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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 Sliding Interfaces
2.4. User Defined Dynamics
3. Preprocessing
3.1. Engineering Sketch Pad
3.2. 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. High Lift Common Research Model (HL-CRM)
6.6. Drag Prediction of Common Research Model
6.7. ONERA M6 Wing
6.8. XV-15 Rotor Blade Analysis using the Blade Element Disk Method
6.9. DTU 10MW Wind Turbine
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
8. Knowledge Base
8.1. Preprocessing
8.1.1. Meshing Recommendations
8.1.2. Nondimensional Inputs
8.1.3. BET Translators
8.1.4.
SectionalPolars
Best Practices.
8.2. Simulation
8.2.1.
timeStepping
8.2.2.
BETDisks
8.2.3.
navierStokesSolver
8.2.4.
turbulenceModelSolver
8.2.5.
slidingInterfaces
8.3. Postprocessing
8.4. Frequently Asked Questions
9. Publications
9.1. Webinar
9.2. Papers
10. Release Notes
.rst
.pdf
Capabilities
2.
Capabilities
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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 Sliding Interfaces
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. Sliding Interfaces
2.4. User Defined Dynamics
2.4.1. PI controller for angle of attack to control lift coefficient
2.4.2. Dynamic grid rotation using structural aerodynamic load
