Title
Air flow PXL geom 1st pass
Date
2008/04/14 17:39:18
1. File Report
Table 1 File Information for fatter flow 2_001
2. Mesh Report
Table 2 Mesh Information for fatter flow 2_001
3. Physics Report
Table 3 Domain Physics for fatter flow 2_001
Table 4 Boundary Physics for fatter flow 2_001
4. Solution Report
Table 5 Boundary Flows for fatter flow 2_001
5. User Data
Figure 1
Figure 2
Figure 3
Case | fatter flow 2_001 |
File Path | C:\Documents and Settings\Howard Wieman\My Documents\aps project\mechanical\PXL Flow CFX cooling\fatter flow\fatter flow 2_001.res |
File Date | 14 April 2008 |
File Time | 03:23:17 PM |
File Type | CFX5 |
File Version | 11.0 |
Fluids | Air at 25 C |
Solids | None |
Particles | None |
Domain | Nodes | Elements |
air | 235638 | 859674 |
Name | Location | Type | Materials | Models |
air | B356 | Fluid | Air at 25 C | Turbulence Model = k epsilon Turbulent Wall Functions = Scalable Buoyancy Model = Non Buoyant Domain Motion = Stationary |
Domain | Name | Location | Type | Settings |
air | inlet | inlet center, inlet left, inlet right | Inlet | Flow Regime = Subsonic Normal Speed = 4 [m s^-1] Mass And Momentum = Normal Speed Turbulence = Default Intensity and Autocompute Length Scale |
air | outlet | outlet | Outlet | Flow Regime = Subsonic Mass And Momentum = Average Static Pressure Relative Pressure = 0 [psi] Pressure Averaging = Average Over Whole Outlet |
air | symetry | air left sym, air right sym | Symmetry | |
air | air Default | F319.356, F320.356, F321.356, F323.356, F324.356, F3... | Wall | Wall Influence On Flow = No Slip Wall Roughness = Smooth Wall |
Location | Type | Mass Flow | Momentum | ||
X | Y | Z | |||
air Default | Boundary | 0.0000e+00 | 3.0427e-01 | -2.3776e-01 | -1.0448e-01 |
inlet | Boundary | 9.6958e-03 | -3.2668e-08 | 1.7887e-08 | 6.9774e-02 |
outlet | Boundary | -9.6956e-03 | 1.8753e-04 | -1.6900e-05 | 3.4980e-02 |
symetry | Boundary | 0.0000e+00 | -3.0441e-01 | 2.3775e-01 | -8.2120e-11 |
Figure 1. |
Figure 2. |
Figure 3. |