 |
 |
 |
|
|
|
[Sponsors] | ||||
Experimental Data for Flow Behind a NACA 0012 Wingtip |
 |
|
|
LinkBack | Thread Tools | Search this Thread | Display Modes |
August 30, 2017, 18:34
|
Experimental Data for Flow Behind a NACA 0012 Wingtip
|
#1 |
|
New Member
Argyris Apost
Join Date: Nov 2014
Posts: 7
Rep Power: 12  |
Hello everyone,
I want to validate my CFD results of a NACA 0012 Wingtip vortex with the experimental results provided by NASA in the following link: https://turbmodels.larc.nasa.gov/Oth...p0012_exp.html However, i dont have a clue of plotting the provided data (.b11 and .dat files). If anyone can give me any advice, it would be extremely helpful. Thank you in advance, Argyris Apostolidis |
|
|
|
|
|
| Tags |
| experimental data, visualization |
|
|
Similar Threads
|
||||
| Thread | Thread Starter | Forum | Replies | Last Post |
| experimental lift and drag coefficients data for the NACA 0012? | Seto | FLUENT | 0 | March 23, 2017 17:15 |
| experimental data for profiled NACA 4digit airfoils at Re=10000 and below | noorul | Main CFD Forum | 0 | May 31, 2013 03:12 |
| NACA 0018 Experimental Data | andygir | Main CFD Forum | 1 | October 15, 2010 13:03 |
| Naca 0012 data | cfang | Main CFD Forum | 0 | August 20, 2009 10:16 |
| NACA 0012 data | pixie | Main CFD Forum | 3 | August 5, 2009 04:01 |
Linear Mode
