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吸气/喷气叶栅的三维贴体网格生成技术
引用本文:孙玺淼,颜培刚,张永军,王松涛. 吸气/喷气叶栅的三维贴体网格生成技术[J]. 航空发动机, 2008, 34(1): 38-40
作者姓名:孙玺淼  颜培刚  张永军  王松涛
作者单位:哈尔滨工业大学,能源科学与工程学院,哈尔滨,150001
摘    要:对某吸气/喷气叶栅的复杂的多联通域边界,采用孔斯双参数样条曲面模型,通过一维问题边界条件控制疏密度,选择合理的参数来强调正交性;分别在双参数域和绝对坐标系下求解微分方程,得到二维、三维网格。应用上述方法,为某叶栅叶片前缘和端壁开多排孔方案生成了三维贴体网格,获得了理想的效果。

关 键 词:自由型曲面  结构化网格  吸气喷气  叶栅
修稿时间:2007-02-11

3D Body-Fitted Grid Generation Technology of Cooling/Bleed Blade Cascades
SUN Xi-miao,YAN Pei-gang,ZHANG Yong-jun,WANG Song-tao. 3D Body-Fitted Grid Generation Technology of Cooling/Bleed Blade Cascades[J]. Aeroengine, 2008, 34(1): 38-40
Authors:SUN Xi-miao  YAN Pei-gang  ZHANG Yong-jun  WANG Song-tao
Abstract:The grid orthogonality was emphasized using the model of Coons two-parameter spline surface,controlling the grid density with 1D problem boundary condition and selecting reasonable parameters for the complicated multiply connected domain boundaries of cooling/bleed cascades.The 2D and 3D grids were obtained by solutions of differentiating equation in the two-porameter region and absolute coordinate system respectively.It was reasonable that 3D body-fitted grids were generated by using this method for the project of opening multi-row holes on the leading edge and endwall.The quality of the computation grid was reasonable.
Keywords:free curved surface  structured grid  cooling  bleed  blade cascades
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