Determine lift and Drag at a particular altitude (10,000 ft)

AlfredOlooAlfredOloo KenyaMember


I want to simulate the amount of LIFT and Drag in an AIRFOIL WING flying at an altitude of 10,000ft at a speed of 24m/s.

Can someone show me what to change within ANSYS FLUENT to help me do this, please?

At 10,000ft the pressure is about 69.7kPa.




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