 |
 |
 |
|
|
|
[Sponsors] | ||||
July 14, 2023, 12:21
|
Supersonic Shock Train Simulation
|
#1 |
|
New Member
Ashwin
Join Date: Jul 2023
Posts: 10
Rep Power: 3  |
Hello, I'm trying to simulate a shock train formed in a rectangular duct under supersonic conditions by referring a research paper.
Boundary Conditions - Pressure Inlet - Total Pressure= 310,000 Pa, Static Pressure= 16,535 Pa Total Temp = 289K Pressure Outlet - Static Pressure = 99,000 Pa. Density based solver, Ive tried k-epsilon and k-w sst. However, when I run the simulation, I'm unable to get a convergent solution and I am unable to replicate the results of the research paper. If anyone has done a similar simulation, could you please guide me? Thanks |
|
|
|
|
|
December 7, 2023, 08:52
|
|
#2 |
|
New Member
Wenbin Bai
Join Date: Dec 2023
Posts: 1
Rep Power: 0 |
Can you produce the residual curves?
|
|
|
|
|
|
 |
| Tags |
| convergence, shock train, supersonic inlet |
|
|
Similar Threads
|
||||
| Thread | Thread Starter | Forum | Replies | Last Post |
| 2D axisymmetric Supersonic flow simulation | gokenq | FLUENT | 19 | August 5, 2022 14:41 |
| Need Help With SU2 Supersonic Simulation | Moose21 | SU2 | 2 | July 18, 2022 18:57 |
| Simulation of Normal Shock in Ansys | 10ume039 | ANSYS | 1 | February 1, 2016 04:34 |
| Problem with pseudo shock simulation! | Sridhar thiru | FLUENT | 1 | December 22, 2015 08:42 |
| 2d axisymmetric simulation of supersonic jet on liquid surface using VOF model | DKanungo | Fluent Multiphase | 0 | June 20, 2014 03:15 |
Linear Mode
