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Spanwise lift distribution on 3D wing

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Old   August 26, 2007, 09:23
Default Spanwise lift distribution on 3D wing
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I'm currently using Fluent and I'd like to carry out a spanwise lift analysis.

But the only thing I manage to do is a Cp analysis along the wing... (using the XY plot function). By any chance, is there a function to plot Cl in function of the spanwise location ?

Sorry, it's seem basics function, I obviously had a look at the user manual and other tutorials, but I haven't find anything !!!

Thanks for your help

Best regards

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Old   August 26, 2007, 21:39
Default Re: Spanwise lift distribution on 3D wing
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please help me, I do need this lift distribution in order to end my MSc thesis ....

Thanks for any kind of help

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