Pressure measurements made at Mach number of 0.13 and Reynolds number of 2.4 million based on mean aerodynamic chord; values of section and wing lift coefficients, and centers of pressure derived from pressure data, also given.


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    Title :

    Chordwise and spanwise loadings measured at low speed on triangular wing having aspect ratio of two and NACA 0012 airfoil section


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Wick, B.H. (author)


    Publication date :

    1948


    Size :

    12 pages


    Remarks:

    16 Supp plates


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :