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

Applicable

Assigned volumes

Cylinder entities defining disk location and dimensions

always

Unit

Choose units used for actuator disk definition

always

Input method

Choose how to define the loading: upload a distribution file or specify a uniform value

always

File upload

Upload a file defining the actuator disk

Input method is Upload file

Inner radius

Inner radius of the region over which the loading is applied (set to 0 to load the full disk)

Input method is Uniform

Outer radius

Outer radius of the region over which the loading is applied

Input method is Uniform

Force per area value

Constant thrust force per unit area applied between the inner and outer radius

Input method is Uniform

Reference velocity

Optional reference velocity vector [Vx, Vy, Vz] for power output calculation

always


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

Input method#

Selects how the disk loading is defined. Two options are available:

  • Upload file (default): import a radial distribution of radius, thrust, and circumferential values from a JSON or CSV file (see File upload below).

  • Uniform: specify a single force-per-area value applied uniformly between an Inner radius and an Outer radius, with no circumferential (swirl) component. The setup form prompts you with: “Specify a uniform force-per-area value across the disk (no swirl).”

Notes:

  • The Uniform option is the quickest way to set up a constant-loading disk when a detailed radial distribution is not needed.

  • For the uniform input, the radii use the Radius unit and the loading uses the Force per area unit selected under Unit above.

  • Because there is no swirl, the integrated Torque of a uniform disk is zero (see Integrated values).

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]
          }
      }
      

Inner radius#

Inner radius of the region over which the uniform loading is applied. Set to 0 to load the full disk.

  • Required when Input method is Uniform.

Outer radius#

Outer radius of the region over which the uniform loading is applied.

  • Required when Input method is Uniform.

Force per area value#

Constant thrust force per unit area applied uniformly between the inner and outer radius, with no circumferential (swirl) component.

  • Required when Input method is Uniform.

Notes:

  • Uses the Force per area unit selected under Unit.

Reference velocity#

An optional velocity vector [Vx, Vy, Vz] used as the reference velocity for actuator disk power output calculations.

  • Optional (default: not set)

  • When provided, the solver uses this fixed velocity vector instead of the local flow velocity when computing the actuator disk power output.


Integrated values#

A live readout displayed in the setup form once a valid loading is defined. Flow360 integrates the force-per-area distribution over the disk so you can sanity-check the total loading before running the case.

Value

Description

Thrust

Total axial thrust, obtained by integrating the thrust (axial) force-per-area over the disk area

Torque

Total torque, obtained by integrating the circumferential (swirl) force-per-area over the disk

  • The values update automatically as you edit the loading, whether it comes from an uploaded file or from the uniform input.

Notes:

  • The readout is computed in the browser for quick feedback during setup; the solver performs its own integration at run time.

  • The Torque reflects only the circumferential (swirl) loading, so it is zero for a uniform disk or for any distribution with no circumferential component.

  • The values use units derived from the selected Radius and Force per area units.


💡 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

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

See also

Python API reference: ActuatorDisk, Cylinder and ForcePerArea.

For a worked example, see DARPA SUBOFF Actuator Disk.

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,
    ),
    # Optional: fix the reference velocity used for power output calculations.
    # Useful for hover or near-zero freestream cases.
    reference_velocity=[0, 0, -10] * fl.u.m / fl.u.s,
)