|December 20, 2010, 14:44||
Join Date: Dec 2010
Posts: 23Rep Power: 8
im new on this forum, im actually working on my individual project where im using GAMBIT to create my mesh around a NACA 0015. ive got my coordinates and arranged it as its said in a tutorial , but after importing the airfoil does not come out properly!!!could someone plz help me out, i would really appreciate....
Attachments for my workings
Last edited by ACER; December 20, 2010 at 18:14.
|December 21, 2010, 04:37||
Join Date: Mar 2009
Posts: 3,186Rep Power: 33
I don't how it works for defining direct your surface, but as you get not so many points you can afford you to create the naca airfoil manually.
*Import the vertex data
*create all edges defining the airfoil by linking points (couple of points)
*if all the points disturb you, you can merge all the edges into one.
*finally creat a surface (wireframe) by choosing the upper and lower edges
In memory of my friend Hervé: CFD engineer & freerider
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