Wing fatigue damage to aircraft was examined in regard to measurements made by peak-counting accelerometers. Major causes of damage were defined as repetitive stresses caused by ground loads, air loads and the ground-air-ground cycle. These phases of the aircraft loads environment were discussed in detail. Recommendations were made on the procedure for converting accelerometer data into loads spectra.


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    Titel :

    The Dissection of an Aircraft Loads Spectrum Produced by Peak-Counting Accelerometers


    Beteiligte:

    Erscheinungsdatum :

    1977


    Format / Umfang :

    24 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch