Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Boundary element methods for damage tolerance design of aircraft structures


    Contributors:

    Published in:

    Publication date :

    1998


    Size :

    173 S


    Remarks:

    23 cm
    Ill., graph. Darst
    Index
    Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek



    Type of media :

    Book


    Type of material :

    Print


    Language :

    English



    Classification :

    DDC:    629.13431
    BKL:    51.32 Werkstoffmechanik / 55.50 Luftfahrzeugtechnik



    Boundary Element Methods for Damage Tolerance Analysis of Aircraft Panels

    Salgado, N. K. / Aliabadi, M. H. / International Committee on Aeronautical Fatigue | British Library Conference Proceedings | 1997


    Boundary element analysis for damage tolerance assessment of aircraft panels

    Aliabadi, M.H. / Wen, P.H. / Salgado, N. | Tema Archive | 2002


    Finite Element-Based Damage Tolerance Methods for Aircraft Composites

    Beasley, J. / Cline, C. / Fay, R. et al. | British Library Conference Proceedings | 2011


    Finite element-based damage tolerance methods for aircraft composites

    Nikishkov, Yuri / Makeev, Andrew / Clinc, Christopher et al. | Tema Archive | 2011


    Optimal Design of Aircraft Structures with Damage Tolerance Requirements

    Arrieta, A. / Striz, A. / American Institute of Aeronautics and Astronautics et al. | British Library Conference Proceedings | 2000