Coordonnées du profil
|
Résultats XFoil 10000 15000 20000 30000 40000 50000 60000 |
incidence = 1°
|
Re Cz Cx Cm x/c 10000 0.10670 0.03506 -0.01800 0.41776 15000 0.10860 0.02926 -0.01800 0.41500 20000 0.10970 0.02586 -0.01810 0.41434 30000 0.12000 0.02181 -0.02000 0.41616 40000 0.12220 0.01949 -0.02040 0.41650 50000 0.12400 0.01794 -0.02080 0.41734 60000 0.12520 0.01681 -0.02110 0.41816 |
incidence = 3°
|
Re Cz Cx Cm x/c 10000 0.26630 0.03810 -0.01290 0.29815 15000 0.26990 0.03235 -0.01320 0.29867 20000 0.27200 0.02899 -0.01340 0.29906 30000 0.28510 0.02511 -0.01660 0.30804 40000 0.28770 0.02291 -0.01730 0.30996 50000 0.28920 0.02147 -0.01790 0.31174 60000 0.29000 0.02046 -0.01840 0.31330 |
incidence = 6°
|
Re Cz Cx Cm x/c 10000 0.4398 0.0522 -0.0124 0.2782 15000 0.4324 0.0478 -0.0149 0.2845 20000 0.8049 0.0497 -0.0355 0.2941 30000 0.8196 0.0458 -0.0340 0.2915 40000 0.8195 0.0418 -0.0348 0.2925 50000 0.8223 0.0388 -0.0355 0.2932 60000 0.8211 0.0383 -0.0365 0.2945 |
incidence = 8°
|
Re Cz Cx Cm x/c 10000 0.45640 0.08018 -0.03100 0.17963 15000 0.76570 0.09203 -0.05190 0.18034 20000 0.84580 0.08322 -0.03620 0.20615 30000 0.84450 0.08182 -0.02740 0.21677 40000 0.88540 0.08245 -0.02540 0.22063 50000 0.88130 0.08010 -0.02400 0.22213 60000 0.90230 0.06287 -0.02190 0.22524 |
