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December 20, 2010, 13:44 |
Airfoil plotting....
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#1 |
New Member
abishai murday
Join Date: Dec 2010
Posts: 23
Rep Power: 15 |
hi everyone
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 thank you gambit.jpg NNaca0015 ori.dat.txt Last edited by ACER; December 20, 2010 at 17:14. |
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December 21, 2010, 03:37 |
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#2 |
Super Moderator
Maxime Perelli
Join Date: Mar 2009
Location: Switzerland
Posts: 3,297
Rep Power: 41 |
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
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In memory of my friend Hervé: CFD engineer & freerider |
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