The present study deals with the behaviour of angle ply composite laminates subjected to low velocity impact. The laminates were prepared by E-glass fibres as reinforcement and epoxy as resin. Experiments were performed on these laminates by using low velocity drop weight set-up machine at three energy levels produced by using two masses. At energy level it was noticed that, [0/90]s laminate was most damage resistant and [0/15]s laminate was least resistant while the contact duration of impactor on laminate(s) was found to be sensitive to mass level. Finite Element (FE) analysis was performed to quantify the damage in laminates and investigate energy absorbed in intra-layer failure modes. During the post-processing FE analysis helps to mark the critical load points on the load-displacement history and quantification of distinct failure modes. The size of delamination profile was seen to be governed by fibre orientation and inter-laminar shear stresses at the interface.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Effect of fibre orientation on damage resistance of composite laminates


    Beteiligte:
    Khan, Sanan H. (Autor:in) / Khan, Ateeb Ahmad (Autor:in) / Husain, Afsar (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    2021-05-04


    Format / Umfang :

    13 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Unbekannt




    Damage Analysis of Composite Laminates

    Kumar, Nathi Venu / Rajamani, Palaniammal | SAE Technical Papers | 2019


    Impact Damage Resistance and Tolerance of Polymer Nanofiber Interleaved Composite Laminates

    Akangah, P. / Shivakumar, K. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012



    Fibre metal laminates

    Vlot, A. ;Gunnink, J. W. | British Library Conference Proceedings | 2001


    OPTIMIZED CROSS-ORIENTATION OF LAYERS IN COMPOSITE LAMINATES

    KISMARTON MAKS U | Europäisches Patentamt | 2018

    Freier Zugriff