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

Hypersonic problem

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   October 28, 2007, 09:20
Default Hypersonic problem
  #1
Subramani Sockalingam
Guest
 
Posts: n/a
What I am trying to do is to find the solution where pressure, temperature and Mach number are 8.1757 Pa, 227 K and 22.41 (freestream conditions). I started with Mach 2 and increased the Mach number using the same pressure and temperature. At Mach 8 the absolute pressure was limited to the minimum 1 in a number of cells and the Mach number at some point in the domain became 90. Why would this happen? I am running a 2D inviscid implicit density based model.

Thanks, Subramani
  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
conduction problem venkataramana OpenFOAM 3 December 1, 2013 07:30
Hypersonic problem Subramani Sockalingam FLUENT 4 December 12, 2007 07:57
CFL for explicit hypersonic problem Subramani Sockalingam FLUENT 1 October 29, 2007 05:05
Adiabatic and Rotating wall (Convection problem) ParodDav CFX 5 April 29, 2007 19:13
Is this problem well posed? Thomas P. Abraham Main CFD Forum 5 September 8, 1999 14:52


All times are GMT -4. The time now is 11:17.