A mathematical model for investigating the fatigue performance of structural materials and configurations is presented. This proposed loading standard has been adopted by Germany and the Netherlands and used to test transport aircraft wing root bending. Algorithms and input data for applying the program to fighter aircraft wing bending are presented. (Author)


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    Titel :

    Falstaff. Description of a Fighter Aircraft Loading Standard for Fatigue Evaluation


    Erscheinungsdatum :

    1976


    Format / Umfang :

    71 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    FALSTAFF : description of a Fighter Aircraft Loading STAndard For Fatigue

    Flugzeugwerke Emmen, Switzerland / Laboratorium für Betriebsfestigkeit | TIBKAT | 1976





    Parametric Fatigue Analysis of USAF Fighter Aircraft

    G. J. Roth / B. S. West | NTIS | 1970