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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    Title :

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


    Contributors:

    Publication date :

    1977


    Size :

    24 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English