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Introduction
Capabilities
Quick Start
Introduction to the Flow360 WebUI
Automated Meshing with the WebUI
Launching a case with the WebUI
Postprocessing a case with the WebUI
Flow360 API Quickstart
User Guide
How Does It Work?
Workflows & Interfaces
Asset Drafts
Meshing
Output Configuration
Run Control
Units & Expressions
Units
User Defined Expressions
Legacy User Defined Expressions
Non-Dimensionalization
Introduction
Non-Dimensional Inputs
Non-Dimensional Outputs
Force and Moment Coefficients
Troubleshooting
Error when calculating patch interpolation coefficients
Fixing Divergence Issues
User Defined Dynamics
Report
GUI
Introduction
Dashboard
Starting Project
Workbench Layout
Top Bar
Viewer Region
Status Bar
General Workflow in Flow360 GUI
Project Tree
Keyboard Shortcuts
Project Settings
Simulation Setup
Operating condition
Mesh
Farfield
Mesh parameters
Rotation regions
Custom zones
Volume mesh slices
Refinements
Surface Edge Refinement
Surface Refinement
Boundary Layer Refinement
Passive Spacing
Uniform Refinement
Axisymmetric Refinement
Geometry Refinement
Flow solver
Boundary Conditions
Wall Boundary Condition
Freestream Boundary Condition
Inflow Boundary Condition
Outflow Boundary Condition
Periodic Boundary Condition
Symmetry Boundary Condition
Slip Wall Boundary Condition
Porous Jump Boundary Condition
Turbulence Quantities
Time Stepping
Physics
Fluid model
Solid model
Rotation model
BET disk model
Actuator disk model
Porous medium model
User-defined dynamics
Output
Reference Dimensions
Outputs List
Volume Output
Time-averaging Volume Output
Surface Output
Time-averaging Surface Output
Slice Output
Time-averaging Slice Output
Probe Outputs
Time-averaging Probe Outputs
Surface Probe Outputs
Surface Slice Output [Python only]
Surface Integral Output
Isosurface Output
Time-averaging Isosurface Output
Aeroacoustic Output
Streamline Output
Time-averaging Streamline Output
Force Output
Force Distribution Output
Time-averaging Force Distribution Output
Output Formats
Available Output Fields
Scaling Values and Nondimensionalization
Analysis
Dashboard
Convergence Monitoring in Flow360
Monitor
Visualization
Aeroacoustic Interface
Entities browser
Geometry
Edges
Faces
Surface Mesh
Volume Mesh
Zones
Boundaries
Volumes
Box
Cylinder
Sphere
Axisymmetric volume
Custom volume
Points
Slices
Sample Surfaces
Derived Entities
Viewpoints
Coordinate Systems
Environment
Entity Tags
Tools
Probing
Variable Settings
Surface Mesh Diagnostics
Volume Mesh Diagnostics
Mesh Statistics Panel
Account Settings
Preferences
Virtual GPU Scheduler
Billing
Python API
Getting Started
CLI
Grab-and-Go Snippets
Calculate Dimensional Forces
Change Account and Submit
Estimate a wheel rotation axis with an OBB
Download Results
Folder Operations
Fork a Case
Generate Multiple Meshes
Transform geometric entities with coordinate systems
Get Averaged Forces from a Boundary
Import Sample Surface
Interpolate
List Projects
Move Case to Folder
Plot Probe Monitor Time History
Print Occupied Storage
Reuse Cloud Project
Run a Case on Virtual GPU
Total Flex Credits
List Cases
List Mesh Resources
Examples Library
RANS CFD on 2D CRM Airfoil
Aeroacoustics
Cold-Started Alpha Sweep
Time-Accurate BET eVTOL Simulation Example
Conjugate Heat Transfer
SRF with Cube
DARPA SUBOFF Actuator Disk
Unsteady DDES HLPW4
Dynamic Derivatives Using Sliding Interfaces
F1 Car Demo
Flat Plate with Structural Aerodynamic Load
Hinge Torques Monitoring
Isolated Wing with Propeller BET Model
MRF rotor
Periodic BCs
Time-Accurate Rotor with Thrust-Convergence Stopping Criterion
Time‑Accurate XV‑15 rotor
Transition Model 2D Airfoil
UDD Alpha Controller (Constant CL)
Unsteady 2D cylinder
Wall Roughness
Warm-Started Alpha Sweep
Windsor Body
Migration Guide
BET Migration Tools
Example Monitor Conversion
API Reference
Setup
SimulationParams
Cloud Assets
Project
Case
Geometry
SurfaceMesh
VolumeMesh
SurfaceMeshStats
Entities
Box
Cylinder
Sphere
AxisymmetricBody
CustomVolume
SeedpointVolume
RotationVolume
Draft
DraftContext
create_draft
CoordinateSystemManager
MirrorManager
OBBResult
Meshing
MeshingParams
ModularMeshingWorkflow
MeshingDefaults
SurfaceEdgeRefinement
AngleBasedRefinement
HeightBasedRefinement
AspectRatioBasedRefinement
ProjectAnisoSpacing
SurfaceRefinement
BoundaryLayer
PassiveSpacing
UniformRefinement
AxisymmetricRefinement
GeometryRefinement
snappy.SurfaceMeshingParams
snappy.CastellatedMeshControls
snappy.QualityMetrics
snappy.SmoothControls
snappy.SnapControls
snappy.SurfaceMeshingDefaults
OctreeSpacing
snappy.BodyRefinement
snappy.RegionRefinement
snappy.SurfaceEdgeRefinement
VolumeMeshingParams
VolumeMeshingDefaults
AutomatedFarfield
UserDefinedFarfield
WindTunnelFarfield
CustomZones
MeshSliceOutput
Farfield Specifications
StaticFloor
FullyMovingFloor
CentralBelt
WheelBelts
Reference Geometry
ReferenceGeometry
Operating Condition
AerospaceCondition
LiquidOperatingCondition
GenericReferenceCondition
ThermalState
Material
Air
SolidMaterial
ThermallyPerfectGas
Water
Sutherland
NASA9CoefficientSet
NASA9Coefficients
FrozenSpecies
Volume Models
Fluid
Solid
ActuatorDisk
BETDisk
Rotation
PorousMedium
Surface Models
Wall
SlipWall
Freestream
Inflow
Outflow
Periodic
SymmetryPlane
PorousJump
Time Stepping
Steady
Unsteady
CFL
AdaptiveCFL
RampCFL
Solver Configurations
NavierStokesSolver
SpalartAllmaras
KOmegaSST
NoneSolver
TransitionModelSolver
HeatEquationSolver
Solver Specs
LinearSolver
KrylovLinearSolver
LineSearch
RoeFlux
SLAU2Flux
DetachedEddySimulation
SpalartAllmarasModelConstants
KOmegaSSTModelConstants
TurbulenceModelControls
Run Control
RunControl
StoppingCriterion
User Defined Expressions
UserVariable
User Defined Dynamics
UserDefinedDynamic
Outputs
VolumeOutput
TimeAverageVolumeOutput
SliceOutput
TimeAverageSliceOutput
SurfaceOutput
TimeAverageSurfaceOutput
IsosurfaceOutput
SurfaceIntegralOutput
SurfaceSliceOutput
ProbeOutput
TimeAverageProbeOutput
SurfaceProbeOutput
TimeAverageSurfaceProbeOutput
ForceOutput
ForceDistributionOutput
TimeAverageForceDistributionOutput
StreamlineOutput
TimeAverageStreamlineOutput
RenderOutput
AeroAcousticOutput
MovingStatistic
RenderOutputGroup
render_config.Camera
render_config.PBRMaterial
render_config.FieldMaterial
Output Fields
Output Entities
Isosurface
Slice
Point
PointArray
PointArray2D
Observer
Results
CaseResultsModel
MonitorsResultModel
MonitorCSVModel
NonlinearResidualsResultCSVModel
LinearResidualsResultCSVModel
CFLResultCSVModel
MinMaxStateResultCSVModel
MaxResidualLocationResultCSVModel
TotalForcesResultCSVModel
SurfaceForcesResultCSVModel
CustomForceResultModel
CustomForceCSVModel
SurfaceHeatTransferResultCSVModel
AeroacousticsResultCSVModel
LegacyForceDistributionResultCSVModel
XSlicingForceDistributionResultCSVModel
YSlicingForceDistributionResultCSVModel
ForceDistributionsResultModel
ForceDistributionCSVModel
UserDefinedDynamicsResultModel
UserDefinedDynamicsCSVModel
ActuatorDiskResultCSVModel
ActuatorDiskCoefficientsCSVModel
BETForcesResultCSVModel
BETDiskCoefficientsCSVModel
BETForcesRadialDistributionResultCSVModel
PorousMediumResultCSVModel
PorousMediumCoefficientsCSVModel
Report
report.Chart2D
report.Chart3D
report.NonlinearResiduals
report.ReportTemplate
report.Summary
report.Table
Figure Specifications
report.Grouper
report.PatternCaption
report.Settings
report.FixedRangeLimit
report.ManualLimit
report.SubsetLimit
Data Utilities
report.DataItem
report.Delta
report.Variable
report.Average
report.Expression
report.GetAttribute
Chart3D Cameras
report.Camera
report.BottomCamera
report.FrontCamera
report.FrontLeftBottomCamera
report.FrontLeftTopCamera
report.LeftCamera
report.RearCamera
report.RearLeftTopCamera
report.RearRightBottomCamera
report.TopCamera
Knowledge Base
Preprocessing
Meshing Recommendations
CGNS Mesh Format and Multizone Interface Connectivity
STEP Format CAD Import for Automated Meshing
BET Disk
ESP Tutorials
ESP Tutorial for the ONERA M6 Wing
ESP Tutorial for a 2D Multi-element Airfoil
Simulation
Time Stepping
NavierStokesSolver
TurbulenceModelSolver
TransitionModelSolver
HeatEquationSolver
Propeller Models and Rotational Volume Zones
Aeroacoustics
Solid
PorousMedium
Validation Studies
NACA 0012 Low Speed Airfoil
2D NACA 4412 Airfoil Trailing Edge Separation
2D Backward Facing Step
Transition Modeling
Wall Model
High Lift Common Research Model (HL-CRM)
Drag Prediction of Common Research Model
ONERA M6 Wing
XV-15 Rotor Blade Analysis using the Blade Element Disk Method
DTU 10MW Wind Turbine
Scale-Resolving Simulations Past a Circular Cylinder
Aeroacoustics and Noise Simulation
Underwater Flow Around the DARPA Model 4740 Submarine
Supersonic Aerodynamics of a Hammerhead Launch Vehicle
Papers
Release Notes
Repository
Open issue
.rst
.pdf
XROTORFile
Contents
XROTORFile
XROTORFile
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class
XROTORFile
[source]
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Bases:
BETSingleInputFileBaseModel
