CFD Online Discussion Forums

CFD Online Discussion Forums (https://www.cfd-online.com/Forums/)
-   Main CFD Forum (https://www.cfd-online.com/Forums/main/)
-   -   Navier stokes and maxwell slip boundary (https://www.cfd-online.com/Forums/main/121141-navier-stokes-maxwell-slip-boundary.html)

archeoptyrx August 3, 2013 01:43

Mr.Alex,

The boundary conditions look correct in the way you said . May be the Maccormack method which i wrote is responsible for the errors i guess. Have you tried implementing this with the navier stokes ? . If so could you check on my entire code ?

flotus1 August 3, 2013 02:38

For NS, i only have a small 1-dimensional (+incompressible +isothermal) code with finite differences.
I guess you will have to go the usual way by debugging your code step by step.

archeoptyrx August 5, 2013 13:29

Thanks for the help Alex . I will start debug my code and find out any errors that prevents me to go further .

archeoptyrx August 20, 2013 17:52

Quote:

Originally Posted by flotus1 (Post 443587)
For NS, i only have a small 1-dimensional (+incompressible +isothermal) code with finite differences.
I guess you will have to go the usual way by debugging your code step by step.

Mr.Alex ,

I recently found that my code over predicts the results . Could you help me with this ? . I dont know what is wrong with this . The results for no slip condition too is over predicted for certain plots .

thanks in advance

flotus1 August 21, 2013 02:26

When you say your results are over-predicted, what exactly do you mean?

archeoptyrx August 21, 2013 02:29

I get exactly same graphs as in t book . but slight variation in t peak values . For example , p/pinf =1.45 (from book) , p/ping=1.6 (from my code)

archeoptyrx October 13, 2013 23:46

1 Attachment(s)
Quote:

Originally Posted by flotus1 (Post 443587)
For NS, i only have a small 1-dimensional (+incompressible +isothermal) code with finite differences.
I guess you will have to go the usual way by debugging your code step by step.

Mr Alex ,

This is the temperature plot i got for Kn=0.0156 . But when i tried the same method with kn=0.0723 . It just blows away giving complex numbers . after 7 steps. But actually this range of knudsen number falls into slip regime right ? The input conditions are as follows

Alt=10km

Pinf=2.65e4;
T=223.2625;
Kn=0.0156

Alt=20km
Pinf=5.523e3;
T=216.65
kn=0.0723


All times are GMT -4. The time now is 10:48.