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Objective:- Perform Computational analysis for the Cold plate and also create the non-conformal mesh for the model. TASK Create non-conformal mesh assembly. Solve for Flow and Temperature model & choose zero equation turbulent model and setup gravity vector. Setup transient simulation with an initial velocity…
Arun Gupta
updated on 14 May 2022
Objective:- Perform Computational analysis for the Cold plate and also create the non-conformal mesh for the model.
TASK
Steps for Performing Analysis
1. Cabinet
The “Cabinet” is said to define the flow domain of interest in Icepak but it may not be the case with every geometry that the fluid domain is simply a cuboid that can be realized just merely by resizing the cabinet.
i) Geometry Shape - Prism.
Specified By - Start/end.
ii) Properties - The wall type for the cabinet is defined.
2. Geometry Solid-Block
Shape - Prism.
Specified By - Start/end.
ii) Properties
3 Geometry - Fluid Domain
Shape - Prism.
Specified By - Start/end.
ii) Properties
4. Geometry - Heated Plate 1
Shape - Rectangular.
Plane - X-Y.
Specified By - Start/end.
ii) Properties
5. Geometry - Heated Plate 2
Shape - Rectangular.
Plane - X-Y.
Specified By - Start/end.
ii) Properties
6 Geometry - Inlet Pipe
Shape - Cylinder.
Plane - X-Z.
ii) Properties
7 Geometry - Outlet Pipe
Shape - Cylinder.
Plane - X-Z.
ii) Properties
8 Geometry - Inlet Fluid region
Shape - Cylinder.
Plane - X-Z.
ii) Properties
9 Geometry - Outlet Fluid region
Shape - Cylinder.
Plane - X-Z.
ii) Properties
10 Boundary - Inlet Opening
Shape - Cylinder.
Plane - X-Z.
ii) Properties
10 Boundary - Outlet Opening
Shape - Cylinder.
Plane - X-Z.
ii) Properties
11 Final Model
Meshing
A. Assemble - 1 Inlet
Select inlet pipe, inlet fluid region, and inlet opening create --> assembly.
Under the meshing tab choose Mesh separately,
i) Slack setting
ii) Mesh type
B. Assemble - 2 Outlet
Select outlet pipe, outlet fluid region, and outlet opening create --> assembly.
Under the meshing tab choose Mesh separately,
i) Slack setting
ii) Mesh type
C Assemble - 3 - Complete Domain
Select solid block, Fluid Block, heated plate 1,heated plate 2, assemble 1 & assemble 2, create --> assemble.
Under the meshing tab choose Mesh separately,
i) Slack setting
ii) Mesh type
Model Check
Macros --> Productivity --> Validation --> Automatic case check tool - It checks the assembly interface between the various objects and assembly.
Mesh Control
ii) Mesh type - Mesher -HD
Mesh View - X Plane
Mesh View - Y Plane
Mesh View - Z Plane
Mesh Verification
Face alignment
Volume
Skewness
Monitor Points
Solver
The three-dimensional steady-state Navier stokes equations for the model are solved within the computational domain.
General Setup
The default value of the parameters is set to default.
Basic settings
Parallel Settings
Advance Solver Setup
Residuals
the residual measures the local imbalance of a conserved variable in each control volume. Therefore, every cell in your model will have its own residual value for each of the equations being solved. In an iterative numerical solution, the residual will never be exactly zero. The residuals for the following equations are plotted against the number of iterations:
Solution
Post-Processing
Temperature Contours
Velocity Contours
Conclusion
In this project, the given model of the cold plate was meshed using ANSYS Icepak using the non-conformal meshing, per-object meshing parameters, and multi-level meshing. The three-dimensional steady-state governing equations for the model were solved for flow and temperature within the computational domain in the Icepak.
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