发明名称 Boundary layer control systems.
摘要 A boundary layer control system is provided which comprises a surface (10), several heater elements (11) lying substantially flush with the surface (10) for heating the boundary layer and several cooling elements (12) lying substantially flush with the surface (10) downstream of the heater elements (11). The arrangement is such that boundary layer flow passing over the heater elements (11) is locally heated and thus destabilised and when passing over the cooling elements (12) the heat flux is directed towards the surface. In this way transition delay of the boundary layer is effected. <IMAGE>
申请公布号 EP0589728(A1) 申请公布日期 1994.03.30
申请号 EP19930307622 申请日期 1993.09.27
申请人 BRITISH AEROSPACE PUBLIC LIMITED COMPANY 发明人 MAJDALAWI, FOUAD;NAYFEH, ALI HASAN
分类号 B64C21/00;(IPC1-7):B64C21/00 主分类号 B64C21/00
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