I am trying to simulate the lift produced on an aircraft wing. The wing is oriented such that air enters from the -y direction. The freestream velocity in the results control, forces and moments coefficients only allows a positive input. Do I have to flip my model in CAD or is there a simple fix for this?
Hi @34a07642e91b43,
Thanks for posting your question. As this (|U<∞>|) Freestream velocity magnitude regards an absolute value, you can directly put the same value as Velocity Inlet, but using the positive value.
Example: Velocity inlet = -5 m/s; (|U<∞>|) = 5 m/s.
best,