High-order schemes for predicting computational aeroacoustic propagation with adaptive mesh refinement

被引:11
|
作者
Peers, Edward [1 ]
Huang, Xun [1 ]
机构
[1] Peking Univ, Coll Engn, Dept Aeronaut & Astronaut, State Key Lab Turbulence & Complex Syst, Beijing 100871, Peoples R China
基金
中国国家自然科学基金;
关键词
Adaptive mesh; Aeroacoustics; High-order schemes; COMPACT SCHEMES; RADIATION; DUCT; ACOUSTICS; NOISE; SOUND; FLOW;
D O I
10.1007/s10409-013-0004-7
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
High-order schemes based on block-structured adaptive mesh refinement method are prepared to solve computational aeroacoustic (CAA) problems with an aim at improving computational efficiency. A number of numerical issues associated with high-order schemes on an adaptively refined mesh, such as stability and accuracy are addressed. Several CAA benchmark problems are used to demonstrate the feasibility and efficiency of the approach.
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页码:1 / 11
页数:11
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