A simple mathematical model of the NF-5A aircraft was developed. The model is validated by measured results. Landing gear loads are calculated for the aircraft taxiing across a repaired runway using an AM-2 mat. The results depend strongly on the heaving and pitching motion of the aircraft when it meets the repair.


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    Title :

    Predicted and Measured Landing Gear Loads for the NF-5 Aircraft Taxiing over a Bumpy Runway


    Contributors:

    Publication date :

    1982


    Size :

    18 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English






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