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Hi, is this solver suitable for compressible flows (e.g. flows around helicopter rotors, where on the advancing side the flow can get transonic) ?
As far as I know, LBM cases are currently limited by the Mach number. Are you also trying to address those limitations ?
Thank you a lot, very nice work indeed !
The text was updated successfully, but these errors were encountered:
The LBM model is limited to the weakly compresswible regime at Mach number < 0.3. In literature there is some extensions to get past this limit, but I'm currently not working on this. Better boundary model is up next.
Hi, is this solver suitable for compressible flows (e.g. flows around helicopter rotors, where on the advancing side the flow can get transonic) ?
As far as I know, LBM cases are currently limited by the Mach number. Are you also trying to address those limitations ?
Thank you a lot, very nice work indeed !
The text was updated successfully, but these errors were encountered: