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An Investigation of the Aerodynamic Performance for a Fuel Saving Double Channel Wing Configuration
Wang, Hongbo; Gan, Wenbiao; Li, Daochun
刊名ENERGIES
2019
卷号12
关键词fuel saving drag reduction lift-to-drag ratio propeller slipstream double channel wing configuration
DOI10.3390/en12203911
URL标识查看原文
收录类别SCIE ; EI
WOS记录号WOS:000498391700107
内容类型期刊论文
URI标识http://www.corc.org.cn/handle/1471x/5914694
专题北京航空航天大学
推荐引用方式
GB/T 7714
Wang, Hongbo,Gan, Wenbiao,Li, Daochun. An Investigation of the Aerodynamic Performance for a Fuel Saving Double Channel Wing Configuration[J]. ENERGIES,2019,12.
APA Wang, Hongbo,Gan, Wenbiao,&Li, Daochun.(2019).An Investigation of the Aerodynamic Performance for a Fuel Saving Double Channel Wing Configuration.ENERGIES,12.
MLA Wang, Hongbo,et al."An Investigation of the Aerodynamic Performance for a Fuel Saving Double Channel Wing Configuration".ENERGIES 12(2019).
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