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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    Titel :

    Span load distribution for tapered wings with partial-span flaps


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- 23rd Annual Report


    Beteiligte:
    Pearson, H.A. (Autor:in)


    Erscheinungsdatum :

    1937


    Format / Umfang :

    18 pages


    Anmerkungen:

    Bibliography


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    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