7. Tutorials

• 7.1. Geometry Modeling and Preparation for Automated Meshing: An Example of the ONERA M6 Wing
  • 7.1.1. 3D Sketches of Airfoils
  • 7.1.2. Wing Planform
  • 7.1.3. Wing Solid Model
  • 7.1.4. Adding Edge Attribute
  • 7.1.5. Adding Face and Group Attributes
• 7.2. Non-Dimensionalization and Integrated Loads Post-Processing in Flow360
  • 7.2.1. Introduction
  • 7.2.2. Flow360 json file input calculations
  • 7.2.3. Force and Moments Output Conventions
• 7.3. RANS CFD on 2D High-Lift System Configuration Using the Flow360 Python Client
  • 7.3.1. Modeling Multi-element Configurations in ESP
  • 7.3.2. RUN CFD on multi-element configurations using Flow360
• 7.4. Blade Element Theory using the XV-15 rotor
  • 7.4.1. Preprocessing
  • 7.4.2. Flow360 BET Configuration
  • 7.4.3. Output and postprocessing
• 7.5. Time-accurate RANS CFD on a propeller using a sliding interface: the XV-15 rotor geometry
  • 7.5.1. Rotational and stationary volumes
  • 7.5.2. Sliding interface requirements
  • 7.5.3. XV-15 setup
  • 7.5.4. Defining a Mesh.json file
  • 7.5.5. Uploading your mesh
  • 7.5.6. Defining a case configuration file.
  • 7.5.7. Case input conditions
  • 7.5.8. Case running
• 7.6. Calculating Dynamic Derivatives using Sliding Interfaces
  • 7.6.1. Geometry and Mesh
  • 7.6.2. Case Setup
  • 7.6.3. Submission
  • 7.6.4. Postprocessing
• 7.7. Automated Meshing for Internal Flow
  • 7.7.1. Geometry
  • 7.7.2. Surface Mesh
  • 7.7.3. Volume Mesh
• 7.8. Conjugate Heat Transfer for Cooling Fins
  • 7.8.1. Geometry and Mesh
  • 7.8.2. Case
  • 7.8.3. Results
• 7.9. TU Berlin TurboLab Stator simulation using periodic boundary conditions
  • 7.9.1. Description
  • 7.9.2. Meshing the geometry
  • 7.9.3. Defining the boundary conditions.
  • 7.9.4. Case running
  • 7.9.5. Translational periodic boundary conditions