Wind tunnel study made to determine aerodynamic loading characteristics at 0.80 to 1.05 Mach and at angles of attack to 26°; pressure distributions and tabulated pressure coefficients are presented; leading edge separation vortex is dominant flow-field phenomenon.


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    Title :

    Transonic load characteristics of 3-percent-thick 60° delta-wing-body combination


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1961


    Size :

    127 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :