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#1 |
New Member
bharath L
Join Date: Dec 2021
Posts: 2
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hello everyone,
i've been trying to do wing analysis in fluent lately, and im using ansys student version software. the wing analysis results giving me values as lift=12000 N and drag=2000N, but i need the lift value to be around 5000N according to the hand calculations and i am getting coeff of lift = around 7 in fluent but i need my coeff of lift value to be 1.6 which is at the stall angle 16 degree for speed of 61 m/s. can some one explain what is need to be done? and my wing design have twist and dihedral angle in it. |
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Tags |
analysis, fluent, wing |
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