Stress analysis on airfoil
Altair Forum User
Altair Employee
Hi,
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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Answers
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the graph data is in dat. format
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Could you please send us an example for your input data in the format you said? then we can give it a try.
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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.
Amanda
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