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The flow remains attached to the airfoil surface on the windward side (the bottom) as the flow turns the corner it cannot sustain the massive amounts of acceleration needed to remain attached so it separates causing the vortex shedding to only occur on top
JoeBrock28 2 weeks ago
How come there's only vortex shedding on the top?
marcofking 2 years ago
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TheIlikecheese 2 years ago
He's using the Spalart-Allmaras one equation turbulence model
kel85uk 3 years ago
Hi I just like to now your flow reynolds number for this simulation, and I see you are using fluent which Viscous model are you using? I'm doing a project in something similar
danieltuerto 4 years ago