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

Subsonic Inflow boundary Condition

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   March 24, 2014, 15:28
Default Subsonic Inflow boundary Condition
  #1
Senior Member
 
Joachim
Join Date: Mar 2012
Location: Paris, France
Posts: 145
Rep Power: 15
Joachim is on a distinguished road
hey everyone!

I am currently implementing the boundary conditions for my solver, and I have a question for you.

I have been reading this article (Inflow/Outflow Boundary Conditions with Application to FUN3D), which is available online at this address.

https://www.google.com/url?sa=t&rct=...62922401,d.dmQ

I have already found some typos in it, but I would like to have your opinion on that one.

If you go page 8, they defined the Riemann characteristics R+ = -Ui - 2ci/(gamma-1) in Eq. 37. Shouldn't it be R+ = -Ui + 2ci/(gamma-1) instead? The same thing happens in Eq. 39, so that their b coefficient in Eq. 43 is 2R+ instead of -2R+.

Is that actually a mistake in the article, or did I miss something?

Thank you for your help!

Joachim
Joachim 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
Wind turbine simulation Saturn CFX 58 July 3, 2020 01:13
inlet velocity boundary condition murali CFX 5 August 3, 2012 08:56
help with velocity boundary condition potentialFoam hfc OpenFOAM Running, Solving & CFD 2 May 31, 2012 19:52
External Radiation Boundary Condition for Grid Interface CFD XUE FLUENT 0 July 9, 2010 02:53
External Radiation Boundary Condition (Two sided wall), Grid Interface CFD XUE FLUENT 0 July 8, 2010 06:49


All times are GMT -4. The time now is 02:43.