Tests were performed on a wing of the lightweight aircraft LFU 205. The wing was tested in critical load cases up to 1.5 times the value of the safe load. Even higher safe load values were to some extent achieved. The test results provide information on the tensile strength, stability, and deformation characteristics of the wing and thus permit an assessment of the spanwise tubular method of construction. (Author)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Static Load Tests on an Lfu 205 Wing of Spanwise Tubular Construction


    Beteiligte:
    R. Schuetze (Autor:in)

    Erscheinungsdatum :

    1975


    Format / Umfang :

    44 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Spanwise Adaptive Wing

    D. Spivey / P. Suh | NTIS | 2018


    Spanwise Adaptive Wing

    Moholt, Matthew / Benafan, Othmane | NTRS | 2017


    Spanwise Adaptive Wing

    Spivey, David / Suh, Peter | NTRS | 2018


    Segmented wing test technique for obtaining spanwise load distributions

    Wasson, H.R. / Mehus, T.E. | Engineering Index Backfile | 1967