CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > Main CFD Forum

Search for cd and cl experimental results of NACA 0012

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

Reply
 
LinkBack Thread Tools Display Modes
Old   April 15, 2012, 15:22
Default Search for cd and cl experimental results of NACA 0012
  #1
spk
Member
 
Join Date: Aug 2009
Posts: 67
Rep Power: 8
spk is on a distinguished road
Hi guys,

I search for cl and cd experimental results for airfoil naca 0012 for Re=3.0E06. I have Abbott's book, but i can't distinguish all the points for this Reynolds number, especially for cl.
Please help!!

spk
spk is offline   Reply With Quote

Old   April 15, 2012, 19:00
Default
  #2
agd
Senior Member
 
Join Date: Jul 2009
Posts: 191
Rep Power: 8
agd is on a distinguished road
Google

http://turbmodels.larc.nasa.gov/naca0012_val.html

First result for a search on "lift coefficient NACA0012 3 million"
agd is offline   Reply With Quote

Old   April 16, 2012, 07:49
Default
  #3
spk
Member
 
Join Date: Aug 2009
Posts: 67
Rep Power: 8
spk is on a distinguished road
Thanks a lot!
I search for accurate experimental data of cl and cd, like a table with the values of cl and cd!
spk is offline   Reply With Quote

Old   April 17, 2012, 14:28
Default
  #4
spk
Member
 
Join Date: Aug 2009
Posts: 67
Rep Power: 8
spk is on a distinguished road
Quote:
Originally Posted by agd View Post
Google

http://turbmodels.larc.nasa.gov/naca0012_val.html

First result for a search on "lift coefficient NACA0012 3 million"
These results are for Re=6E06
spk is offline   Reply With Quote

Reply

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



All times are GMT -4. The time now is 10:43.