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	Numerical Simulation of Supersonic Twin-Jet Noise with High-Order Finite Difference Scheme
	Gao, Junhui; Xu, Xin; Li, Xiaodong
刊名	22nd AIAA/CEAS Aeroacoustics Conference
	2018
卷号	56页码:290-300
关键词	Aeroacoustics Computational aeroacoustics Eigenvalues and eigenfunctions Finite difference method Geometry Harmonic analysis Navier Stokes equations Nozzles Supersonic aerodynamics Convective velocity Coupling mechanism Dynamic mode decompositions Filtered Navier-Stokes equations Flux reconstruction High order finite difference schemes High-order finite differences Nozzle configuration Fighter aircraft
ISSN号	0001-1452
DOI	10.2514/1.J055751
URL标识	查看原文
收录类别	SCIE
WOS记录号	WOS:000419855200022
内容类型	期刊论文
URI标识	http://www.corc.org.cn/handle/1471x/5935737
专题	北京航空航天大学
推荐引用方式 GB/T 7714	Gao, Junhui,Xu, Xin,Li, Xiaodong. Numerical Simulation of Supersonic Twin-Jet Noise with High-Order Finite Difference Scheme[J]. 22nd AIAA/CEAS Aeroacoustics Conference,2018,56:290-300.
APA	Gao, Junhui,Xu, Xin,&Li, Xiaodong.(2018).Numerical Simulation of Supersonic Twin-Jet Noise with High-Order Finite Difference Scheme.22nd AIAA/CEAS Aeroacoustics Conference,56,290-300.
MLA	Gao, Junhui,et al."Numerical Simulation of Supersonic Twin-Jet Noise with High-Order Finite Difference Scheme".22nd AIAA/CEAS Aeroacoustics Conference 56(2018):290-300.

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