Pressure distribution at supersonic speeds on conically cambered wing with and without pylon mounted engine nacelles


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Pressure distributions at Mach numbers of 1.6 and 1.9 of a conically cambered wing of triangular plan form with and without pylon- mounted engine nacelles


    Contributors:

    Publication date :

    1956-04-20


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English