Drag and Lift coefficient calculation -- CFD Online Discussion Forums

February 5, 2010, 06:41	Drag and Lift coefficient calculation	#1
viraj New Member viraj Join Date: Feb 2010 Posts: 2 Rep Power: 0	HI I am solving a problem of flow past a circular cylinder using ghost cell Immersed boundary method. I need to calculate Cd and Cl values over the cylinder. Can anyone guide me on this??? Currently i am integrating respective components of pressure and shear stress over the cylinder but not getting the correct values. Re No=100. I require Cd (avg) and Cl(rms) values. thanks in advance viraj Last edited by viraj; February 5, 2010 at 07:37.

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 Forum Rules

Similar Threads
Thread	Thread Starter	Forum	Replies	Last Post
Lift and drag calculation	Franny	CFX	16	November 27, 2019 14:47
lift & drag coefficient on airfoil	n. natik	FLUENT	8	March 31, 2015 20:02
Drag coefficient & Lift coefficient??	mehrdadeng	CFX	15	December 9, 2009 22:49
Automotive test case	vinz	OpenFOAM Running, Solving & CFD	98	October 27, 2008 09:43
drag and lift coefficient	Noé	Siemens	5	July 13, 2004 11:21

All times are GMT -4. The time now is 19:59.