Air enters the enclosure from the environment, passes through the device, and is exhausted to the environment. In most applications a fan moves the air, and the incoming air temperature is known. Buoyancy effects are negligible. Heat dissipated by the components is convected away by moving air and conducted through the enclosure. Radiation is typically negligible for these applications.
Application Examples
Projector
Computing hardware
Lab equipment
Telecommunications devices
Data center equipment
Modeling Strategy
Materials
Boundary Conditions
There are several possible combinations of flow boundary conditions. Select the combination that best matches the device:
Known inlet flow
Known outlet flow
Known Pressure Drop
Known Internal Fan
Heat transfer boundary conditions should always be applied if the objective is to learn the temperature distribution. (These can be omitted if the objective is to assess only the flow.)
Apply a Temperature boundary condition to all openings in which air enters the device. Do not apply a temperature to outlets.
Apply a Total Heat Generation boundary condition on components that dissipate heat. Note that power is evenly dissipated over the entire volume.
To simulate heat transfer to the surroundings, apply a Film Coefficient boundary condition to the external surfaces. The value depends on the air that surrounds the physical device:
Mesh
A basic guideline for a high-quality analysis model is that the mesh distribution be sufficient to resolve the flow and temperature gradients efficiently. In regions where the flow circulates or experiences large gradients (such as in wakes, vortices, and separation regions), a finer mesh is required.
For most models, use Automatic Sizing to define the mesh distribution. It may be necessary to locally refine the mesh on geometric features that are highly detailed. For more information about Mesh Autosizing and model preparation...
In some cases, it may be necessary to adjust the Minimum Refinement Length to reduce their effect on the overall mesh count.
To locally refine the mesh in high-gradient flow regions:
Running
On the Physics tab of the Solve dialog:
Flow = On
Heat Transfer = On
Automatic Forced Convection = On
Turbulence:
Autodesk® CFD stops the solution either when the specified number of iterations have elapsed or when the solution is converged, whichever comes first. To ensure the analysis is not stopped before converging, set the Iterations to Run to 500. Most analyses converge within 200-300 iterations so 500 should provide an adequate margin.
Flow Distribution
Component Temperatures
For more general information, use the extensive collection of results visualization tools to extract flow and thermal results.
Troubleshooting
Oscillating convergence, as shown by a "saw tooth" convergence plot, is a problem that occasionally occurs when internal fans are defined with a fan curve:
This is caused when the operating point of the system varies significantly from one iteration to the next, and the operating point on the fan curve varies with it. The intersection of the fan curve and the system curve is the operating curve of the fan. If the solution changes too rapidly from one iteration to the next, this point develops a repeating overshoot/undershoot, and the "saw tooth" convergence plot is the result.
To fix this issue:
This change slows the solution of the velocity and pressure variables, and prevents the operating point from varying do dramatically:
Things to Avoid