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境界層制御装置及び風洞装置

机译:边界层控制装置及风洞装置

摘要

PROBLEM TO BE SOLVED: To provide a boundary layer control device capable of performing a more accurate wind tunnel test and a wind tunnel device having the boundary layer control device.;SOLUTION: A boundary layer control device includes: a chamber 14 is a box-shaped which is recessed from an inner wall surface 3A constituting an air flow passage causing air-flow W generated by a blower to flow and provided with a front plate 16 formed in a shape toward a downstream side of the air-flow W as approaching to the inner wall surface 3A; a partition plate 18 provided inside the chamber 14 and dividing a space inside the chamber 14 into a duct space 10 of an upstream side and a header 12 for blowout at the downstream side; and the airflow passage and a nozzle 21 for blowing out the air inside the header 12 for blowout via an opening to the inner wall surface 3A of the chamber 14. The duct space 10 includes a main duct 10A of the upstream side and a sub-duct 10B being connected to a downstream side of the main duct 10A and smaller in depth than the main duct.;SELECTED DRAWING: Figure 3;COPYRIGHT: (C)2019,JPO&INPIT
机译:解决的问题:提供一种能够进行更精确的风洞测试的边界层控制装置以及具有该边界层控制装置的风洞装置。解决方案:边界层控制装置包括:腔室14是箱形的-该前板16从构成空气流路的内壁面3A凹进,该空气流道使由鼓风机产生的气流W流动,并且设有前板16,该前板形成为朝向气流W的下游侧。内壁面3A。隔板18设置在腔室14内,并且将腔室14内的空间分成上游侧的导管空间10和下游侧的用于吹出的集管12。通道空间10包括:上游侧的主导管10A;以及从上游侧的主导管10A;以及用于从集管12内部吹出空气的喷嘴的气流通道和喷嘴21,该开口通往腔室14的内壁表面3A。管道10B连接到主管道10A的下游侧,并且深度小于主管道。;选定图:图3;版权:(C)2019,日本特许厅&INPIT

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