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

How to get shock self oscillation in Sajben transonic diffuser?

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   April 2, 2014, 22:45
Default How to get shock self oscillation in Sajben transonic diffuser?
  #1
New Member
 
Yao, Cheng
Join Date: Nov 2011
Location: Harbin
Posts: 7
Rep Power: 15
slaon is on a distinguished road
Hi, all:

I'm doing a transient flow in the Sajben diffuser including self-excited oscillation, following the work of
Hsieh, T., Bogar, T. J., and Coakley, T. J. (1987) "Numerical Simulation and Comparison with Experiment for Self-Excited Oscillations in a Diffuser Flow," AIAA Journal, Vol. 25, No. 7, pp. 936-943.

The steady state flow is list in NASA's verification page. The geometry looks like this.

First, I get the steady state flow. It agrees well with the mean experiment results, as shown in NASA's verification page.

Then, I start a transient calculation. The time increment is set to 1e-6 s. However, it still keeps steady state. I changed the turbulence models (standard k-e, RNG k-e, standard k-w, SST k-w). Still steay flow.

Anybody know how to get a self oscillating flow in the Sajben diffuser?

Thanks for many suggestions.

Best wishes,
Cheng, Yao.
slaon is offline   Reply With Quote

Old   May 22, 2014, 00:39
Default
  #2
New Member
 
Yao, Cheng
Join Date: Nov 2011
Location: Harbin
Posts: 7
Rep Power: 15
slaon is on a distinguished road
I solved the problem by using CFL=100 in a 2nd order implicit time scheme. :-)
slaon 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
Shock wave over the wing in transonic flow malik Main CFD Forum 0 February 26, 2013 17:30
Strong oscillation at transonic mach number martingariepy FLUENT 2 May 12, 2009 12:40
Strong oscillation at transonic mach number martingariepy ANSYS 0 May 12, 2009 09:45
Unable to Capture Shock in Transonic Flow Tim Siemens 6 January 29, 2009 07:05
Inlet diffuser of ramjet Mohammad Kermani Main CFD Forum 25 December 29, 2000 19:46


All times are GMT -4. The time now is 20:11.