No 310: Effects of changes in forces on each wing of biplane cellule when either stagger or gap is varied are shown in data obtained from distribution tests made in atmospheric wind tunnel; since each test was carried up to 90-deg. angle of attack, results may be used in study of stalled flight and of spinning as well as in structural design of biplane wings.


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    Title :

    Wind tunnel pressure distribution tests on a series of biplane wing models; effects of changes in stagger and gap


    Additional title:

    Nat. Advisory Committee Aeronautics -- Tech. Note


    Contributors:
    Knight, M. (author) / Noyes, R.W. (author)


    Publication date :

    1929


    Size :

    13 pages


    Remarks:

    23 Figs.


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :