Fluent Aero Fluid reversed flow on pressure inlet
Can you guide me, what does this statement means? (refer attachment)
Can we conclude based on this statement that our boundary condition is wrong? what does this statement signifies? How to resolve this?
I'm doing simulation in pressure far-field condition at outlet and at side, at inlet we considered pressure inlet and I have tried to increase the domain size but no change.
Mach 0.55 & AOA, AOS & Altitude is 0