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    기술보고서 게시판 내용
    타이틀 AIR EJECTOR EXPERIMENTS USING THE TWO-DIMENSIONAL SUPERSONIC-CASCADE TUNNEL (2nd Report, Relationship between Ejector Performance and Throat Area Ratio [I] )
    저자 Susumu TAKAMORI, Hajime SAKAGUCHI
    Keyword compressible flow; subsonic air ejector experiments, ejector performance
    URL http://send.nal.go.jp/send/jpn/dlpdf.php3/naltm00642.pdf?id=NALTM0000642
    보고서번호 NAL TM-642
    발행년도 1991.12
    출처 NAL (National Aerospace Laboratory of Japan)
    ABSTRACT To determine the feasibility of using an ejector as a suction pump for boundary-layer air removal in the Two-Dimensional Supersonic Cascade Tunnel, especially when a portion of the tunnel′s air supply is used for its primary flow, both subsonic and supersonic air ejector tests were conducted. The area ratio on the secondary-flow rate of a subsonic ejector.

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