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Table of Contents
1. Quick Start
1.1. Introduction to Flow360
1.2. ONERA M6 Wing with WebUI
1.3. ONERA M6 Wing with Python API
1.4. Automated Meshing with WebUI
1.5. Automated Meshing with Python API
1.6. NREL S809 Airfoil
1.7. XV-15 Rotor
2. Capabilities
2.1. Overview
2.2. Feature Compatibility Matrix
2.3. Propeller Models and Rotational Volume Zones
2.4. Aeroacoustics
2.5. User Defined Dynamics
2.6. User Defined Post Processing
3. Preprocessing
3.1. Mesh Configuration File
3.2. Engineering Sketch Pad
3.3. Automated Meshing
4. Solver Configuration
5. Python API Reference
6. Case Studies
6.1. NACA 0012 Low Speed Airfoil
6.2. 2D NACA 4412 Airfoil Trailing Edge Separation
6.3. 2D Backward Facing Step
6.4. Transition Modeling
6.5. Wall Model
6.6. High Lift Common Research Model (HL-CRM)
6.7. Drag Prediction of Common Research Model
6.8. ONERA M6 Wing
6.9. XV-15 Rotor Blade Analysis using the Blade Element Disk Method
6.10. DTU 10MW Wind Turbine
6.11. Scale-Resolving Simulations Past a Circular Cylinder
6.12. Aeroacoustics and Noise Simulation
7. Tutorials
7.1. Geometry Modeling and Preparation for Automated Meshing: An Example of the ONERA M6 Wing
7.2. Non-Dimensionalization and Integrated Loads Post-Processing in Flow360
7.3. RANS CFD on 2D High-Lift System Configuration Using the Flow360 Python Client
7.4. Blade Element Theory using the XV-15 rotor
7.5. Time-accurate RANS CFD on a propeller using a sliding interface: the XV-15 rotor geometry
7.6. Calculating Dynamic Derivatives using Sliding Interfaces
7.7. Automated Meshing for Internal Flow
7.8. Conjugate Heat Transfer for Cooling Fins
7.9. TU Berlin TurboLab Stator simulation using periodic boundary conditions
7.10. User Defined Dynamics
7.11. User Defined Postprocessing via
userDefinedFields
8. Knowledge Base
8.1. Preprocessing
8.1.1. Meshing Recommendations
8.1.2. CGNS Mesh Format and Multizone Interface Connectivity
8.1.3. STEP Format CAD Import for Automated Meshing
8.1.4. Nondimensional Inputs
8.1.5.
Boundary Conditions
8.1.6. User Defined Expressions
8.1.7. BET Translators
8.1.8.
SectionalPolars
Best Practices.
8.2. Simulation
8.2.1.
timeStepping
8.2.2.
BETDisks
8.2.3.
actuatorDisks
8.2.4.
navierStokesSolver
8.2.5.
turbulenceModelSolver
8.2.6.
transitionModelSolver
8.2.7.
heatEquationSolver
8.2.8.
volumeZones
8.2.9.
porousMedia
8.3. Postprocessing
8.4. Fixing Divergence Issues
8.5. Frequently Asked Questions
9. Publications
9.1. Webinar
9.2. Papers
10. Release Notes
.rst
.pdf
Capabilities
2.
Capabilities
#
2.1. Overview
2.1.1. Meshing
2.1.2. Modeling Options
2.1.3. Turbulence Models
2.1.4. Boundary Conditions
2.2. Feature Compatibility Matrix
2.3. Propeller Models and Rotational Volume Zones
2.3.1. Overview
2.3.2. Actuator Disk (AD)
2.3.3. Blade Element Theory Disk (BET Disk)
2.3.4. Blade Element Theory Line (BET Line)
2.3.5. Rotational Volume Zone
2.3.6. Multiple Reference Frame (MRF)
2.3.7. Single Reference Frame (SRF)
2.4. Aeroacoustics
2.4.1. Overview
2.5. User Defined Dynamics
2.5.1. Overview
2.6. User Defined Post Processing
2.6.1. Overview
2.6.2. User Defined Fields
2.6.3. User Defined Surface Integrals
2.6.4. User Defined Monitors
