Hi Rob,nnThe material density is not pressure dependent so i have left the outlet pressure = 0. nWhen Run the simulation i get this result:n
nThis does not look right compared to other simulation that were run (The contour plane is at the cross-section of the Nacelle). Surely the pressure should increase towards the fan area and the walls of the Turbofan. Do you think this may be a boundary condition problem or a mesh problem or somthing else that i am not aware of.Regardsn
nThis does not look right compared to other simulation that were run (The contour plane is at the cross-section of the Nacelle). Surely the pressure should increase towards the fan area and the walls of the Turbofan. Do you think this may be a boundary condition problem or a mesh problem or somthing else that i am not aware of.Regardsn
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