Project

Conjugate Heat Transfer Analysis on a graphics card

Objective:

Here we are performing conjugate heat transfer analysis for graphic card.Here graphic card is divided into three components namely Core,Base and Fins. Core and fins are placed above base. Here core is the source where heat is generated while operating a PC or a computer. Core need to be cooled inorder for PC working seamlessly, So fins are used to do the work of cooling.Fins has more surface are when the air is blown over the fin due to large surface aresa the core is cooled much faster here we are trying to find out whta would be the temperature distrubution and velocity distrubution and how well the core is cooled and max temperature attained by the core

Case I

Geomentry

Graphic Card

Naming the components we are focusing in Graphic card

Shared tropology to enbling conduction between fins and base

Meshing:

Base line mesh

Element Size:1.0289e-002

Nodes:15776

Elements:84296

Steady state conjugate heat transfer analysis on a model of a graphics card

Setup

General

Steady state,Pressure based Model,Axisymmentric

Models

Energy --> Viscous -->K-Epsilon -->Standard -->Standard Wall Function

Boundary Conditions

Air-Inlet:10m/sec

Material

Core-Gold(Source term added to this) if power of core is 15W then the energy will be 15/64*1e-9=234375000 Base-Alluminium

Fins-Copper

Here we have only one inlet so we can use standard initialiation with inlet as the compute zone

Iterations-600

Results

Average weighted Temperature

Average weighted Velocity

The above graphs helps us to underastand that solution has converged

Temperature Contour

Velocity Contour

Heat Transfer Coefficient Contour

Temperature Volume rendering

Case II

Fine Mesh

element size:5e-003

Nodes:33233

Elements:183153

Unlike base line mesh here the element size is reduced along with that proximity capture has been enabled to capture more and accurate data at the walls of graphic card

Setup

General

Steady state,Pressure based Model,Axisymmentric

Models

Energy --> Viscous -->K-Epsilon -->Standard -->Standard Wall Function

Boundary Conditions

Air-Inlet:10m/sec

Material

Core-Gold(Source term added to this) if power of core is 15W then the energy will be 15/64*1e-9=234375000 Base-Alluminium

Fins-Copper

Here we have only one inlet so we can use standard initialiation with inlet as the compute zone

Iterations-600

Results

Residuals

Average weighted Temperature

Average weighted Velocity

The above graphs helps us to underastand that solution has converged

Temperature Contour

Velocity Contour

Heat Transfer Coeffient contour

Temperature Volume rendering

Variables Base Line Mesh Fine Mesh Units
Core Temperture 360.2 354.8 K
Velocity 11.92 11.76 m/sec
Heat transfer coefficient 953.4 939.5 W/m2K

As we can see that there is a huge variation in values between base line mesh and fine mesh so mesh is an important attribute for obtaining a perfect solution.

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