 |
 |
 |
|
|
|
[Sponsors] | ||||
April 30, 2013, 11:14
|
NACA 0012 FLAP experimental data
|
#1 |
|
New Member
Join Date: Apr 2013
Posts: 7
Rep Power: 13  |
Hello everyone,
I'm looking for experimental Cp, Cl, Cd data for the NACA 0012 airfoil to validate simulations that I've run. The Reynolds number is 1e6 and the simulations use 45° -45° flap deflections. Does anyone have any suggestions? Thanks |
|
|
|
|
|
May 1, 2013, 12:08
|
|
#2 |
|
Senior Member
Lefteris
Join Date: Oct 2011
Location: UK
Posts: 341
Rep Power: 16 |
1. Theory of wing sections
2. nasa's website
__________________
Lefteris |
|
|
|
|
|
 |
|
|
Similar Threads
|
||||
| Thread | Thread Starter | Forum | Replies | Last Post |
| Step Changes in Roughness Experimental Data | syler3321 | Main CFD Forum | 0 | October 20, 2010 01:45 |
| NACA 0018 Experimental Data | andygir | Main CFD Forum | 1 | October 15, 2010 13:03 |
| NACA 0012 data | pixie | Main CFD Forum | 3 | August 5, 2009 04:01 |
| transient velocity profile with experimental data | Janneke | FLUENT | 3 | August 19, 2008 11:11 |
| NACA 6A-series airfoil data | Shereef | Main CFD Forum | 2 | February 15, 1999 06:25 |
Linear Mode
