No 325: Effects of changes in decalage; dihedral, sweepback, and overhang upon biplane wings are discussed; data obtained from pressure distribution tests made in atmospheric wind tunnel; way in which loadings on wings are effected by changes shows that results may be used in study of stalled flight and spinning and 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 :

    6 pages


    Remarks:

    36 Supp. Figs.


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :