|
[Sponsors] | |||||
|
|
|
#1 |
|
New Member
Join Date: Apr 2024
Location: India
Posts: 14
Rep Power: 3 ![]() |
hello everyone, I have simulated the flow through a CD planar nozzle. The nozzle was made using Method of Characteristics for an exit mach number of 2.
The simulation was done in Ansys Fluent for inviscid condition. However, I just need some validation to check whether my results are correct or not. I have attached the mach number contour plot and the contour line. I do see a reflection of the mach line. Anyway I can mitigate this? Maybe modifying the code, refining the mesh etc? Any insights on this is appreciated. Thank you! |
|
|
|
|
|
![]() |
| Thread Tools | Search this Thread |
| Display Modes | |
|
|
Similar Threads
|
||||
| Thread | Thread Starter | Forum | Replies | Last Post |
| Compressible nozzle flow - no problem for fluent but impossible with openFOAM? | flar.t | OpenFOAM Running, Solving & CFD | 10 | March 30, 2022 02:21 |
| CFG file for Nozzle | Nicola_Fontana | SU2 | 0 | November 26, 2021 06:42 |
| Oscillating flow over a cavity validation case | Sparow89 | FLUENT | 0 | June 2, 2016 16:18 |
| Different flow patterns in CFX and Fluent | avi@lpsc | CFX | 6 | April 17, 2012 02:22 |
| compressible flow in a counterflow nozzle | d.vamsidhar | FLUENT | 0 | November 24, 2005 02:45 |