CFD Online Logo CFD Online URL
Home > Forums > FLUENT

simulation of airfoil at high AOA

Register Blogs Members List Search Today's Posts Mark Forums Read

LinkBack Thread Tools Display Modes
Old   January 26, 2007, 22:34
Default simulation of airfoil at high AOA
Posts: n/a
What are the empirical ways to improve the convergence efficiency and accuracy of cl and cd when simulating an airfoil at high angle of attack ? I can think of packing more grids onto suction side BL region as one way. Is there anything else that might be helpful? thanks!
  Reply With Quote


Thread Tools
Display Modes

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 On
Pingbacks are On
Refbacks are On

Similar Threads
Thread Thread Starter Forum Replies Last Post
Simulating flow past airfoil with different AOA ramin FLUENT 4 April 22, 2015 13:09
Comparison the airfoil 0012 experimental result and simulation result harrislcy FLUENT 30 August 29, 2013 10:27
result on airfoil wortmann fx63-137 simulation jdfortune FLUENT 5 January 31, 2011 20:26
Simulation of transonic flow over NACA0012 airfoil MSc Student Siemens 2 August 9, 2006 13:49
Simulating flow past airfoil with different AOA Quarkz Main CFD Forum 2 January 6, 2006 11:56

All times are GMT -4. The time now is 09:42.