To provide data for use in interceptor aircraft mission analyses, studies made in NACA Lewis icing tunnel, included effect of icing on airfoil section lift, drag, and pitching. See also NACA -- Tech Note 4151, separately indexed.


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    Title :

    Aerodynamic effects caused by icing of unswept NACA 65A004 airfoil


    Additional title:

    NACA -- Tech Note


    Contributors:


    Publication date :

    1958


    Size :

    47 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :