Theoretical investigations of certain shapes of supersonic wings require knowledge of upwash in front of triangular wings with supersonic leading edges; such determination of upwash given.


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    Title :

    Flat triangular wing with subsonic leading edges in steady pitch and roll at supersonic velocities


    Additional title:

    Svenska Aeroplan Aktiebolaget -- Tech Note


    Contributors:


    Publication date :

    1952


    Size :

    22 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :