南京航空航天大学学报2011，Vol.43Issue(3)：335-340,6.
基于嵌套网格技术和多种空间离散格式的旋翼流场数值模拟
Numerical Simulation of Rotor Flowfield Based on Overset Grids and Several Spatial Discretisation Schemes
赵明 1曹义华1
作者信息
- 1. 北京航空航天大学航空科学与工程学院,北京,100191
- 折叠
摘要
Abstract
A numerical method based on solutions of 3-D Euler/N-S equations is used for calculating the rotor flowfield in hover. Jameson central scheme, Van Leer scheme and AUSM scheme are implemented for spatial discretisation, and Van Albada limiter is also applied. Simultaneously, overset grids are adopted. Hole-Map method is utilized to identify intergrid boundary points (IGBPs). Furthermore, aiming at identification issue of donor elements, Inverse-Map method is implemented. Finally, blade surface pressure distributions derived from numerical simulation are validated compared with the experimental data. Results show that all the schemes mentioned above can accurately simulate the rotor flowfield.关键词
旋翼流场/计算流体力学/嵌套网格/有限体积法Key words
rotor flowfield/ computational fluid dynamics/ overset grids/ finite volume method分类
航空航天引用本文复制引用
赵明,曹义华..基于嵌套网格技术和多种空间离散格式的旋翼流场数值模拟[J].南京航空航天大学学报,2011,43(3):335-340,6.
