airfoil stall -- CFD Online Discussion Forums

November 21, 2007, 08:50	airfoil stall	#1
marek Guest Posts: n/a	Hi! I made simulation of flow around airfoil and I got very good results for AOA up to stall angle. I used SST model with gamma-theta transition model, y+ is less than 1 (about 0.75),... I tried with stady state simulation and also with transient but results were the same. Drag was near true but lift was too high because flow didn't separate. Can anybody tell me how can I improve results around stall angle! Best Regards marek

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