Numerically Analyzing More Efficiently High-Lift Aerodynamics of Transport Aircraft with Omni-tree Cartesian Grids
A modified Cartesian grid method isintroduced to simulate the flow fields around wing/body high-lift configurations by using a multi-zone technique. With a face-to-face algorithm, the Euler equations are solved numerically, in combination with the cellcenter finite volume method and dual-time stepping scheme. The multi-zone technique is employed to simplify the great difficulties in grid generation. The face-to-face algorithm is constructed to precisely establish the information exchange of flow fields on the interface between zones. The numerical results are presented and compared with experimental data.
modified cartesian grid Euler equations 3D high-lift systems multi-zone and face-to-face technique
Sang Weimin Liu Qiong Lei Xiwei
Northwestern Polytechnical University, Xian, Shaanxi, 710072, China The First Aircraft Institute of AVICI, Xian, Shaanxi, 710089, China
国际会议
2010 Asia-Pacific International Symposium on Aerospace Technology(2010 亚太航空航天技术研讨会 APISAT 2010)
西安
英文
399-402
2010-09-01(万方平台首次上网日期,不代表论文的发表时间)