High-Order Discontinuous Galerkin Method for Hovering Rotor Simulations Based on a Rotating Reference Frame

被引:0
|
作者
ZHANG Tao [1 ]
Lü Hongqiang [1 ]
QIN Wanglong [1 ]
CHEN Zhengwu [2 ]
机构
[1] Department of Aerodynamics,Nanjing University of Aeronautics and Astronautics
[2] China Aerodynamics Research and Development Center
基金
中国国家自然科学基金;
关键词
high?order method(HOM); discontinuous Glaerkin method(DGM); Euler equation; hovering rotor simulation; tip vortex;
D O I
10.16356/j.1005-1120.2019.01.005
中图分类号
V211.52 [直升飞机、旋翼机空气动力学];
学科分类号
0801 ; 080103 ; 080104 ;
摘要
An implicit higher ? order discontinuous Galerkin(DG) spatial discretization for the compressible Euler equations in a rotating frame of reference is presented and applied to a rotor in hover using hexahedral grids. Instead of auxiliary methods like grid adaptation,higher ? order simulations(fourth ? and fifth ? order accuracy) are adopted.Rigorous numerical experiments are carefully designed,conducted and analyzed. The results show generally excellent consistence with references and vigorously demonstrate the higher?order DG method’s better performance in loading distribution computations and tip vortex capturing, with much fewer degrees of freedom(DoF). Detailed investigations on the outer boundary conditions for hovering rotors are presented as well. A simple but effective speed smooth procedure is developed specially for the DG method. Further results reveal that the rarely used pressure restriction for outlet speed has a considerable advantage over the extensively adopted vertical speed restriction.
引用
收藏
页码:57 / 70
页数:14
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