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    기술보고서 게시판 내용
    타이틀 A Pressur Test of RCS Jet Interference at a Mach Numbere of 5 for a Tip Fin Configuration TM-714
    저자 Shinji NAGAI, Koichi HOZUMI, Akira YOSHIZAWA, Nobutoshi HARA, Kiyomichi ISHIDA, Keisuke FUJII
    Keyword hypersonic flow; reaction control system; jet interference; tip fin
    URL http://send.nal.go.jp/send/jpn/dlpdf.php3/naltm0000714.pdf?id=NALTM0000714
    보고서번호 NAL TM-714
    발행년도 1977.7
    출처 NAL (National Aerospace Laboratory of Japan)
    ABSTRACT Aerodynamic interference induced by a reaction control system (RCS) jet was investigated for a tip fin configuration at a Mach number of 5. Surface pressure distributions and oil-flow photographs were obtained using cold gas simulation techniques with yaw jet scaled nozzles in the NAL φ50 cm hypersonic wind tunnel. It was found that the interference flow field changed as angles of atta

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