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Search: Posts Made By: Fly
Forum: Pointwise & Gridgen April 19, 2014, 00:16
Replies: 14
Views: 5,696
Posted By Fly
Hi andromeda, Sorry for the late reply. Have...

Hi andromeda,

Sorry for the late reply. Have you solved the problem now?
Forum: Pointwise & Gridgen October 19, 2013, 23:50
Replies: 14
Views: 5,696
Posted By Fly
Thank you for your reply. It is straightforward...

Thank you for your reply. It is straightforward and simple to understand.

I am sorry that I did not make it clear about the last sentence in the last message. I mean that I want the length from...
Forum: Pointwise & Gridgen October 19, 2013, 23:27
Replies: 14
Views: 5,696
Posted By Fly
Thanks, Taxalian. Yes, my growth rate is...

Thanks, Taxalian.

Yes, my growth rate is about 1.1. There is about 240 points on the airfoil and the first step size is 4.0e-4 (the chord length is 1).

I followed your instruction but I can...
Forum: Pointwise & Gridgen October 19, 2013, 06:39
Replies: 14
Views: 5,696
Posted By Fly
Hi Chrish, I tried your idea and it does...

Hi Chrish,

I tried your idea and it does work to improve the mesh. The attachment is my best result.

I have no idea about the meaning of volume smoothing parameter even after I read the...
Forum: Pointwise & Gridgen October 18, 2013, 09:18
Replies: 14
Views: 5,696
Posted By Fly
Hi, Taxalian, Thank you so much for your...

Hi, Taxalian,

Thank you so much for your suggestion. The mesh is so great in your picture.

I tried your way, but the extrusion will stop after some steps, my result is attached.

I am...
Forum: Pointwise & Gridgen October 18, 2013, 00:00
Replies: 14
Views: 5,696
Posted By Fly
Hi Chris, Thank you very much for your...

Hi Chris,

Thank you very much for your reply.

I tried your suggestion, but the problem is not solved. When it runs about 50 steps, it crashed. I think it is because the extrusion interval at...
Forum: Pointwise & Gridgen October 17, 2013, 09:37
Replies: 14
Views: 5,696
Posted By Fly
Smile Generate a c topology mesh of an airfoil

Dear all,

I want to a c type mesh around airfoil NACA 0012. I am a new user of Pointwise and I think my application is something wrong. The followings are my steps:

1. import the airfoil...
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