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Propeller cavitation with non condensable gas(first constant property then ideal gas)

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Old   February 9, 2015, 04:47
Default Propeller cavitation with non condensable gas(first constant property then ideal gas)
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Behrooz Jamshidi
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Hi
Im modeling cavitation on a propeller with a constant volume fraction of air.After a procedure I got converged solution with reasonable results.
Now when I change air to ideal gas (with isothermal heat transfer) or define an expression for variable density with the previous run as initial value, I get overflow error on the first time step.
B.C:velocity inlet and opening with static pressure.
tstep=0.0001

Ive also decreased time step to 10e-9 which didnt help.
Decreasing relaxation factors caused overflow happen later(on 6th tstep)
Any idea?
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