Menu

Discussion Forum

New Discussion
Filter

Discussion Closed This discussion was created more than 6 months ago and has been closed. To start a new discussion with a link back to this one, click here.

Shock waves in High Mach Number flow

Posted Aug 12, 2014, 10:51 a.m. EDT Computational Fluid Dynamics (CFD) Version 4.4, Version 5.2 1 Reply

Nagaraja S R
Send Private Message Flag post as spam

Please login with a confirmed email address before reporting spam

Hi

I am modelling high mach number flow over rigid bodies. I am unable to capture the normal shock or oblique shock wave. do I need any special settings for CFL number or Mesh
1 Reply Last Post Apr 20, 2016, 12:48 p.m. EDT
COMSOL Moderator

Hello Nagaraja S R

Your Discussion has gone 30 days without a reply. If you still need help with COMSOL and have an on-subscription license, please visit our Support Center for help.

If you do not hold an on-subscription license, you may find an answer in another Discussion or in the Knowledge Base.

Ozan Isur
Send Private Message Flag post as spam

Please login with a confirmed email address before reporting spam

Posted: 8 years ago Apr 20, 2016, 12:48 p.m. EDT
Hello,

I ve seen your comsol thread about 2 years ago with a subject of shock waves over rigid bodies. Were you able sort out the the problem? I am asking because I want to make a high mach flow over a 2-D wing profile and observe the strong and weak shocks over it.

Sincerely
Kerozi
Hello, I ve seen your comsol thread about 2 years ago with a subject of shock waves over rigid bodies. Were you able sort out the the problem? I am asking because I want to make a high mach flow over a 2-D wing profile and observe the strong and weak shocks over it. Sincerely Kerozi

Note that while COMSOL employees may participate in the discussion forum, COMSOL® software users who are on-subscription should submit their questions via the Support Center for a more comprehensive response from the Technical Support team.

Suggested Content