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Old   November 5, 2013, 05:12
Default Characteristic length
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Hi all,

I am trying to simulate flow over an aircraft that has an external storage.

I would like to estimate the drag on the external storage.

What should be my characteristic length to calculate the Re and hence the near wall node spacing? and why?

Can anyone help me out pl.

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Studentdrak
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Old   November 5, 2013, 16:17
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Jim KIT
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Hi,
please correct me, when I am wrong.
you can choose any lenght for your problem as charactristic length.
But If you want to know if flow is turbulent or laminar can u estimate it from flow over a flat plane Re(x) = 5 e5, where x is the distance from the leading edge of the flat plate.
(you should know that cfx doesnt simulate Transition)
How fine should be the meh near the wall can you estimate from y+:
Simulate your case and see the y+ term in Post.
Or you may estimate Cf frome a flat plane and calculate shear stress on Wand. and thus, takking to account that y+ should be smaller than 1, you can find your y (wall node spacing).

However you have take to the account that RANS use wall function and you must not have y<1 you can have y to 5 or 10.

Vile Grüße,
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Old   November 5, 2013, 17:12
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Glenn Horrocks
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As a starting point the length scale should be the chord of the wing. But then do a sensitivity analysis on your mesh to check if your starting point was correct or not.
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