The motivation was to create an animation demonstrating the Von Karman vortex street effect with airflow over a 2D cylinder cross section
The computational domain (wind tunnel area) will be 2.5 m tall by 10 m long and will contain a 0.1 m diameter cylinder which is 2.5 m from the front of the tunnel and 1 m from the bottom of the tunnel.
the boundary conditions include a 25 m/s velocity inlet, pressure outlet condition, and no-slip at the wall.
this analysis assumes incompressible flow and is evaluated under the transient time condition.
the following models where used:
Multiphase - off
Energy - off
Viscous - SST k-omega
Radiation - off
Heat Exchanger - off
Species - off
Discrete Phase - off
Solidification and Melting - off
Acoustics - off
Structure - off
Potential/Li-ion Battery - off
Air was assumed to have a constant density and constant viscosity
The Solution Methods used the following parameters
Pressure-Velocity Coupling - SIMPLE Scheme
Spatial Discretization
Least Square Cell Based Gradient
Second Order Pressure
Second Order Upwind Momentum
Second Order Upwind Turbulent Kinetic Energy
Second Order Upwind Specific Dissipation Rate
Second Order Implicit Transient Formulation
The Calculation was then run for 500 timesteps (0.001 s intervals) with max 20 iterations per timestep. The results for this calculation are shown bellow.