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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    Titel :

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


    Beteiligte:
    H. H. Ottens (Autor:in)

    Erscheinungsdatum :

    1982


    Format / Umfang :

    18 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






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