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

The two drag contributions

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   April 28, 2001, 13:33
Default The two drag contributions
  #1
Hakeem
Guest
 
Posts: n/a
Hi everybody ...

As most of you are aware, for creeping (slow) flow of Newtonian fluid moving over a sphere the ratio of pressure coefficient to viscous coefficient should be ~ 0.5. Unfortunately, when I use Fluent 5.3, it is not the case. The total coefficient is right, namely, for Re = 0.01, the total drag coefficient should be ~ 2400. I got it 2400.8. However the ratio of pressure coefficient to viscous coefficient is 640.66629/1760.1434 = 0.36. Could anyone think of possible reason.
  Reply With Quote

Old   April 28, 2001, 15:08
Default Re: The two drag contributions
  #2
John C. Chien
Guest
 
Posts: n/a
(1). Ask the code vendor whether what you are getting is consistent with the code you are using. (2). If they think, you are wrong, then ask them to show you how to get the right answer using the code. (3). We are not here to speculate reasons why you think you are not getting the right answer. (that is, a right answer from the code by you could be the wrong answer to the problem.) (4). There are endless reasons which could lead to such solution, mesh size, mesh distribution, not enough mesh points(cells), accuracy of numerical algorithm, convergence, location of boundary conditions, treatment of boundary conditions, etc... (5). Even the post-processing (graphic and derived variables) can give you headache from time to time.
  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
Pressure drag, friction drag and total drag? Cheng CFX 9 January 26, 2024 13:46
formula used for drag force? kamma Main CFD Forum 0 April 2, 2010 10:21
Drag coefficient for parcels in dieselFoam sebastian_vogl OpenFOAM Running, Solving & CFD 5 December 31, 2008 12:19
Drag formulation REMY FLUENT 0 March 10, 2002 14:05
Inviscid Drag at subsonic, subcritical Mach # Axel Rohde Main CFD Forum 1 November 19, 2001 12:19


All times are GMT -4. The time now is 11:19.