Flow360 Documentation
release-22.2.3.0
Table of Contents
1. Quick Start
2. Capabilities
3. Preprocessing
4. Solver Configuration
5. Postprocessing
6. Python API Reference
7. Frequently Asked Questions
8. Case Studies
8.1. NACA 0012 Low Speed Airfoil
8.2. 2D NACA 4412 Airfoil Trailing Edge Separation
8.3. 2D Backward Facing Step
8.4. High Lift Common Research Model (HL-CRM)
8.5. Drag Prediction of Common Research Model
8.6. ONERA M6 Wing
8.7. XV-15 Rotor Blade Analysis using the Blade Element Disk Method
9. Tutorials
10. Conventions
11. Publications
12. Release Notes
Flow360 Documentation
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8.
Case Studies
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8.
Case Studies
8.1. NACA 0012 Low Speed Airfoil
8.1.1. Introduction
8.1.2. Mesh and Flow Configuration
8.1.3. SA/SA-RC Model Results
8.1.4. SST(m) Model Results
8.1.5. Remarks
8.2. 2D NACA 4412 Airfoil Trailing Edge Separation
8.2.1. Introduction
8.2.2. Simulation setup
8.2.3. Numerical Results
8.3. 2D Backward Facing Step
8.3.1. Introduction
8.3.2. Simulation setup
8.3.3. Numerical Results
8.4. High Lift Common Research Model (HL-CRM)
8.4.1. Introduction
8.4.2. Problem Description
8.4.3. Mesh
8.4.4. Setup and Solution
8.4.5. Grid Convergence
8.4.6. Results
8.4.7. Summary
8.5. Drag Prediction of Common Research Model
8.5.1. Introduction
8.5.2. Problem Description
8.5.3. Mesh
8.5.4. Setup and Solution
8.5.5. Grid Convergence
8.5.6. Results
8.5.7. Summary
8.6. ONERA M6 Wing
8.6.1. Introduction
8.6.2. Setup and Solution
8.6.3. Grid Convergence
8.6.4. Results
8.6.5. Summary
8.7. XV-15 Rotor Blade Analysis using the Blade Element Disk Method
8.7.1. Highlights
8.7.2. Introduction
8.7.3. Helicopter Hovering Mode
8.7.4. Airplane Mode
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