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    Title :

    The Effect on Zero-lift Drag of an Indented Fuselage or a Thickened Wing-root Modification to a 45 Degrees Sweptback Wing-body Configuration as Determined by Flight Tests at Transonic Speeds


    Contributors:

    Publication date :

    1951-09-20


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English