It has been customary to calculate strength of rear wing beam for "high-speed" condition on assumption that center of pressure was at 0.50 of wing chord. It is shown that this assumption is not justified.


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    Title :

    Center of pressure coefficients for aerofoils at high speeds


    Additional title:

    Nat. Advisory Committee Aeronautics Tech. Notes


    Contributors:
    Diehl, W.S. (author)


    Publication date :

    1922


    Size :

    2 pages


    Remarks:

    3 Figs.


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :