The analytical part of an extensive damage tolerance evaluation of the fighter aircraft 37 Viggen is presented. The complementing experimental investigation is discussed in the companion paper. Topics addressed include load spectra, stress analysis, fracture mechanics and fatigue crack propagation. The following conclusions are made: the methodology used is verified and is state of the art; damage tolerance is analytically proven and experimentally demonstrated; extension of the original design life is currently being considered.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Damage Tolerance of the Fighter Aircraft 37 Viggen. Part 1: Analytical Assessment


    Beteiligte:
    B. Palmberg (Autor:in) / P. Boman (Autor:in) / M. Olsson (Autor:in) / A. F. Blom (Autor:in)

    Erscheinungsdatum :

    1990


    Format / Umfang :

    12 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






    Damage tolerance assessment of the fighter aircraft 37 Viggen main wing attachment

    PALMBERG, BJORN / OLSSON, MATS-OLOF / BOMAN, PER-OLOF et al. | AIAA | 1993


    Damage Tolerance Analysis and Testing of the Fighter Aircraft 37 Viggen

    B. Palmberg / M. O. Olsson / P. O. Boman et al. | NTIS | 1990


    EMC in Viggen aircraft

    Rapp, L.J. / Paulsson, A.I. | Engineering Index Backfile | 1968