Inlet Profile for Supersonic Flow

BrianB · May 21, 2020, 17:09

How can I implement an inlet profile for a 2D supersonic flow? I am running a compressible, RANS-SA Mach 5 flow in SU2 v6.2 and would like to use an inlet profile to impose an incoming boundary layer. However, I am using a supersonic inlet and the SU2 Laminar Backward-facing Step tutorial uses a normal inlet. Can I implement an inlet profile if I am using a supersonic inlet?

pcg · May 21, 2020, 17:46

No, you would have to modify some code for that.
Also the supersonic inlet is purely convective, it does not account for diffusion terms.

May 21, 2020, 17:09	Inlet Profile for Supersonic Flow	#1
BrianB New Member Join Date: May 2020 Posts: 7 Rep Power: 5	How can I implement an inlet profile for a 2D supersonic flow? I am running a compressible, RANS-SA Mach 5 flow in SU2 v6.2 and would like to use an inlet profile to impose an incoming boundary layer. However, I am using a supersonic inlet and the SU2 Laminar Backward-facing Step tutorial uses a normal inlet. Can I implement an inlet profile if I am using a supersonic inlet?

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May 21, 2020, 17:46		#2
pcg Senior Member Pedro Gomes Join Date: Dec 2017 Posts: 465 Rep Power: 13	No, you would have to modify some code for that. Also the supersonic inlet is purely convective, it does not account for diffusion terms.