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W193535166 abstract "A computational method is presented for threedimensional turbulent boundary layers. The turbulence model is a simple eddy-viscosity formulation. An hybrid difference scheme is used, which has the robustness of first order schemes and accuracy of second order schemes. The boundary layer is computed in the region of determinacy of the initial data. No extra data is required to be given along the lateral boundaries of the computational domain. In this paper the results are presented of the boundary layer flow over the fuselage of an aircraft-like body. The computation follows the strongly 3D flow over the leading edge of the fairing and wing, after which the boundary layer on wing upper and lower surface is computed." @default.
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W193535166 date "1982-12-31" @default.
W193535166 modified "2023-09-26" @default.
W193535166 title "Three-dimensional boundary layer calculations on wings, starting from the fuselage" @default.
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