发明名称 Establishment of laminar boundary layer flow on an aerofoil body
摘要 In order to establish laminar flow on the attachment line (18) of an aerofoil body, a duct entrance (27) is provided on the leading edge of the aerofoil body for receiving spanwise boundary layer flow BLt. The exit (23) of the duct is located spanwise downstream of the duct entrance (27). The boundary layer flow BLt enters the duct (23) and is discharged downstream. The height of the duct entrance (27) above the leading edge of the aerofoil body is greater than the depth of the boundary layer BLt and thus a fresh laminar boundary layer is established on the outer surface (20) of the duct which propagates spanwise along the surface to rejoin the leading edge of the aerofoil body.
申请公布号 US8172185(B2) 申请公布日期 2012.05.08
申请号 US20070448437 申请日期 2007.12.20
申请人 GASTER MICHEAL;GASTER CONSULTANTS LTD 发明人 GASTER MICHEAL
分类号 B64C23/06 主分类号 B64C23/06
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