72 wing flap combinations, including two aspect ratios, four taper ratios, and nine flap lengths are included in tables; comparisons between theoretical and experimental results for wings indicate that theory may be used to predict load distribution with sufficient accuracy for structural purposes.


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    Title :

    Span load distribution for tapered wings with partial-span flaps


    Additional title:

    Nat Advisory Committee Aeronautics -- 23rd Annual Report


    Contributors:


    Publication date :

    1937


    Size :

    18 pages


    Remarks:

    Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    Span load distribution for tapered wings with partial-span flaps

    Pearson, H.A. | Engineering Index Backfile | 1937



    Calculation of aerodynamic characteristics of tapered wings with partial-span flaps

    Pearson, H.A. / Anderson, R.F. | Engineering Index Backfile | 1939