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:
- Boundary Conditions
- Far Side → Pressure Far-Field
- Pressure = 45.829 psia
- Mach Number = .8395
- Angle of Attack = 3.06 deg
- x-component: 0.9986
- y-component: 0.0534
- Temperature = 460 R
- Repeat for Inlet and Outlet
- Near Side → Symmetry
- Wing Surface and Wing tip → Wall