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N-S EQUATION CALCULATIONS ON MULTI-ELEMENT AIRFOILS WITH ZONAL PATCHED GRIDS

机译:带网格的多元素翼型的N-S方程计算

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摘要

For a complex flow about multi-element airfoils a mixed grid method is set up. C-type grids are produced on each element's body and in their wakes at first, O-type grids are given in the Outmost area, and H-type grids are used in middle additional areas. An algebra method is used to produce the initial grids in each area. And the girds are optimized by elliptical differential equation method. Then C-O-H zonal patched grids around multi-element airfoils are produced automatically and efficiently. A time accurate finite-volume integration method is used to solve the compressible laminar and turbulent Navier-Stokes (N-S) equations on the grids. Computational results prove the method to be effective.
机译:对于多元素机翼的复杂流动,建立了混合网格方法。 C型栅格在每个元素的主体上生成,首先在它们的尾部产生,O型栅格在最外侧区域给出,H型栅格在其他中间区域使用。代数方法用于在每个区域中生成初始网格。并通过椭圆微分方程法对网格进行了优化。然后自动高效地生成围绕多元素机翼的C-O-H纬向修补网格。使用时间精确的有限体积积分方法来求解网格上的可压缩层流和湍流Navier-Stokes(N-S)方程。计算结果证明了该方法的有效性。

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