CFD Online Logo CFD Online URL
Home > Forums > Main CFD Forum

Shock wave over the wing in transonic flow

Register Blogs Members List Search Today's Posts Mark Forums Read

LinkBack Thread Tools Display Modes
Old   February 26, 2013, 17:30
Default Shock wave over the wing in transonic flow
New Member
Join Date: Nov 2012
Posts: 19
Rep Power: 6
malik is on a distinguished road
hi everyone,

I am running the inviscid transonic flow over ONERA M6 wing (density-based case) but I am not getting the shock-wave over the wing. I am running at M=0.84 and AoA=3.06. The questions that I want to confirm are:
1. Can we get shock wave with first order scheme or i need to use second order scheme.
2. In solution methods do I need to choose Implicit or Explicit (I am choosen implicit)
3. Which smoothing shoukd i use AUSM or Roe

I am sure that my mesh is fine.

Any help will be greatly appreciated.

Thanks in advance
malik is offline   Reply With Quote


Thread Tools
Display Modes

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 On
Pingbacks are On
Refbacks are On

Similar Threads
Thread Thread Starter Forum Replies Last Post
Boundary condition for transonic flow over slender body rock.senthilkumar FLUENT 0 February 19, 2013 06:26
help - Running Converging Diverging Nozzle with a shock wave Daco FLUENT 0 September 3, 2012 08:23
Review: Reversed flow CRT FLUENT 0 July 20, 2012 13:03
Setting up Flow around a Wing Simulation help Atella CFX 3 January 3, 2010 12:51
Exp. data for transonic flow J. Held Main CFD Forum 4 April 1, 1999 22:21

All times are GMT -4. The time now is 12:18.