Setting the Boundary Conditions

Here, you will learn to set-up the wing model in Ansys Fluent. We will discuss the boundary conditions necessary to solve this flow around the wing.

Summary of the above video:
  1. Boundary Conditions
  2. Far Side → Pressure Far-Field
  3. Pressure = 45.829 psia
  4. Mach Number = .8395
  5. Angle of Attack = 3.06 deg
  6. x-component: 0.9986
  7. y-component: 0.0534
  8. Temperature = 460 R
  9. Repeat for Inlet and Outlet
  10. Near Side → Symmetry
  11. Wing Surface and Wing tip → Wall