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[DesignModeler] Changing airfoil thickness for DOE analysis |
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September 7, 2015, 08:13
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Changing airfoil thickness for DOE analysis
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New Member
Soheil
Join Date: Mar 2014
Location: Helsinki
Posts: 21
Rep Power: 12  |
Hi.
I'm using ANSYS DesingXplorer for optimizing a wing. Wing root chord length is 1.21m and tip chord is 0.234m. One of my input parameters for DOE is airfoil thickness to chord ratio (t/c). I'm wondering how can I change airfoil thickness without any change to chord length? is it even possible or it's just the only way? for example, I'm changing it from t/c=0.1 to t/c=0.06. but root chord changes from 1.21 to 0.731, respectively. Airfoil is naca64a210. Thank you. |
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| Tags |
| airfoil, design modeler, doe, thickness |
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