Home > Forums > General Forums > Main CFD Forum

Experimental data for NACA 0012

Updated Threads

Reply

Search this Thread

February 26, 2014, 08:58	Experimental data for NACA 0012	#1
mag1000 New Member Manuel Join Date: Feb 2014 Posts: 2 Rep Power: 0	Hi, does anyone know where to find experimental data (i.e. cp) for the NACA 0012 airfoil at following conditions: M=0.65 Re=500,000 AOA=2° These are really unusual conditions and therefore it is really hard to find anything. I would be very grateful, if someone has some data, that is nearly at these conditions! Best regards Manuel

Reply

Tags

« 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
ABL simulation with experimental data: problems and doubts	Davide_sd	OpenFOAM Running, Solving & CFD	0	May 22, 2013 18:35
[Commercial meshers] fluentMeshToFoam multidomain mesh conversion problem	Attesz	OpenFOAM Meshing & Mesh Conversion	12	May 2, 2013 10:52
NACA 0012 FLAP experimental data	ferra89	Main CFD Forum	1	May 1, 2013 11:08
set experimental data as boundary condition	nalin	FLUENT	4	November 16, 2008 09:13
transient velocity profile with experimental data	Janneke	FLUENT	3	August 19, 2008 10:11

All times are GMT -4. The time now is 10:49.