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CFD of quadcopter

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April 16, 2022, 07:03	CFD of quadcopter	#1
Al_Psi New Member Abdul Samad Join Date: Apr 2022 Posts: 3 Rep Power: 4	Hi. I am trying to carryout aeroacoustics of a quadcopter. Can someone please guide me how to setup the model for a hovering platform. What should be the inlet and exit conditions, with no x and y velocity? i am using Moving mesh for fluid domain against each rotor, do I need to employ moving wall for the blades inside the domain as well. More so, which model is more appropriate for use SST-Kw or LES? i was getting reverse flow at exit for pressure outlet, tried to replace it with outflow but the problem still persists? Any suggestions please? Regards

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