发明名称 Fluid flow control device
摘要 A fluid flow control device controllably maintains attached flow in the region of a body having a contour of rapid curvature utilizing tangential fluid discharge slots, positioned just upstream from the separation line, which issue a thin jet sheet to energize the boundary layer and entrain the surrounding flow. When applied to the aft fuselage of an aircraft, the device reduces separation and vortex drag at cruise and provides control forces and moments during low speed operation of the aircraft.
申请公布号 US4736913(A) 申请公布日期 1988.04.12
申请号 US19860909349 申请日期 1986.09.19
申请人 LOCKHEED CORPORATION 发明人 BENNETT, JOHN A.;ENGLAR, ROBERT J.;THOMAS, ANDREW S. W.
分类号 B64C21/04;B64C23/06;(IPC1-7):B64C21/04 主分类号 B64C21/04
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