Purpose of analysis is to enable designers to evaluate significance of such effects in early design stages; it also should serve as guide to structural analysts who must set up and carry out detailed program for defining load life histories and establishing design criteria.


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    Titel :

    Effects of operational factors on structural fatigue in fighter type aircraft


    Weitere Titelangaben:

    Soc Automotive Engrs -- Paper


    Beteiligte:
    Mangurian, G.N. (Autor:in) / Brooks, P.D. (Autor:in)

    Kongress:

    Society of Automotive Engineers -- Meeting ; 1954 Stresses



    Erscheinungsdatum :

    1954


    Format / Umfang :

    10 pages


    Anmerkungen:

    Bibliography


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Effects of Operational Factors on Structural Fatigue in Fighter Aircraft

    Mangurian, George N. / Brooks, Philip D. | SAE Technical Papers | 1955


    Parametric Fatigue Analysis of USAF Fighter Aircraft

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


    OPERATIONAL LOAD REGRESSION EQUATION DEVELOPMENT FOR ADVANCED FIGHTER AIRCRAFT

    Kaneko, H. / Furukawa, T. / International Council of the Aeronautical Sciences | British Library Conference Proceedings | 2004


    Structural composites on future fighter aircraft

    GLENN, T. / KOCH, L. | AIAA | 1973