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aeroengine intake at altitude

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Old   September 12, 2003, 15:45
Default aeroengine intake at altitude
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In a 2d case of an aeroengine intake at altitude, with given pressure and temperature boundary conditions, Fluent predicts the density at altitude too low. I am using ideal gas with default air values of Cp etc. Does anyone know how to model altitude conditions correctly? Thanks, Friederike
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