CFD Online Logo CFD Online URL
Home > Forums > Software User Forums > ANSYS > FLUENT

Engine Boundary Conditions

Register Blogs Members List Search Today's Posts Mark Forums Read

LinkBack Thread Tools Display Modes
Old   October 20, 2008, 16:05
Default Engine Boundary Conditions
Posts: n/a
I am attempting to model the influence of the engine nacelle on the wing of a Gulfstream G-II business jet. Does anyone know what boundary condition I should use for the inlet face and outlet face of the engine?

Currently, I have a pressure outlet boundary condition for the back of the flow volume, with velocity inlets for the other 5 faces.
  Reply With Quote

Old   October 20, 2008, 16:07
Default Re: Engine Boundary Conditions
Posts: n/a
I should mention, I want to simulate the engine running, i.e. with a mass flow rate though the nacelle, if that makes sense...
  Reply With Quote


Thread Tools
Display Modes

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 On
Pingbacks are On
Refbacks are On

Similar Threads
Thread Thread Starter Forum Replies Last Post
Engine Nacelle Boundary Conditions Tyler Neale FLUENT 0 November 14, 2008 16:53
Burgerbs equation non constant Boundary Conditions Initial Conditions arkangel OpenFOAM Running, Solving & CFD 1 October 2, 2008 14:48
Boundary conditions for turbulent boundary layer Thomas FLUENT 1 June 17, 2008 05:14
boundary conditions for boundary layer flow A. Al-zoubi CFX 0 November 3, 2007 08:11
Integral boundary conditions turbulent intensitylength boundary conditions olesen OpenFOAM Running, Solving & CFD 0 July 27, 2006 07:18

All times are GMT -4. The time now is 14:52.