Airfoil Pressure coefficients don't match! -- CFD Online Discussion Forums

August 17, 2009, 05:57

Airfoil Pressure coefficients don't match!

Kappe

New Member

Kappe

Join Date: Aug 2009

Posts: 8

Rep Power: 16

Hi,
I meshed a NACA0012, C-grid about 20K node points. Used K-Epsilon viscous model. Compared it with Abbott values. Doesn't match satisfactorily.
Please suggest where i would've gone wrong.

Attached Images

Graph.JPG (25.7 KB, 19 views)

August 18, 2009, 04:58		#2
Kappe New Member Kappe Join Date: Aug 2009 Posts: 8 Rep Power: 16	I have also checked the y+ values which are between 30-60

« Previous Thread | Next Thread »

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
"Pressure Inlet" Boundary Setup	Wijaya	FLUENT	15	May 18, 2016 10:08
Pressure enigma.	Sara	Main CFD Forum	22	July 30, 2009 04:46
Q: how to draw pressure distribution on an airfoil	mario	FLUENT	0	February 9, 2007 21:45
Terrible Mistake In Fluid Dynamics History	Abhi	Main CFD Forum	12	July 8, 2002 09:11
pressure. lift and drag coefficients	waqar mahboob	Main CFD Forum	0	July 25, 1998 03:34

All times are GMT -4. The time now is 22:27.