8. Case Studies

• 8.1. NACA 0012 Low Speed Airfoil
  • 8.1.1. Introduction
  • 8.1.2. Mesh and Flow Configuration
  • 8.1.3. Numerical Results
  • 8.1.4. Remarks
• 8.2. High Lift Common Research Model (HL-CRM)
  • 8.2.1. Introduction
  • 8.2.2. Problem Description
  • 8.2.3. Mesh
  • 8.2.4. Setup and Solution
  • 8.2.5. Grid Convergence
  • 8.2.6. Results
  • 8.2.7. Summary
• 8.3. Drag Prediction of Common Research Model
  • 8.3.1. Introduction
  • 8.3.2. Problem Description
  • 8.3.3. Mesh
  • 8.3.4. Setup and Solution
  • 8.3.5. Grid Convergence
  • 8.3.6. Results
  • 8.3.7. Summary
• 8.4. ONERA M6 Wing
  • 8.4.1. Introduction
  • 8.4.2. Setup and Solution
  • 8.4.3. Grid Convergence
  • 8.4.4. Results
  • 8.4.5. Summary
• 8.5. XV-15 Rotor Blade by Blade Element Disk Method
  • 8.5.1. Highlights
  • 8.5.2. Introduction
  • 8.5.3. Helicopter Hovering Mode
  • 8.5.4. Airplane Mode