|March 25, 2009, 06:02||
Help! Supersonic/hypersonic flow over sharp wedge/cone, detached shock
Tan Jun Wei
Join Date: Mar 2009
Posts: 1Rep Power: 0
Hi, im doin supersonic and hypersonic flow over a 2D wedge and 3D cone.
I've used symmetry and axisymmetric condition for them to save computational time.
I'm interested in finding the detached shock when the wedge/cone angle exceeds the max. angle. However, i cant seem to get a converged solution and the shock cant seem to detach.
Im using inviscid model, implicit, 2nd order model to run fluent.
Can anyone tell me what settings i need to input to be able to get a satisfactory result?
|cone, detached shock, wedge|
|Thread||Thread Starter||Forum||Replies||Last Post|
|benchmark: flow over a circular cylinder||goodegg||Main CFD Forum||12||January 22, 2013 12:47|
|Can 'shock waves' occur in viscous fluid flows?||diaw||Main CFD Forum||105||November 20, 2009 05:19|
|Mass flow and U-Mom flow in CFX||Zhihua Xie||CFX||0||September 3, 2007 09:49|
|Question on 3D potential flow||Adrin Gharakhani||Main CFD Forum||13||June 21, 1999 05:18|
|computation about flow around a yawed cone||Tylor Xie||Main CFD Forum||0||June 9, 1999 07:33|