Three critical compression splice joint locations in a stitched graphite-epoxy transport wing stub box have been analyzed to determine their expected structural performance. The wing box is representative of a section of a commercial transport wing box and was designed and constructed by McDonnell Douglas Aerospace Company as part of the NASA Advanced Composites Technology (ACT) program. The results of the finite element analyses of the splice joints are presented. The analysis results indicate that failure will not occur in the splice joint regions for loads less than the Design Ultimate Load of the wing box.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Analysis of Selected Compression Splice Joint Locations in a Graphite-Epoxy Transport Wing Stub Box


    Beteiligte:
    D. C. Jegley (Autor:in)

    Erscheinungsdatum :

    1995


    Format / Umfang :

    34 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Composite material stub-blade wing joint

    Franklin, W.M. / Kreimendahl, B.W. | Tema Archiv | 1992


    Retractable angle-adjustable helicopter stub wing

    LI JUN | Europäisches Patentamt | 2020

    Freier Zugriff

    Fold wing tip having stub spar

    FOX BRUCE ROBERT | Europäisches Patentamt | 2018

    Freier Zugriff

    Novel helicopter stub wing and helicopter

    XU WEI / CHEN HONGYU / XU JINPENG et al. | Europäisches Patentamt | 2021

    Freier Zugriff