reversed flow in over-expanded supersonic nozzle
hi All,
got a headache with convergence of the solution because of reversed flow. i do have over-expanded supersonic nozzle where the back-flow presents at the end of the nozzle wall. pressure inlet- 6 bar (means 5 bar as gauge pressure) + To- 800K pressure outlet- 1 bar (absolute) + To- 300K reference- 1 bar tried first order, solution steering, limits. nothing helps... once I got reversed flow the solution is down.. NB: have no problem with the same nozzle in CFX (using the opening at the outlet). The reason I'd like to use Fluent is because of the CUT-CELL mesh. Any suggestion or ideas on how to get rid of the reversed flow at the end of the nozzle wall? pls help. |
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