The required properties of standard load sequences are reviewed. The standard load sequence for transport aircraft wings (TWIST) and the fighter aircraft loading standard (FALSTAFF) are compared and reasons are given for their differences. The uses of standard load sequences for evaluation of material properties, fabrication techniques, structural details (fasteners), spectrum variation effects, and analytical prediction techniques are summarized.


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    Title :

    The Use of Standardized Fatigue Load Sequences in Coupon and Component Tests


    Contributors:

    Publication date :

    1980


    Size :

    30 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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