Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Langley Full-scale-tunnel Investigation of the Fuselage Boundary Layer on a Typical Fighter Airplane with a Single Liquid-cooled Engine


    Contributors:

    Publication date :

    1946-06-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English