Newly designed aircraft structures must be subjected to full scale fatigue/damage tolerance testing. The present paper describes an automated procedure for the generation of fatigue test load sequences, with specific reference to gust loads. The procedure uses a continuous gust concept. A statistical gust model, based on gust data recently published by FAA, is proposed. Specific attention is paid to the determination of the incremental load distributions due to gust on PSD basis.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Gust Load Conditions for Fatigue Tests Based on a Continuous Gust Concept


    Beteiligte:
    J. B. de Jonge (Autor:in) / W. J. Vink (Autor:in)

    Erscheinungsdatum :

    1997


    Format / Umfang :

    18 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Tests of gust-alleviating flap in gust tunnel

    Donely, P. / Shufflebarger, C.C. | Engineering Index Backfile | 1940


    Tests of gust-alleviating flap in gust tunnel

    Donely, P. / Shufflebarger, C.C. | Engineering Index Backfile | 1940


    Gust and counter gust

    Pritchard, D. | Engineering Index Backfile | 1966