Report supplements information presented previously (see reference to NACA -- TN 1368, by L.K.LOFTIN, Jr, in Engineering Index 1947 p 25), and provides ordinates of additional airfoil sections useful in design of supersonic aircraft; simplified procedure for obtaining pressure distributions about airfoil sections of intermediate thicknesses.


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    Titel :

    Ordinates and theoretical pressure-distribution data for NACA 6- and 6a-series airfoil sections with thicknesses from 2 to 21 and from 2 to 15 percent chord, respectively


    Weitere Titelangaben:

    NACA -- Tech Note


    Beteiligte:
    Patterson, E.W. (Autor:in) / Braslow, A.L. (Autor:in)


    Erscheinungsdatum :

    1958


    Format / Umfang :

    99 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :