This presentation is regarding tool validation used for prediction of the GIII wing normal, bending, and torque loads.


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    Title :

    Evaluation of Load Analysis Methods for NASA's GIII Adaptive Compliant Trailing Edge Project


    Contributors:

    Conference:

    AIAA SciTech 2016 ; 2016 ; San Diego, CA, United States


    Publication date :

    2016-01-04


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English