Question: Simulate the flow around a SeligDonovan SD 2 0 3 0 airfoil section at a Reynolds number Re = 2 0 0 , 0 0

Simulate the flow around a SeligDonovan SD 2030 airfoil section at a Reynolds number Re =200,000 for air. Find the Lift Coefficient for an Angle of Attack 5 and 6.5 degrees from simulation. Show all your works.
Simulate the flow around a SeligDonovan SD 2 0 3

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