Factors derived from wing theory presented; by means of these factors, angle of zero lift, lift curve slope, pitching moment, aerodynamic center position, and induced drag of tapered wings with partial span flaps may be calculated; factors given for wings of aspect ratios 6 and 10, of taper ratios from 0.25 to 1.00, and with flaps of various lengths. (10¢)


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    Title :

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


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:


    Publication date :

    1939


    Size :

    18 pages


    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


    Span load distribution for tapered wings with partial-span flaps

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