Solution will not converge?
Hi,
I'm trying to simulate a wind tunnel test. The Fluent model has a fluid domain of 460 x 460 x 1220 mm, & at the center is a wing 'projected span' = 200mm, 'center chord' = 81.82mm. The educational version I'm using is limited to 512,000 cells. I've tried to use a fine mesh with 'inflation' layer on the wing. Slightly bigger mesh in a 'sphere of influence' around wing. Again a slightly bigger mesh for the rest of the 'fluid domain'. I'm using a coupled 'Pressure/Velocity', 1st order model, but can not get convergence. What should I do to try and get it to converge? Just incase, I've attached the files below: wbpj: https://app.box.com/s/vmiug2jscpole18zgod4 associated: https://app.box.com/s/vvezn5irwk2l9f5ga9is |
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