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    기술보고서 게시판 내용
    타이틀 Static Pressure Measurements on the Surface of the Model Strut and the Sidewall in the NAL 2m×2m Transonic Wind Tunnel Test Section
    저자 Akira KOIKE, Nobuyuki HOSOE, Seigo NAKAMURA, Yasuo OGUNI, Koichi SUZUKI, Toshio KARASAWA
    Keyword model support system; aerodynamical vibration; static pressure distribution
    URL http://send.nal.go.jp/send/jpn/dlpdf.php3/naltm00657.pdf?id=NALTM0000657
    보고서번호 NAL TM-657
    발행년도 1993.7
    출처 NAL (National Aerospace Laboratory of Japan)
    ABSTRACT To identify the source of severe aerodynamical vibration encountered with the complete-air-plane model support system of the NAL 2m×2m Transonic Wind Tunnel at higher supersonic Mach numbers, static pressure distributions were measured on the surface of the model strut and the sidewall. The model strut is installed in the Semispan-model Test Section which originally has a free space at the portion corresponding to the model support system position in the Complete

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