CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > Software User Forums > SU2

Odd Mach region around leading edge

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   July 22, 2024, 11:43
Default Odd Mach region around leading edge
  #1
R.K
New Member
 
Rutvik Khedkar
Join Date: Mar 2024
Posts: 14
Rep Power: 2
R.K is on a distinguished road
Hi all,

I am simulating flow over an inlet at hypersonic speeds (Mach 7) in 2D using the JST scheme. I have done a mesh convergence study with inviscid simulations and the residuals go to machine accuracy for all the meshes.

I am using the Navier-Stokes solver for the viscous simulations. I have 5 meshes (very_coarse, coarse, medium, fine, very_fine) to do a mesh convergence study. The very_coarse (VC) and coarse (C) meshes converge to a residual rho of -8.5 and -9 with Cauchy on drag = -10 orders of magnitude. The finer meshes barely converge to -4 to -5, before increasing -2 where they plateau. Something I noticed on the very_coarse and coarse meshes, is that there is an abnormal region at the leading edge where the Mach number is higher (11 for VC and 9 for C). I increased the area around the leading edge, but this region still persists.

I played around with the 2nd and 4th coefficients in the scheme; the 4th coefficient has not effect on this region. Increasing 2nd coefficient smooths shocks, so it decreases the Mach number in those regions but its still higher than freestream. Increasing the 2nd coefficient also makes the shock structure in the rest of the flow field very smooth (looks like a smudge on the screen).

Is there a reason why this happens? I did a few first order upwind simulations; they converge almost instantly and the higher Mach region does not exist. Nor does it exist in 2nd order upwind scheme, but these dont converge any further than -4. I want to conduct optimisation, which the JST scheme shows good stability and convergence.

I have attached the config file, history convergence and images of the domain around the leading. The history file also contains information of the meshes (number of cells and y+ values) and images of the high Mach regions. The file is too big to upload, I have uploaded it to google drive: https://drive.google.com/drive/folde...by?usp=sharing

Thank you,
RK
R.K is offline   Reply With Quote

Old   July 23, 2024, 15:09
Default
  #2
Senior Member
 
bigfoot
Join Date: Dec 2011
Location: Netherlands
Posts: 676
Rep Power: 21
bigfootedrockmidget is on a distinguished road
Do you have a converging and nonconverging mesh for us?
This could be seen as a bug, so you can also report it on github issues. But it might also be something that can be solve by using some different settings or mesh, it's hard to tell at this moment.
bigfootedrockmidget is offline   Reply With Quote

Old   July 24, 2024, 06:10
Default
  #3
R.K
New Member
 
Rutvik Khedkar
Join Date: Mar 2024
Posts: 14
Rep Power: 2
R.K is on a distinguished road
I have uploaded two meshes on the drive - one which converges and another which diverges. I will report it on github later today.

Thanks,
RK
R.K is offline   Reply With Quote

Reply


Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

BB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Trackbacks are Off
Pingbacks are On
Refbacks are On


Similar Threads
Thread Thread Starter Forum Replies Last Post
Negative initial temperature error (chtMultiRegionFoam) jebin OpenFOAM Pre-Processing 60 July 17, 2022 06:10
[ANSYS Meshing] Wing leading edge curvature meshing problem Alexia166 ANSYS Meshing & Geometry 2 April 21, 2021 05:29
Meshing near leading and trailing edge of propeller surajp92 STAR-CCM+ 1 June 1, 2017 02:40
Leading edge separation and efficiency KK Main CFD Forum 2 December 3, 2008 07:19
Airfoil Heat Transfer Near Leading Edge Glenn Main CFD Forum 0 June 28, 2007 13:53


All times are GMT -4. The time now is 14:35.