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RSTM convergence issues

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Old   June 23, 2006, 07:23
Default RSTM convergence issues
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Does anyone know good boundary and solution conditions to apply to the RSTM. I am struggling to get a good convergence having never used this particular turb model before. I am expecting a laminar flow from the inlet and my study involves a study of 2 different aerofoils IGE. Any suggestions would be very useful. Thanks in advance.

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