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July 21, 2015, 17:16
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DAKOTA/Openfoam
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#1 |
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New Member
samira
Join Date: Feb 2015
Location: Iran
Posts: 16
Rep Power: 11  |
Dear everyone,
I am working on airfoil shape optimization with openfoam and Dakota.. The a irfoil shapes are parameterized using Bezier curves,12 control points are used for parameterization,For an airfoil curve, two points are fixed since they represent the leading and trailing edge of the airfoil. The intermediate points are a llowed to move within the specified boundaries. A maximum thickness constraint of 19% - 22% of chord is imposed on the airfoil.. how I define control points and The constraints in DAKOTA for generate different airfoil? Any comments and suggestions are welcomed Best regards Samira |
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July 27, 2015, 09:45
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#2 |
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New Member
samira
Join Date: Feb 2015
Location: Iran
Posts: 16
Rep Power: 11 |
waiting for a reply
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July 28, 2015, 06:11
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#3 |
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Senior Member
Niels Nielsen
Join Date: Mar 2009
Location: NJ - Denmark
Posts: 555
Rep Power: 27 |
Using Google for 1s,
First result. http://www.dicat.unige.it/guerrero/dakotaof.html Second result http://www.tfd.chalmers.se/~hani/kur...nsource_AJ.pdf Nobody are going to give you a ready to run case, you need to do the leg work yourself.
__________________
Linnemann PS. I do not do personal support, so please post in the forums. |
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