The new developed airplane structures present a collection of several technologies and materials. This tendency is based on the load tailored design of modern airplanes. Especially, the fuselage contains different affected areas. In consequence of the technology substitutions made, the effort of validation and approval activities grows significantly. So the role of curved panel tests has to be redefined. The capability of special task test devices has improved continuously. With the reached higher simulation accuracy the experimental fatigue and damage tolerance analysis has been enabled for the whole panel including every stiffener detail.


    Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    A test concept for future aircraft fuselage panels


    Contributors:
    Best, R. (author) / Fleischer, T. (author) / Götze, M. (author) / Sachse, M. (author) / Semsch, M. (author)


    Publication date :

    2009


    Size :

    12 Seiten, 11 Bilder, 4 Quellen




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    A test concept for future aircraft fuselage panels

    Best, R. / Fleischer, T. / Gotze, M. et al. | British Library Conference Proceedings | 2009


    Aircraft fuselage panels of expanded steel

    Sherman, W.F. | Engineering Index Backfile | 1942


    AIRCRAFT FUSELAGE ASSEMBLY JIG AND METHOD FOR HANDLING AIRCRAFT FUSELAGE PANELS

    KASAHARA KENJI / SEGAWA SHUHEI | European Patent Office | 2017

    Free access

    VIRTUAL TESTING OF AIRCRAFT FUSELAGE STIFFENED PANELS

    Linde, P. / Pleitner, J. / Rust, W. et al. | British Library Conference Proceedings | 2004