A standardized load sequence was derived by averaging the theoretical and experimental frequency distributions of loads on the wing roots of transport aircraft. The sequence is considered to be representative for the load history of the wing root of transport aircraft. It is proposed to adopt the standardized sequence for various aeronautical fatigue testing purposes.


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    Title :

    A Standardized Load Sequence for Flight Simulation Tests on Transport Aircraft Wing Structures Standardisierter Einzelflug-Belastungsablauf fuer Schwingfestigkeitsversuche an Tragflaechenbauteilen von Transportflugzeugen


    Contributors:
    D. Schuetz (author) / H. Lowak (author) / J. B. Dejonge (author) / J. Schijve (author)

    Publication date :

    1973


    Size :

    58 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English