iteration on angles of attack -- CFD Online Discussion Forums

May 11, 2005, 12:52	iteration on angles of attack	#1
Vincent Guest Posts: n/a	Hi, Does anyone knows how to program in Fluent-Scheme so as to iterate a flow calculation around an airfoil on angles of attack ranging from 1 to 20 degrees for example, using the same mesh ? I also need to save the results of the calculation in a different file at each iteration. Thank you in advance Vincent.

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