Lattice Boltzmann Method used for the aircraft characteristics   computation at high angle of attack

doi:10.1007/s11431-010-3222-2

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	Lattice Boltzmann Method used for the aircraft characteristics computation at high angle of attack
	Du TeZhuan ; Li XiangQun ; Zhang XiaLing ; Wang YiWei
刊名	science china technological sciences
	2010
关键词	LBM CFD high AOA NAVIER-STOKES EQUATION
DOI	10.1007/s11431-010-3222-2
英文摘要	Traditional Finite Volume Method (FVM) and Lattice Boltzmann Method (LBM) are both used to compute the high angle attack aerodynamic characteristics of the benchmark aircraft model named CT-1. Even though the software requires flow on the order of Ma < 0.4, simulation at Ma=0.5 is run in PowerFLOW after theoretical analysis. The consistency with the wind tunnel testing is satisfied, especially for the LBM which can produce perfect results at high angle attack. PowerFLOW can accurately capture the detail of flows because it is inherently time-dependent and parallel and suits large-scale computation very well.; Engineering, Multidisciplinary; Materials Science, Multidisciplinary; SCI(E); EI; 0; ARTICLE; 8; 2068-2073; 53
语种	英语
内容类型	期刊论文
源URL	[http://ir.pku.edu.cn/handle/20.500.11897/154821]
专题	工学院
推荐引用方式 GB/T 7714	Du TeZhuan,Li XiangQun,Zhang XiaLing,et al. Lattice Boltzmann Method used for the aircraft characteristics computation at high angle of attack[J]. science china technological sciences,2010.
APA	Du TeZhuan,Li XiangQun,Zhang XiaLing,&Wang YiWei.(2010).Lattice Boltzmann Method used for the aircraft characteristics computation at high angle of attack.science china technological sciences.
MLA	Du TeZhuan,et al."Lattice Boltzmann Method used for the aircraft characteristics computation at high angle of attack".science china technological sciences (2010).