In this paper, the mechanical behaviors of pure Ti and new Ti-alloy films and CFRP/Ti-alloy laminated composites are investigated in order to research of development of fiber metal laminates tanks for cryogenic rocket propellants. Tensile tests of pure Ti and new -Ti alloy films and CFRP/Tialloy laminated composites are performed. Characterization of the nonlinear behaviors of pure Ti and new Ti-alloy films are evaluated by elastoplastic model. As for CFRP/Ti alloy, it is shown that there is little residual strain compared with CFRP/pure Ti. Internal damage is evaluated by cross-sectional observation. From the crosssectional observation, no damage was observed in the metal layer, though transverse cracks were propagated in the CFRP 90 degree layers.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Mechanical properties of CFRP/Ti-alloy laminated composites


    Contributors:


    Publication date :

    2007


    Size :

    7 Seiten, 10 Bilder, 2 Tabellen, 12 Quellen


    Type of media :

    Conference paper


    Type of material :

    Storage medium


    Language :

    English





    Electric Current Analysis for Thick Laminated CFRP Composites

    Todoroki, A. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012


    CFRP Laminated structure of CFRP roof rail

    SONG IL JONG / JEON JAEMIN | European Patent Office | 2019

    Free access

    CFRP Laminated structure of CFRP roof rail

    SONG IL JONG / JEON JAEMIN | European Patent Office | 2019

    Free access

    Probabilistic Progressive Failure Analysis of CFRP Laminated Plates

    Xiangyang, W. / Jianqiao, C. / Xiedong, Z. | British Library Online Contents | 2004