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January 21, 2022, 13:09 |
High error % moment coefficient
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#1 |
New Member
Kaung Myat
Join Date: Jan 2022
Posts: 1
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I simulated naca 4412 at 0 degree AoA and Re 1e6 in ansys fluent. Lift and drag coefficient results got acceptable value.but moment coefficient was positive value for chamber airfoil at 0 AoA(Cm= 0.21). Experimental value is -0.1. don't know why(. Advice me please
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