# Actuator disk model

The actuator disk model in Flow360 provides a simplified representation of a propulsor using a momentum source term distributed across a disk-shaped region.

# Available Parameters

Parameter	Description
Assigned volumes	Cylinder entities defining disk location and dimensions
Unit	Choose units used for actuator disk definition
File upload	Upload a file defining the actuator disk

# Detailed Descriptions

# Assigned volumes

The cylinder entities that define the location and dimensions of the disk. The cylinder's center, axis, height, and outer radius are used as the actuator disk's center, thrust axis, thickness, and radius respectively.

Required

Notes:

The cylinder axis defines the direction of the thrust

Ensure the cylinder is sized appropriately for your application

# Unit

Specifies units of the values specified in the uploaded file.

Required

Notes:

Arrays for radius, thrust, and circumferential must all have the same length

Positive thrust means the axial force follows the same direction as the thrust axis

Positive circumferential force follows the same direction as the thrust axis with the right hand rule

In the GUI, you can either input values directly or upload JSON/CSV files with the distribution data

# File upload

A window for uploading a file defining the behaviour of the actuator disk.

Options:

CSV Format

CSV files can be uploaded with or without headers. If headers are present, they must be: radius, thrust, circumferential

Example with headers:
```
radius, thrust, circumferential
0, 1, 0 
1, 2, 20
10, 1, 1
```
Example without headers:
```
0, 1, 0 
1, 2, 20
10, 1, 1
```

JSON Format

{
    "force_per_area": {
        "radius": [0, 1, 10],
        "thrust": [1, 2, 1],
        "circumferential": [0, 20, 1]
    }
}

💡 Tips

# When to Use Actuator Disk Model

For propellers or fans where detailed blade modeling is unnecessary
In preliminary design studies requiring quick turnaround
When only the thrust and torque effects matter, not detailed wake structures
For wind turbine analysis where detailed blade aerodynamics are less important
In applications where the general influence of a propulsor on flow is needed, but not blade-specific phenomena

# Comparison with BET Disk Model

Feature	Actuator Disk	BET Disk
Complexity	Lower	Higher
Setup Time	Fast	Moderate
Computational Cost	Lower	Higher
Accuracy	Basic	More detailed
Wake Prediction	General structure	Blade-specific effects
Required Inputs	Thrust/pressure	Detailed blade geometry

# Common Applications

Propeller/Fan Simulation: Aircraft propulsion, marine propulsors, cooling fans, HVAC systems
Wind Turbine Analysis: Single turbine performance estimation, wind farm wake interactions, site assessment studies
General Flow Control: Modeling jet fans in tunnels, representing flow accelerators, simplified representation of thrust-producing devices

# Implementation Tips

Consider upgrading to BET Disk for more accurate wake prediction
Ensure adequate mesh resolution around the disk
- Typically 10-20 cells across the disk radius
- Maintain refined mesh downstream to capture wake development
Start with uniform loading for initial studies
Base thrust and pressure values on experimental or analytical data when possible
For accurate flow-field predictions, include swirl effects

# Limitations

Cannot capture blade-specific effects
Simplified wake structure
No inherent modeling of performance variation with flow conditions
Less accurate than BET Disk or fully-resolved blade simulations
May oversimplify flow-field effects in cases with complex inflow conditions

❓ Frequently Asked Questions

When should I use Actuator Disk instead of BET Disk?

Use Actuator Disk for preliminary design studies requiring quick turnaround, cases where detailed wake structures aren't needed, or applications where only the thrust and torque effects matter. Use BET Disk when blade-specific aerodynamics are important.
How do I determine appropriate thrust values?

Thrust values can be determined from experimental data, analytical calculations, or known performance metrics of your propulsor. Typically, you'd convert a known thrust to a pressure by dividing by the disk area.
Can I model non-uniform loading?

Yes, by specifying different thrust values across the radial positions, you can create custom radial distributions to model tip effects or other non-uniform loading patterns.
Does the actuator disk model capture tip vortices?

Not directly. The model produces a simplified wake structure without capturing detailed blade-specific phenomena like tip vortices. For those effects, consider the BET Disk model or fully-resolved blade simulations.
How does this model handle different flow conditions?

The model applies the specified force distribution regardless of inflow conditions. It doesn't inherently account for performance variations with flow speed or angle. You would need to manually update the force distribution for different operating conditions.
Can I use this model for contra-rotating propellers?

Yes, by creating two actuator disk models with opposite swirl directions, positioned in sequence along the flow path.
How do I import data from existing propeller analysis?

You can prepare your data in CSV or JSON format and upload it through the GUI. This is useful when you have force distributions from other analysis tools or experimental data.

🐍 Python Example Usage

Below is an example of how to configure an Actuator Disk model using the Flow360 Python API:

# Example (for reference only, not included in GUI documentation)
actuator_disk = fl.ActuatorDisk(
    entities = fl.Cylinder(
        name="actuator_disk",
        center=(0,0,0)*fl.u.mm,
        axis=(-1,0,0),
        height = 30 * fl.u.mm,
        outer_radius=5.0 * fl.u.mm,
    ),
    force_per_area = fl.ForcePerArea(
        radius=[0, 1] * fl.u.mm,
        thrust=[4.1, 5.5] * fl.u.Pa,
        circumferential=[4.1, 5.5] * fl.u.Pa,
    )
)

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