Six fatigue tests were conducted on C-46 aircraft wings; 2 at high constant-amplitude load, 2 with loading schedules based on gust-frequency statistics, and 2 with loading schedules developed from maneuver-loads statistics; results presented, discussed, and compared with previously published data from other tests in this series.


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    Title :

    Fatigue investigation of full-scale transport-airplane wings -- Tests with constant-amplitude and variable-amplitude loading schedules


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1960


    Size :

    37 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English