viscous-inviscid solutions are about 1.8 times the comparable inviscid values. Comparison of the results obtained with experimental data on three airfoils are presented. These comparisons demonstrate that the explicitly coupled viscous-inviscid solutions can provide efficient predictions of pressure distributions and lift for unsteady two-dimensional transonic flows." @default.
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- W2028821384 date "1987-11-01" @default.
- W2028821384 modified "2023-09-26" @default.
- W2028821384 title "Efficient self-consistent viscous-inviscid solutions for unsteady transonic flow" @default.
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- W2028821384 doi "https://doi.org/10.2514/3.45515" @default.
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