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I am new to Hypermesh and am trying to analyse the load that will be exerted on the airfoil based on the pressure distribution along the airfoil (refer to pic). 

Is it possible to import these values from the graph into hypermesh? 


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Hi Toan,


I have attached the file. The first column indicates the chord wise position around airfoil from the leading edge in the clockwise sense, and the second column indicates the magnitude of pressure i wish to apply on the airfoil. 


Thanks so much for your help.




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