It is shown that lift distribution for biplane with unequal chords may be calculated by method developed in NACA Tech Report n 458, indexed in Engineering Index 1933 p 40, if corrections are made for inequality of chord lengths, method applied to four cases. (5¢)


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    Title :

    Relative loading on biplane wings of unequal chords


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:
    Diehl, W.S. (author)


    Publication date :

    1934


    Size :

    8 pages


    Remarks:

    Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :




    Relative loading on biplane wings

    Diehl, Walter S. | TIBKAT | 1933


    Relative loading on biplane wings

    Diehl, W.S. | Engineering Index Backfile | 1933


    Convertible monoplane -- Biplane wings

    Hall, R.F. | Engineering Index Backfile | 1926