1–10 von 10 Ergebnissen
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    Computational intelligence aspects for defect classification in aeronautic composites by using ultrasonic pulses

    Cacciola, M. / Calcagno, S. / Morabito, F.C. et al. | Tema Archiv | 2008
    from faults and problems. Errors during the manufacturing or the plies' overlapping, in fact, can cause particular flaws in the resulting ...

    Recent advances in building with composites

    Soutis, C. | Tema Archiv | 2009
    Composite materials have gained popularity (despite their generally high cost) in high performance products that need to be lightweight ...

    Influence of delamination on impact damage in composite structures

    Johnson, A.F. / Holzapfel, M. | Tema Archiv | 2006
    To reduce development and certification costs for composite aircraft structures, efficient computational methods are required by the ...

    Fatigue Analysis of a Motorcycle Frame System Based on a Road Test and the Finite Element Method

    Zhang, Liang / Lu, Cheng / Tieu, A.Kiet | Tema Archiv | 2013
    frame manufactured from two different materials by carrying out a road test in combination with computational simulation work based on the ...

    Delamination testing and modelling for composite crash simulation

    Greve, L. / Pickett, A.K. | Tema Archiv | 2006
    The availability of high performance low cost carbon fibre in materials such as non crimp fabrics (NCF) has led to renewed interest in ...

    A Machine Learning Approach to Load Tracking and Usage Monitoring for Legacy Fleets

    Cheung, Catherine / Sehgal, Srishti / Valdés, Julio J. | Springer Verlag | 2019
    aircraft component loads during flight is a challenge that has inspired the implementation of computational intelligence and machine learning ...

    Structural design and development of multiband aero-vehicle smart skin antenna

    Park, Gyuhae / Lee, Jung-Ryul / Park, Chan-Yik et al. | Tema Archiv | 2014
    The load-bearing antenna approach for state-of-the-art aero-vehicle structure has been made for military aircraft in recent studies. This ...

    Static and dynamic indentation response of fine grained boron carbide

    Subhash, Ghatu / Ghosh, Dipankar / Maiti, Spandan | Tema Archiv | 2008
    a function of grain size. It was noted that the indentation-induced cracks during static indentation were transgranular in nature with zig ...

    Fracture analysis for damaged aircraft fuselage using substructure method

    Ju, Jinsan / You, Xiaochuan / Jiang, Xiugen et al. | Tema Archiv | 2008
    This paper primarily describes the development and application of substructure computational analysis techniques to determine stress ...