Home > Forums > General Forums > Main CFD Forum

shocktube

Mark Forums Read

Reply

Search this Thread

July 18, 2007, 02:29	shocktube	#1
Shuo Guest Posts: n/a	Hello, I am testing a 2D code on the one dimensional shock tube problem. The numerical scheme is a second order flux splitting version of the MacCromick method (Beam & Warming). For some reason, the u and v velocity components are the same at each iteration. Shuo

Reply

« Previous Thread | Next Thread »

Thread Tools	Search this Thread
Show Printable Version Email this Page	Search this Thread: Advanced Search
Display Modes
Linear Mode Switch to Hybrid Mode Switch to Threaded Mode

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 Forum Rules

Similar Threads
Thread	Thread Starter	Forum	Replies	Last Post
Shocktube in OpenFoam	foamer	OpenFOAM	6	January 5, 2013 10:02
Shocktube help needed please	cfdguy08	FLUENT	4	October 4, 2010 07:31
shockTube simulation different solvers	feijooos	OpenFOAM Running, Solving & CFD	8	November 20, 2009 17:20
SHOCKTUBE INITIAL CONDITION	Stefano	FLUENT	0	May 10, 2006 15:55
help:gas-water shocktube problem	gooo	Main CFD Forum	0	May 8, 2005 22:51

All times are GMT -4. The time now is 06:24.