VIRTUAL GRID AND NAVIER-STOKES COMPUTATION FOR CONTROL-SURFACE
摘要
The virtual grid method used in the embedding technique to solve the problem of finding interpolatingcells of the inner and outer boundary points near joint regions was developed for calculating the viscous flowsaround a wing with control-surface.The main purpose of the virtual grid is to effectively treat the geometry of thecrossed facial pIanes at the interface,and to convert a solid wall boundary condition into an interface condition,however,no fluid flow computations are conducted within the virtual grid.Navier-Stokes computations were per-formed for transonic flow over a clipped delta wing with control surface,and the computed results compare wellwith the experimental data.
引用本文（GB/T 7714）
Li .., Xiaowei Xiaowei, Fan Fan, 等. VIRTUAL GRID AND NAVIER-STOKES COMPUTATION FOR CONTROL-SURFACE[J]. 上海交通大学学报：英文版, 2002.
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