Curves of lift, moment, and drag were determined up to Mach numbers of M=0.87, and are compared to rectangular wing. English translation from Lilienthal-Gesellschaft fuer Luftfahrtforschung, Report 156, p 30-40.


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    Title :

    High-speed measurements on swept-back wing (Sweepback Angle phi=35°)


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Memo


    Contributors:


    Publication date :

    1947


    Size :

    17 pages


    Remarks:

    16 Supp plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :




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