6. Case Studies 📖

• 6.1. NACA 0012 Low Speed Airfoil
  • Introduction
  • Mesh and Flow Configuration
  • SA/SA-RC Model Results
  • SST(m) Model Results
  • Remarks
• 6.2. 2D NACA 4412 Airfoil Trailing Edge Separation
  • Introduction
  • Simulation setup
  • Numerical Results
• 6.3. 2D Backward Facing Step
  • Introduction
  • Simulation setup
  • Numerical Results
• 6.4. Transition Modeling
  • Introduction
  • Flat Plate Case
  • NLF(1)-0416 Airfoil Case
  • Conclusions
• 6.5. Wall Model
  • Introduction
  • Wall Model Formulation in Flow360
  • Flat Plate Case
  • NACA0012 Case
  • ONERAM6 Wing Case
  • Ahmed Body Case
  • Windsor Body Case
  • Conclusions
• 6.6. High Lift Common Research Model (HL-CRM)
  • Introduction
  • Problem Description
  • Mesh
  • Setup and Solution
  • Grid Convergence
  • Results
  • Summary
• 6.7. Drag Prediction of Common Research Model
  • Introduction
  • Problem Description
  • Mesh
  • Setup and Solution
  • Grid Convergence
  • Results
  • Summary
• 6.8. ONERA M6 Wing
  • Introduction
  • Grid Convergence
  • Results
  • Summary
• 6.9. XV-15 Rotor Blade Analysis using the Blade Element Disk Method
  • Highlights
  • Introduction
  • Helicopter Hovering Mode
  • Airplane Mode
• 6.10. DTU 10MW Wind Turbine
  • Introduction
  • Rotor Geometry
  • Automated Meshing
  • Flow Configuration
  • Residual Convergence
  • Surface and Volumetric Results
  • Sectional Loads on One of the Blades
  • Integrated Loads on the Entire Rotor
  • Off-Design Performance
• 6.11. Scale-Resolving Simulations Past a Circular Cylinder
  • Introduction
  • Simulation Setup
  • Grid Refinement Study
  • Time-Dependent Flow Field Results
  • Time-Averaged Flow Field Results
  • Conclusions
• 6.12. Aeroacoustics and Noise Simulation
  • Introduction
  • Cross Flow over Circular Cylinder
  • Rod-Airfoil Configuration
  • Two-bladed Propeller
  • Conclusions