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Table of Contents
1. Quick Start
1.1. Run CFD using Web UI: An example of ONERA M6 Wing
1.2. Run CFD using Python API: An example of ONERA M6 Wing
1.3. Run CFD using Automated Meshing and Web UI
1.4. Run CFD using Automated Meshing and Python API
1.5. Run CFD using Automated Meshing: An example of S809 Airfoil
1.6. Run CFD on a propeller: An example XV-15 rotor geometry
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. Install Engineering Sketch Pad (ESP)
3.2. Manual Meshing
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. High Lift Common Research Model (HL-CRM)
6.5. Drag Prediction of Common Research Model
6.6. ONERA M6 Wing
6.7. XV-15 Rotor Blade Analysis using the Blade Element Disk Method
6.8. 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. Time-accurate RANS CFD on a propeller using a sliding interface: the XV-15 rotor geometry
8. Knowledge Base
8.1. Pre-Processing
8.2. Solver Configuration Recommendations
8.2.1. BET Disk and BET Line
8.3. Post-Processing
8.4. Frequently Asked Questions
9. Publications
9.1. Webinar
9.2. Papers
10. Release Notes
.rst
.pdf
Solver Configuration Recommendations
8.2.
Solver Configuration Recommendations
#
8.2.1. BET Disk and BET Line
8.2.1.1.
radius
8.2.1.2.
rotationDirectionRule
8.2.1.3.
axisOfRotation
8.2.1.4.
omega
8.2.1.5.
chords
and
twists
