NACA 0012 airfoil analysis -- CFD Online Discussion Forums

June 29, 2018, 14:51	NACA 0012 airfoil analysis	#1
Rookier New Member Ramesh Join Date: Jun 2018 Posts: 8 Rep Power: 8	Hi, I have done my airfoil NACA0012 domain mesh and I am about to do analysis.The experiment is validation of subsonic flow past an airfoil.I need some help regarding the parameters to be set.If anybody is willing to help,please guide me.I have few questions.You can message me as well. Thank you

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
Fluent analysis for an airfoil	pratikvn	FLUENT	2	October 7, 2014 14:15
2D FFD Optimization	RLangtry	SU2	2	August 5, 2014 10:48
NACA 0012 - M 0.7 - 4 º - Residual Problems	leo_NM	FLUENT	0	October 8, 2013 18:15
Comparison the airfoil 0012 experimental result and simulation result	harrislcy	FLUENT	30	August 29, 2013 11:27
problem with stall in naca 0012 airfoil	thanos	FLUENT	0	February 18, 2010 12:36

All times are GMT -4. The time now is 01:42.