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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    Title :

    NASA supercritical airfoils: A matrix of family-related airfoils


    Contributors:

    Publication date :

    1990-03-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :