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

Problem for Mass flow average in Post...

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   October 25, 2005, 02:35
Default Problem for Mass flow average in Post...
  #1
ST
Guest
 
Posts: n/a
I recently run a transient simulation for my problem and wish to take mass flow averaged total pressure at each time period. However, I can't actually get the mass flow average value from the caculator when I use the minimal output option for the transient results. I did choose pressure,total pressure,velocity,absolute pressure in the output variable list. It worked okay when I click everything in the output control but it takes lots of space.

Just wonder if anyone know what variables I should add in the output list to get the mass flow averaged values of a plane. Thanks....
  Reply With Quote

Old   October 25, 2005, 02:36
Default Re: Problem for Mass flow average in Post...
  #2
ST
Guest
 
Posts: n/a
I'm using CFX5.7.1 with SST model at the moment.
  Reply With Quote

Old   October 27, 2005, 14:35
Default Re: Problem for Mass flow average in Post...
  #3
Robin
Guest
 
Posts: n/a
Hi ST,

If you have pressure, then absolute pressure is redundant since it is simply 'pressure + reference pressure'. You will need Density to calculate the mass flow rate.

Normally when you calculate mass flow, Post will use the integration point (ip) flows written to the RES file by the solver. This is the most accurate, since the details on how the solver computes the flows at each subface are complicated. When you write a partial results file, the ip flows are not included. The closest estimate is to calculate the area integral of density times normal velocity, thus:

Vnorm = Normal X * Velocity u + Normal Y * Velocity w + Normal Z * Velocity w
rho = xxx [kg/s] #or write density to .trn if it is variable
mass flow = areaInt(rho*Vnorm)@Plane 1

Note that this is only an approximation to the actual mass flow, since it assume contant mass flow across the face, which is not what the solver is calculating.

Regards,
Robin
  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
flow past abdominal aorta. Complex BC problem. ziemowitzima OpenFOAM Running, Solving & CFD 1 July 26, 2022 06:12
Axisymmetric Vs 2D Flow problem nikhil FLUENT 0 March 30, 2010 00:52
A problem: reversed flow in ... on outflow. vandadt FLUENT 10 November 10, 2009 17:40
Can 'shock waves' occur in viscous fluid flows? diaw Main CFD Forum 104 February 16, 2006 06:44
problem in mass flow boundary bapi CFX 2 December 3, 2001 23:47


All times are GMT -4. The time now is 18:07.