ICEM Wing Mesh Problem -- CFD Online Discussion Forums

March 4, 2018, 18:30

ICEM Wing Mesh Problem

andrewmichael

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Bota Amdrei

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Hello everybody,

I tried to create the mesh for a wing having the aerofoil NACA23015 and my wing has round trailing edge. I cannot create the mesh at the wing tip ( see attached pictures). Thus, somehow at the walls of the domain, ICEM computed them I must say that my wing does not have a sharp trailing edge.

Does someone help me with this problem ?

Kind regards,
Andrei

Attached Images

	2018-03-04_22h21_28.jpg (95.9 KB, 15 views)
	2018-03-04_22h19_26.jpg (171.0 KB, 13 views)
	2018-03-04_22h17_22.jpg (177.7 KB, 10 views)

Last edited by andrewmichael; March 8, 2018 at 07:15.

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