CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > Software User Forums > ANSYS > FLUENT

Pressure Inlet BC Inputs

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

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   October 29, 2021, 15:48
Question Pressure Inlet BC Inputs
  #1
New Member
 
Kevin Davis
Join Date: Oct 2021
Posts: 2
Rep Power: 0
kdavis1521 is on a distinguished road
I'm attempting to do a pressure inlet boundary condition for a supersonic oxygen inlet. The values given for the inlet are 914,468 Pa for stagnation pressure, 2.1 for mach number and 298 K for total temperature.

I was under the impression that stagnation pressure would be entered into "Gauge Total Pressure" and the "Supersonic/Initial Gauge Pressure" could then be calculated as static pressure using the isentropic flow relation, resulting in a value of 100,000 Pa. However, when I enter these values I end up with an initial velocity that is more than double what is expected for this oxygen jet. I am struggling to figure out what I am doing wrong and would greatly appreciate if anyone could provide any help. Thanks.
kdavis1521 is offline   Reply With Quote

Old   October 29, 2021, 18:52
Default
  #2
Senior Member
 
Lorenzo Galieti
Join Date: Mar 2018
Posts: 373
Rep Power: 12
LoGaL is on a distinguished road
is the operating pressure set to zero?
LoGaL is offline   Reply With Quote

Old   October 29, 2021, 19:55
Default
  #3
New Member
 
Kevin Davis
Join Date: Oct 2021
Posts: 2
Rep Power: 0
kdavis1521 is on a distinguished road
No it was not. This fixed my solution, thank you.
kdavis1521 is offline   Reply With Quote

Reply

Tags
pressure inlet, stagnation pressure, supersonic

Thread Tools Search this Thread
Search this Thread:

Advanced Search
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 Off
Pingbacks are On
Refbacks are On


Similar Threads
Thread Thread Starter Forum Replies Last Post
Adjuting oulet pressure till inlet pressure reaches a certain value in timestep pvpnrao OpenFOAM Running, Solving & CFD 2 September 11, 2018 10:14
"Pressure Inlet" Boundary Setup Wijaya FLUENT 15 May 18, 2016 10:08
Assign static pressure at inlet Tanjina FLUENT 0 November 3, 2013 11:34
Neumann pressure BC and velocity field Antech Main CFD Forum 0 April 25, 2006 02:15
what the result is negatif pressure at inlet chong chee nan FLUENT 0 December 29, 2001 05:13


All times are GMT -4. The time now is 19:49.