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Search: Posts Made By: zhongyu
Forum: Main CFD Forum February 25, 2011, 04:18
Replies: 18
Views: 7,756
Posted By zhongyu
Yes, Martin, That is good idea, I think I will...

Yes, Martin, That is good idea, I think I will try today!
Forum: Main CFD Forum February 25, 2011, 04:17
Replies: 18
Views: 7,756
Posted By zhongyu
Thank you, can you tell me if it is work after...

Thank you, can you tell me if it is work after your try.

I did not attach the code, only write it in the FORTRAN. and I checked a few times, it seems I write it excatly the same as that book...
Forum: Main CFD Forum February 24, 2011, 14:02
Replies: 18
Views: 7,756
Posted By zhongyu
The problem is I put all code in FORTRAN, but it...

The problem is I put all code in FORTRAN, but it says floating point error, invalid!
Forum: Main CFD Forum February 24, 2011, 10:27
Replies: 18
Views: 7,756
Posted By zhongyu
Thanks Martin, Yes, my research is only...

Thanks Martin,

Yes, my research is only focus on the low order panel method and incompressible flow, this code is what I will used as hydrofoil which sailing in the water, so I think subsonic in...
Forum: Main CFD Forum February 24, 2011, 08:40
Replies: 18
Views: 7,756
Posted By zhongyu
Lol, u mean the programming 14 in appendix works?...

Lol, u mean the programming 14 in appendix works? have u tried about that? cause I write it all down in FORTRAN, but it seems doesn't work, is it the publish problem?

I am agree with u that the...
Forum: Main CFD Forum February 24, 2011, 04:11
Replies: 18
Views: 7,756
Posted By zhongyu
Hi, Do Thank you very much for your help! ...

Hi, Do

Thank you very much for your help!

I have checked the two information u provided, the first one I think is software, but now I am trying to make the FORTRAN programming, but I think it...
Forum: Main CFD Forum February 22, 2011, 13:58
Replies: 18
Views: 7,756
Posted By zhongyu
Help! 3d hess smith panel method

Dear all :):

I am doing the research of numerical investigation about the potential flow around hydrofoil.

I use Hess and Smith panel method as my basic method (airfoil), I have finished 2D...
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