The impact of buckling containment features on the stability of thin-gauge fuselage, metallic stiffened panels has previously been demonstrated. With the continuing developments in manufacturing technology, such as welding, extrusion, machining, and additive layer manufacture, understanding the benefits of additional panel design features on heavier applications, such as wing panels, is timely. This compression testing of thick-gauge panels with and without buckling containment features has been undertaken to verify buckling and collapse behaviors and validate sizing methods. The experimental results demonstrated individual panel mass savings on the order of 9%, and wing cover design studies demonstrated mass savings on the order of 4 to 13%, dependent on aircraft size and material choice.


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    Titel :

    Wing Panel Design with Novel Skin-Buckling Containment Features



    Erschienen in:

    Erscheinungsdatum :

    2016




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :

    Klassifikation :

    BKL:    55.50 Luftfahrzeugtechnik / 55.50
    Lokalklassifikation TIB:    770/7040




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    Houston, G. / Quinn, D. / Murphy, A. et al. | AIAA | 2015


    Fatigue performance of aircraft panels with novel skin buckling containment features

    Quinn, D / Murphy, A / Cervi, L | SAGE Publications | 2011



    The Impact of Geometric Imperfections on Metallic Stiffened Panels with Skin Bay Buckling Containment Features

    Houston, G. / Quinn, D. / Murphy, A. et al. | British Library Conference Proceedings | 2012