Description and constructional details of facility which by exchanging part of test section can be employed as high speed annular cascade wind tunnel and transonic axial flow test compressor; specifications for two installations are given. (In Japanese with English abstract)


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    Title :

    High speed annular cascade wind tunnel and transonic axial flow test compressor


    Additional title:

    Tokyo. Univ -- Inst Space Aeronautical Science -- Bul


    Contributors:
    Tanaka, H. (author) / Maruta, H. (author) / Hatta, K. (author) / Amino, K. (author)


    Publication date :

    1965


    Size :

    19 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    Japanese


    Keywords :


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