Flight Tests at Supersonic Speeds to Determine Effect of Taper on Zero-Lift Drag of Sweptback Low-Aspect-Ratio Wings.


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    Title :

    Flight tests at supersonic speeds to determine effect of taper on zero-lift drag of sweptback low-aspect-ratio wings


    Additional title:

    NACA -- Tech Note


    Contributors:
    Pittel, M. (author)


    Publication date :

    1956


    Size :

    20 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English