|
[Sponsors] |
October 18, 2019, 01:13 |
Supersonic Inlet Boundary Condition
|
#1 |
Member
Yuva
Join Date: Oct 2015
Location: Korea Rep of
Posts: 33
Rep Power: 10 |
Dear CFD Online Community,
We are working on the simulation of a centrifugal compressor of high RPM where the inlet Mach number could reach a unity. I would like know if ANSYS CFX can handle the supersonic nature of the flow at the inlet of the compressor and I am not sure which options should be used for this purpose. In order to obtain a stable and high accurate supersonic compressor performance CFD results, what would be the recommendations for the mesh quality, boundary layer refinement, turbulence model, boundary conditions robustness, convergence tips and solver type of ANSYS CFX. Thank you in advance for your help. Kind regards. |
|
October 18, 2019, 04:23 |
|
#2 |
Senior Member
Join Date: Nov 2015
Posts: 244
Rep Power: 11 |
Question is too common. Yes, CFX can calculate high Mach flow.
You can read FAQ and Best Practices for guidance. https://www.cfd-online.com/Wiki/Ansys_FAQ https://www.cfd-online.com/Wiki/Best...omachinery_CFD |
|
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
Acoustic boundary condition with pressure perturbation at inlet | hand90 | CFX | 2 | August 10, 2018 07:36 |
CFD analaysis of Pelton turbine | amodpanthee | CFX | 31 | April 19, 2018 18:02 |
UDF fluent:Change boundary condition. determination inlet and outlet boundary in "t" | gzamiri@gmail.com | FLUENT | 0 | September 27, 2015 05:32 |
Wrong flow in ratating domain problem | Sanyo | CFX | 17 | August 15, 2015 06:20 |
Question about heat transfer coefficient setting for CFX | Anna Tian | CFX | 1 | June 16, 2013 06:28 |