Shock expansion method described in Tech Note n 1143, separately indexed, was used to determine principal aerodynamic characteristics of supersonic airfoils; effect of thickness ratio, free stream Mach number, angle of attack, camber, thickness distribution, and aileron deflection; minimum drag of supersonic airfoils obtained when maximum thickness is behind 0.50 chord.


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    Title :

    Notes on theoretical characteristics of two-dimensional supersonic airfoils


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Ivey, H.R. (author)


    Publication date :

    1947


    Size :

    9 pages


    Remarks:

    14 Supp Plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :