Date

2008/06/27 18:27:04

Contents

1. File Report
    Table 1  File Information for TopLeoCFXsym1_001
2. Mesh Report
    Table 2  Mesh Information for TopLeoCFXsym1_001
3. Physics Report
    Table 3  Domain Physics for TopLeoCFXsym1_001
    Table 4  Boundary Physics for TopLeoCFXsym1_001
4. User Data
    Figure 1
    Figure 2
    Figure 3

1. File Report

**Table 1.** File Information for TopLeoCFXsym1_001
Case	TopLeoCFXsym1_001
File Path	C:\Documents and Settings\hhwieman\My Documents\aps project\mechanical\cfx pixel\Leo Thermal Ladder sym\TopLeoCFXsym1_001.res
File Date	27 June 2008
File Time	06:16:06 PM
File Type	CFX5
File Version	11.0
Fluids	Air at 25 C
Solids	c dummy,si dummy
Particles	None

2. Mesh Report

**Table 2.** Mesh Information for TopLeoCFXsym1_001
Domain	Nodes	Elements
air	4237	10807
c	432	894
si	240	509
All Domains	4909	12210

3. Physics Report

**Table 3.** Domain Physics for TopLeoCFXsym1_001
Name	Location	Type	Materials	Models
air	B39	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
c	B40	Solid	c dummy	Domain Motion = Stationary
si	B41	Solid	si dummy	Domain Motion = Stationary

**Table 4.** Boundary Physics for TopLeoCFXsym1_001
Domain	Name	Location	Type	Settings
air	inlet	inlet	Inlet	Flow Regime = Subsonic Heat Transfer = Static Temperature Static Temperature = 23 [C] Normal Speed = 1 [m s^-1] Mass And Momentum = Normal Speed Turbulence = Medium Intensity and Eddy Viscosity Ratio
air	Default Fluid Solid Interface in air Side 1	F50.39, F42.39, F53.39, F51.39, F44.39, F46.39, F52.3...	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 sym	air sym	Symmetry
air	air Default	F54.39, F55.39, F57.39	Wall	Heat Transfer = Adiabatic Wall Influence On Flow = No Slip Wall Roughness = Smooth Wall
c	Default Fluid Solid Interface in c Side 1	F44.40, F42.40, F47.40, F46.40, F43.40	Interface	Heat Transfer = Conservative Interface Flux
c	Default Solid Solid Interface Side 1	F49.40	Interface	Heat Transfer = Conservative Interface Flux
c	c sym	c cym	Symmetry
si	Default Fluid Solid Interface in si Side 2	F51.41, F52.41, F50.41, F53.41	Interface	Heat Transfer = Conservative Interface Flux
si	Default Solid Solid Interface Side 2	F49.41	Interface	Heat Transfer = Conservative Interface Flux
si	si sym	si sym	Symmetry

4. User Data

Figure 1.

Figure 1 - ReportTopLeoCFXsym1001/Figure001.png

Figure 2.

Figure 2 - ReportTopLeoCFXsym1001/Figure002.png

Figure 3.

Figure 3 - ReportTopLeoCFXsym1001/Figure003.png