NACA 0012 Drag Minimization -- CFD Online Discussion Forums

January 15, 2022, 11:01

NACA 0012 Drag Minimization

abhijithmoni

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Abhijith

Join Date: Nov 2020

Location: United Kingdom

Posts: 19

Rep Power: 5

I'm trying to minimize the drag of the NACA 0012 airfoil. Please find the details in the attached image. It is a symmetric case with only the upper surface.

I'm trying the following constraints:

OPT_OBJECTIVE= DRAG

OPT_CONSTRAINT= ( AIRFOIL_THICKNESS > 0.6 ) * 1.0

But the results are wrong. I think the problem is with my constraints. Please help me fix this.

Attached Images

naca0012.jpg (52.1 KB, 12 views)

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