|
[Sponsors] |
September 7, 2005, 18:21 |
How can I get Cp=1 at the stagnation point ?
|
#1 |
Guest
Posts: n/a
|
From the flow around a circular cylinder, the pressure coefficient around stagnation area is not 1. As my understanding, it should be 1. Please let me know how to calculate the pressure coefficient from the FLUENT simulation.
I tried to change reference values but it seems not working. |
|
September 7, 2005, 19:03 |
Re: How can I get Cp=1 at the stagnation point ?
|
#2 |
Guest
Posts: n/a
|
The value you would be getting is higher than 1, when you refine the mesh near wall, the CP gets to correct values. I use the mesh with yplus less than one, then i get max Cp around 1.05, and the CP values match experimental values.
|
|
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
block-structured mesh for t-junction | Robert@cfd | ANSYS Meshing & Geometry | 20 | November 11, 2011 05:59 |
NO STAGNATION POINT FOR AIRFOIL SIMULATION | Rif | Main CFD Forum | 6 | February 4, 2008 08:33 |
[Gmsh] Gmsh and samplesurface | touf | OpenFOAM Meshing & Mesh Conversion | 2 | December 10, 2007 03:27 |
Stagnation point and other issues | Freeman | FLUENT | 0 | December 12, 2005 16:16 |
CFX4.3 -build analysis form | Chie Min | CFX | 5 | July 13, 2001 00:19 |