What is the Basic Calculation of Lift Coef In Modelling 2D?? -- CFD Online Discussion Forums

October 14, 2009, 05:52	What is the Basic Calculation of FLUENT on Computing Lift Coef In Modelling 2D??	#1
teguhtf Senior Member teguh hady Join Date: Aug 2009 Location: Saga, Japan Posts: 222 Rep Power: 18	Hello All!!! I wanna find Lift coefficient of an airfoil. My drawing is 2D. Do you know the basic calculation of FLUENT in computing Lift coefficient in 2D?? Because the equation of CL = L/(qA). where L is the lift force, q is dynamic pressure, and A is planform area. If A is zero then CL is infinite. (2D has no planform area(A)) Can you tell me?? What is the Basic Calculation of FLUENT on Computing Lift Coef In Modelling 2D?? thanks teguhtf Last edited by teguhtf; October 14, 2009 at 14:19. Reason: completing

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
Thin foil analsis (sail) - Lift Coeff Problem	Kelvin	CFX	3	December 22, 2008 17:22
Lift calculation	icem-noob	CFX	1	June 23, 2008 07:37
Warning 097-	AB	Siemens	6	November 15, 2004 05:41
good basic book on turbulence modelling ?	lvlin	Main CFD Forum	4	May 29, 2002 08:31

All times are GMT -4. The time now is 03:53.