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Old   May 24, 2005, 12:15
Default ablation
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Hi, I'm a fluent 6.2 user and I'm trying to solve the flow field in a hybrid rocket motor, but now I have the problem of defining the fuel mass flux at the solid wall (due to the solid ablation). I guess that the problem is to couple the temperature field in the solid with the flow field. Can anyone help me? Please let me know some good news as soon as possible. Raffaella
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