CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > General Forums > Main CFD Forum

Quick Scheme for supersonic reacting flows

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   March 9, 2018, 03:01
Default Quick Scheme for supersonic reacting flows
  #1
Member
 
ARAVIND SRIDHARA
Join Date: Jan 2017
Posts: 32
Rep Power: 9
aravind vashista is on a distinguished road
Hii all
i am solving a problem on 3d supersonic flow with flamelet model for chemical kinetics with 10 species and k-e turbulence model. i employ coupled solver to solve for pressure. i had initially employed second order for all other variables (energy, density,momentum, turbulent kinetic energy, mixture fraction) then later on after few thousand iterations i changed my solution methods to quick scheme for (density, momentum, energy) and retained second order for (turbulent kinetic energy, and mixture fraction). indoing so my mass imbalance and residuals have increased. is it beacuse of quick scheme ? is quick scheme be used for this complex flows? please let me know on this
thank u for your time
aravind vashista is offline   Reply With Quote

Old   March 9, 2018, 19:01
Default
  #2
Senior Member
 
Lucky
Join Date: Apr 2011
Location: Orlando, FL USA
Posts: 5,754
Rep Power: 66
LuckyTran has a spectacular aura aboutLuckyTran has a spectacular aura aboutLuckyTran has a spectacular aura about
You should mention that you are using Fluent because QUICK is not the same in all codes.

Residuals are higher, but the solution is still stable right? And do you mean the residuals converged to higher values or they just spiked after you changed settings? You should expect a spike in residuals whenever you change anything.

My first guess which be to keep density discretization as before to help stabilize the p-v coupling. In general, QUICK is slightly higher order and hence more unstable than 2nd order upwind.
LuckyTran is offline   Reply With Quote

Old   March 10, 2018, 16:40
Default
  #3
Member
 
ARAVIND SRIDHARA
Join Date: Jan 2017
Posts: 32
Rep Power: 9
aravind vashista is on a distinguished road
Thank u for the reply
Yes I am using fluent. Yes the residuals hv spiked up n came back , the solution is not stable yet . The mass imbalance has also increased. N residuals r getting stable at higher value as compared to second order in terms of magnitude
aravind vashista is offline   Reply With Quote

Reply

Tags
quick scheme, reacting, reacting flows, second order schems, supersonic flows


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
Problem in coding QUICK scheme for convection term mahdi_kh8 Main CFD Forum 1 February 17, 2014 04:25
Upwind, central, QUICK scheme for Re~10000 quarkz Main CFD Forum 4 June 23, 2011 16:04
can u suggest me a paper to benchmark the code for quasi-1d reacting flows RAMIREDDY.V.MUVVA Main CFD Forum 0 April 25, 2000 05:51
TVD scheme applied to axsymetric nozzle flows Zhou Hua Main CFD Forum 0 May 7, 1999 01:10
ability of fluent to predict scalar fields in reacting flows ? Mounir Main CFD Forum 1 January 21, 1999 11:08


All times are GMT -4. The time now is 19:16.