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Mistake: negative pressure factor

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Old   May 3, 2005, 15:43
Default Mistake: negative pressure factor
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1.Why Fluent at non-stationary process for calculation of wing structure gives wrong results? 2.Mistake: distribution of pressure factor to a back edge is negative and that cannot be. 3.Boundary conditions: on an input speed is set (Velosity- inlet), on back border I set Outflow
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