 |
 |
 |
|
|
|
[Sponsors] | ||||
October 11, 2007, 07:39
|
Aerospatiale A-Airfoil data file?
|
#1 |
|
Guest
Posts: n/a
|
Hello,
Do you know where I can find a data file for the ONERA A-Airfoil used in the LESFOIL project? Thank you. I need it to reproduce the simulations for learning. Many Thanks, Jim |
|
|
||
|
October 11, 2007, 16:49
|
Re: Aerospatiale A-Airfoil data file?
|
#2 |
|
Guest
Posts: n/a
|
These are the upper coordinate: 0.000000 0.000006
0.000685 0.006377 0.002737 0.012991 0.006152 0.019846 0.010919 0.026942 0.017025 0.034234 0.024455 0.041616 0.033187 0.048946 0.043198 0.056081 0.054459 0.062883 0.066941 0.069232 0.080609 0.075022 0.095426 0.080171 0.111351 0.084627 0.128340 0.088368 0.146346 0.091398 0.165321 0.093747 0.185213 0.095466 0.205966 0.096609 0.227524 0.097229 0.249829 0.097363 0.272818 0.097041 0.296428 0.096292 0.320596 0.095146 0.345255 0.093641 0.370336 0.091810 0.395773 0.089686 0.421494 0.087293 0.447429 0.084649 0.473507 0.081766 0.499657 0.078653 0.525807 0.075319 0.551886 0.071774 0.577821 0.068036 0.603542 0.064132 0.628978 0.060102 0.654060 0.055992 0.678718 0.051837 0.702886 0.047661 0.726497 0.043482 0.749486 0.039319 0.771790 0.035192 0.793348 0.031121 0.814102 0.027125 0.833993 0.023224 0.852968 0.019440 0.870975 0.015791 0.887964 0.012299 0.903888 0.008982 0.918705 0.005860 0.932373 0.002950 0.944855 0.000268 0.956117 -0.002173 0.966128 -0.004358 0.974860 -0.006275 0.982289 -0.007913 0.988396 -0.009264 0.993163 -0.010321 0.996577 -0.011079 0.998972 -0.011611 1.000000 -0.011840 and these the lower: 0.000000 0.000006 0.000685 -0.006083 0.002737 -0.011828 0.006152 -0.017176 0.010919 -0.022102 0.017025 -0.026594 0.024455 -0.030647 0.033187 -0.034265 0.043198 -0.037466 0.054459 -0.040292 0.066941 -0.042800 0.080609 -0.045058 0.095426 -0.047127 0.111351 -0.049056 0.128340 -0.050877 0.146346 -0.052611 0.165321 -0.054285 0.185213 -0.055918 0.205966 -0.057509 0.227524 -0.059027 0.249829 -0.060432 0.272818 -0.061688 0.296428 -0.062761 0.320596 -0.063603 0.345255 -0.064174 0.370336 -0.064456 0.395773 -0.064447 0.421494 -0.064155 0.447429 -0.063592 0.473507 -0.062763 0.499657 -0.061674 0.525807 -0.060333 0.551886 -0.058758 0.577821 -0.056977 0.603542 -0.055030 0.628978 -0.052960 0.654060 -0.050797 0.678718 -0.048564 0.702886 -0.046275 0.726497 -0.043945 0.749486 -0.041591 0.771790 -0.039228 0.793348 -0.036873 0.814102 -0.034540 0.833993 -0.032247 0.852968 -0.030012 0.870975 -0.027852 0.887964 -0.025793 0.903888 -0.023849 0.918705 -0.022033 0.932373 -0.020350 0.944855 -0.018805 0.956117 -0.017400 0.966128 -0.016143 0.974860 -0.015039 0.982289 -0.014096 0.988396 -0.013320 0.993163 -0.012713 0.996577 -0.012277 0.998972 -0.011972 1.000000 -0.011840 Bye |
|
|
|
||
|
October 12, 2007, 04:52
|
Re: Aerospatiale A-Airfoil data file?
|
#3 |
|
Guest
Posts: n/a
|
Thank you very much Marco, your help is extremely appreciated.
|
|
|
|
||
|
March 23, 2016, 02:13
|
|
#4 |
|
New Member
Hanxun Yao
Join Date: Feb 2016
Posts: 5
Rep Power: 10  |
Hi,
May I know the database of this airfoil coordinates ? Thank you |
|
|
|
|
 |
|
|
Similar Threads
|
||||
| Thread | Thread Starter | Forum | Replies | Last Post |
| [OpenFOAM.com] OpenFOAM 1.7.1 installation on LINUX UBUNTU 10.10 | electrosin | OpenFOAM Installation | 40 | May 31, 2016 05:11 |
| [swak4Foam] swak4foam building problem | GGerber | OpenFOAM Community Contributions | 54 | April 24, 2015 16:02 |
| [swak4Foam] GroovyBC the dynamic cousin of funkySetFields that lives on the suburb of the mesh | gschaider | OpenFOAM Community Contributions | 300 | October 29, 2014 18:00 |
| paraview installation woes | vex | OpenFOAM Installation | 15 | January 30, 2011 07:11 |
| How to update polyPatchbs localPoints | liu | OpenFOAM Running, Solving & CFD | 6 | December 30, 2005 17:27 |
Linear Mode
