The NASA supercritical airfoil development program is summarized in a chronological fashion. Some of the airfoil design guidelines are discussed, and coordinates of a matrix of family related supercritical airfoils ranging from thicknesses of 2 to 18 percent and over a design lift coefficient range from 0 to 1.0 are presented.


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    Titel :

    NASA (National Aeronautics and Space Administration) Supercritical Airfoils: A Matrix of Family-Related Airfoils


    Beteiligte:
    C. D. Harris (Autor:in)

    Erscheinungsdatum :

    1990


    Format / Umfang :

    76 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch