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Fluent Airfoil Analysis: Fixed CL mode

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Old   February 28, 2017, 05:25
Default Fluent Airfoil Analysis: Fixed CL mode
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I've performed some analyses on supercritical airfoils with the code SU2; I used the 'FIXED_CL_MODE' of Su2, to evaluate the behaviour of the airfoils at different Mach conditions, fixing the target CL (useful to evaluate de Drag Rise condition and the influence of the lift coefficient on transonic performances).

I want to realize the same analysis in Fluent, but I don't know if is it possible to perform a FIXED CL calculation in Fluent. Is there a way (not only a direct command but also a script) to fix the target CL before performing a 2D calculation in Fluent?

Thank You!
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airfoil, fixed cl, fluent, transonic

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