Loads are presented for wing-body combination at Mach numbers from 0.80 to 1.03 at angles of attack up to 26°; one wing was constructed of solid steel, other of plastic with steel core; twist distributions were calculated from experimental influence coefficients and pressure data; studies of flow in boundary layer presented.


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    Title :

    Investigation at transonic speeds of loading over 30° sweptback wing of aspect ratio 3, taper ratio 0.2, and NACA 65A004 airfoil section mounted on body


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1960


    Size :

    79 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :