In case of small leading airfoil full-scale and model maximum lift coefficients are in agreement at 0.74; with large leading airfoil, however, full scale reaches 0.85 as compared with 0.77 for model.


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    Title :

    Full-scale and model measurements of lift and drag of Bristol fighter with Handley Page slotted wings


    Additional title:

    Aeronautical Research Committee -- Reports Memoranda


    Contributors:
    Jones, E.T. (author) / Caygill, L.E. (author)


    Publication date :

    1925


    Size :

    9 pages


    Remarks:

    14 Figs.


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :