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

normal shock in diverging section of cd nozzle

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   March 19, 2013, 09:41
Default normal shock in diverging section of cd nozzle
  #1
New Member
 
Naveen Raj N
Join Date: Mar 2013
Posts: 3
Rep Power: 13
naveenraj is on a distinguished road
hi
i have a cd nozzle having area function as A=1+2.2(x-1.5)^2
pe/po = 0.6784
while solving through fluent getting divergence in the solution.
i tried an inviscid,density based model. can anybody help me to rectify this problem.
naveenraj 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
[Commercial meshers] converting Fluent mesh to openfoam standard mesh deepesh OpenFOAM Meshing & Mesh Conversion 31 March 29, 2017 05:59
dsmcInitialise - dsmcFoam archymedes OpenFOAM Pre-Processing 94 July 15, 2016 16:14
help - Running Converging Diverging Nozzle with a shock wave Daco FLUENT 0 September 3, 2012 08:23
NACA0012 geometry/design software needed Franny Main CFD Forum 13 July 7, 2007 15:57
Normal shock waves Fernando Velasco Main CFD Forum 1 April 6, 2000 14:10


All times are GMT -4. The time now is 09:38.