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	Effect of Sideslip on High-Angle-of-Attack Vortex Flow over Close-Coupled Canard Configuration
	Chen, Mingqian; Liu, Peiqing; Guo, Hao; Qu, Qiulin
刊名	JOURNAL OF AIRCRAFT
	2016
卷号	53页码:217-230
关键词	Aerodynamic configurations Aerodynamic stability Aerodynamics Angle of attack Angle of attack indicators Fighter aircraft Aerodynamic response Asymmetric vortices Canard configuration Delayed-detached eddy simulation High angle of attack Lateral stability Non-linear response Nonlinear behavior Vortex flow
ISSN号	0021-8669
DOI	10.2514/1.C033305
URL标识	查看原文
收录类别	SCIE ; EI
WOS记录号	WOS:000372799300017
内容类型	期刊论文
URI标识	http://www.corc.org.cn/handle/1471x/5954306
专题	北京航空航天大学
推荐引用方式 GB/T 7714	Chen, Mingqian,Liu, Peiqing,Guo, Hao,et al. Effect of Sideslip on High-Angle-of-Attack Vortex Flow over Close-Coupled Canard Configuration[J]. JOURNAL OF AIRCRAFT,2016,53:217-230.
APA	Chen, Mingqian,Liu, Peiqing,Guo, Hao,&Qu, Qiulin.(2016).Effect of Sideslip on High-Angle-of-Attack Vortex Flow over Close-Coupled Canard Configuration.JOURNAL OF AIRCRAFT,53,217-230.
MLA	Chen, Mingqian,et al."Effect of Sideslip on High-Angle-of-Attack Vortex Flow over Close-Coupled Canard Configuration".JOURNAL OF AIRCRAFT 53(2016):217-230.

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