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.
Predicted and Measured Landing Gear Loads for the NF-5 Aircraft Taxiing over a Bumpy Runway
1982
18 pages
Report
Keine Angabe
Englisch
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