|April 28, 2011, 22:28||
Join Date: Nov 2009
Posts: 411Rep Power: 11
can someone recommend me some good references about shape optimization of airfoils for a range of angles of attack ? Say to minimize the Cd for alpha from 0 to 10 degree.
I wonder if this approach to airfoil optimization (keeping the Mach and Reynolds fixed but for multiples incidences) is possible especially for transonic flows.
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