Hi,
I am getting different values for CL/CD depending on if I use half or full model geometry.
I setup a simple wing geometry.
My procedure for running half model. I set the geometry to no symmetry (half model). But set the VLM solver to X-Z symmetry. The Sref is for half wing.
CL = 0.55, CDtot = 0.03
Next, I set the geometry to symmetry X-Z (full model), no symmetry in the solver.
The Sref is for full wing.
CL = 0.275, CDtot = 0.015
Now obviously, there is a factor of 2 delta between the two solutions.
Is this intended behavior? or should the half model forces be decreased by 2?
- Daniel