My acceleration-time datas are in Excel table. There is acceleration(1G) condition in FE Model. My datas must effect my wing acceleration from 1g to 1.5g with time, and I want to see after 2000 sec, my fatigue life in FE Model
There is moment which is constant in FE model.
I want to analyze that performing fatigue analysis of my wing, whose acceleration changes during the flight between 1-1.5g.
What should my workflow be?
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