Date
2008/07/29 15:25:07
1. File Report
Table 1 File Information for 4 ladder inflated full path_001
2. Mesh Report
Table 2 Mesh Information for 4 ladder inflated full path_001
3. Physics Report
Table 3 Domain Physics for 4 ladder inflated full path_001
Table 4 Boundary Physics for 4 ladder inflated full path_001
4. User Data
Figure 1
Figure 2
Figure 3
Figure 4
5. Summary and conclusion
Case | 4 ladder inflated full path_001 |
File Path | C:\Documents and Settings\hhwieman\My Documents\aps project\mechanical\cfx pixel\longer 4 ladder clean\4 ladder inflated full path_001.res |
File Date | 29 July 2008 |
File Time | 02:53:12 PM |
File Type | CFX5 |
File Version | 11.0 |
Fluids | Air at 25 C |
Solids | c dummy,si dummy |
Particles | None |
Domain | Nodes | Elements |
air | 648129 | 2317271 |
carbon | 128885 | 580643 |
si 1 | 17944 | 76888 |
si 2 | 16932 | 72718 |
si 3 | 16221 | 68705 |
si 4 | 15588 | 66092 |
All Domains | 843699 | 3182317 |
Name | Location | Type | Materials | Models |
air | B176 | Fluid | Air at 25 C | Heat Transfer Model = Thermal Energy Turbulence Model = k epsilon Turbulent Wall Functions = Scalable Buoyancy Model = Non Buoyant Domain Motion = Stationary |
carbon | B174 | Solid | c dummy | Domain Motion = Stationary |
si 1 | B173 | Solid | si dummy | Domain Motion = Stationary |
si 2 | B178 | Solid | si dummy | Domain Motion = Stationary |
si 3 | B177 | Solid | si dummy | Domain Motion = Stationary |
si 4 | B175 | Solid | si dummy | Domain Motion = Stationary |
Domain | Name | Location | Type | Settings |
air | inlet | inlet | Inlet | Flow Regime = Subsonic Heat Transfer = Static Temperature Static Temperature = 23 [C] Normal Speed = 8 [m s^-1] Mass And Momentum = Normal Speed Turbulence = Medium Intensity and Eddy Viscosity Ratio |
air | Default Fluid Solid Interface in air Side 1 | F203.176, F201.176, F218.176, F183.176, F211.176, F1... | Interface | Heat Transfer = Conservative Interface Flux Wall Influence On Flow = No Slip Wall Roughness = Smooth Wall |
air | outlet | outlet | Opening | Flow Direction = Normal to Boundary Condition Flow Regime = Subsonic Opening Temperature = 23 [C] Heat Transfer = Opening Temperature Mass And Momentum = Opening Pressure and Direction Relative Pressure = 0 [Pa] Turbulence = Medium Intensity and Eddy Viscosity Ratio |
air | air Default | F155.176, F156.176, F157.176, F158.176, F159.176, F1... | Wall | Heat Transfer = Adiabatic Wall Influence On Flow = No Slip Wall Roughness = Smooth Wall |
carbon | Default Fluid Solid Interface in carbon Side 1 | F213.174, F214.174, F212.174, F150.174, F211.174, F2... | Interface | Heat Transfer = Conservative Interface Flux |
carbon | Default Solid Solid Interface in carbon Side 1 | F200.174, F194.174, F152.174, F187.174 | Interface | Heat Transfer = Conservative Interface Flux |
carbon | carbon Default | F208.174 | Wall | Heat Transfer = Adiabatic |
si 1 | Default Fluid Solid Interface in si 1 Side 2 | F204.173, F201.173, F203.173, F205.173, F206.173 | Interface | Heat Transfer = Conservative Interface Flux |
si 1 | Default Solid Solid Interface in si 1 Side 2 | F152.173 | Interface | Heat Transfer = Conservative Interface Flux |
si 1 | si 1 Default | F202.173 | Wall | Heat Transfer = Adiabatic |
si 2 | Default Fluid Solid Interface in si 2 Side 1 | F199.178, F182.178, F197.178, F198.178, F195.178 | Interface | Heat Transfer = Conservative Interface Flux |
si 2 | Default Solid Solid Interface in si 2 Side 2 | F200.178 | Interface | Heat Transfer = Conservative Interface Flux |
si 2 | si 2 Default | F196.178 | Wall | Heat Transfer = Adiabatic |
si 3 | Default Fluid Solid Interface in si 3 Side 2 | F189.177, F191.177, F193.177, F180.177, F192.177 | Interface | Heat Transfer = Conservative Interface Flux |
si 3 | Default Solid Solid Interface in si 3 Side 2 | F194.177 | Interface | Heat Transfer = Conservative Interface Flux |
si 3 | si 3 Default | F190.177 | Wall | Heat Transfer = Adiabatic |
si 4 | Default Fluid Solid Interface in si 4 Side 2 | F183.175, F186.175, F185.175, F188.175, F179.175 | Interface | Heat Transfer = Conservative Interface Flux |
si 4 | Default Solid Solid Interface in si 4 Side 2 | F187.175 | Interface | Heat Transfer = Conservative Interface Flux |
si 4 | si 4 Default | F184.175 | Wall | Heat Transfer = Adiabatic |
Figure 1. |
Figure 2. |
Figure 3. |
Figure 4. |
C:\Documents and Settings\hhwieman\My Documents\aps project\mechanical\cfx pixel\longer 4 ladder clean\4 ladder inflated full path_001.res
Inflated mesh with full return path opening
12 deg Temperature rise.
This is less than the similar run 16 deg without inflated mesh, but this also has the correct si conductivity this time, so not yet know what was important for the change.
Input velocity 8 m/s
Exhaust velocity 9 m/s in center of path
Fig. 1 Silicon surface temperature
Fig. 2 Air velocity contours on selected surfaces
Fig. 3 Temperature contour near exit/entrance
Fig. 4 A flow stream lines, colors show velocity