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Solid Rocket Simulation (Transient Case) Fuel Reduction

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Old   October 8, 2013, 12:57
Default Solid Rocket Simulation (Transient Case) Fuel Reduction
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Hi,

I am trying to simulate a solid rocket motor in Fluent where my focus in the study is to see the regression on the fuel surface within the combustion chamber for a certain range of time. Is this possible to do in Fluent?

Thank you very much for your insights!!
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