Analysis of stresses and aerodynamical characteristics of tapered cantilever wings; determination of shape of wing for producing given lift distribution; it is shown that tips of tapered wing are more heavily loaded than middle portion. (see also translation in Nat. Advisory Committee for Aeronautics -- Tech. Mem., no. 578, Aug. 1930, 20 pp., 16 figs.)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Design of tapered monoplane wings


    Additional title:

    Zur Berechnung von spitzendigen Eindecker-Trafluegeln


    Contributors:
    Amstutz, E. (author)

    Published in:

    Publication date :

    1930


    Size :

    6 pages


    Remarks:

    16 Figs.


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    German


    Keywords :


    Design of tapered monoplane wings

    Amstutz, E. | Engineering Index Backfile | 1930



    Calculation of tapered monoplane wings

    Amstutz, E. | TIBKAT | 1930


    Monoplane Wings With Sweep

    Crean, J.R. | Emerald Group Publishing | 1938


    Single-spar monoplane wings

    Engineering Index Backfile | 1929