How to model vortex of supersonic wing tip
I tried modelling a wing tip inside a rectangular mesh and simulate vortex behind it using fluent.
I used large eddy simulation as my solver and somehow there is no vortex in the contour plot no matter what other i choose.
Can anyone pls help on how to model a vortex for a supersonic wing tip?
|All times are GMT -4. The time now is 13:52.|