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- W2355109804 abstract "We introduce the control point concept defining body surface's geometry features, then distributing grid points between adjacent control points. A surface mesh method for complex shaped fuselage is proposed in an interactive interface. Using the above method, a complete surface grid with little distortion can be gained rapidly. Based on the transfinite interpolation theory, an improved algebraic grid generation method is presented in this paper. Our improvements of existing algebraic grid generation method include: (1) orthogonality control, which greatly improves grid orthogonality adapted to viscous flow calculation; (2) weighted average smoothing, which efficiently handles with grid intersection due to concave corner existence; (3) normal vector control, which adjusts grid smoothing near convex corner. For the grid generation of complex shaped aircraft, The usage of the above measures result in the satisfactory mesh which has appropriate normal mesh spacing、body fitted quality and peripheral grid fairness. Being algebraic grid generation technique, The improved method is quite practical and effective." @default.
- W2355109804 created "2016-06-24" @default.
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- W2355109804 date "2001-01-01" @default.
- W2355109804 modified "2023-09-23" @default.
- W2355109804 title "A practical surface and space grid generation method for complex-shaped aircraft configurations" @default.
- W2355109804 hasPublicationYear "2001" @default.
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