Coordonnées du profil
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Résultats XFoil 5000 10000 15000 20000 25000 30000 35000 40000 45000 50000 55000 60000 |
Re Cl Cd Cm x/c 5000 0.2970 0.06185 -0.0308 0.3527 10000 0.2673 0.05041 -0.0271 0.3505 15000 0.2507 0.04651 -0.0267 0.3556 20000 0.2429 0.04494 -0.0277 0.3630 25000 0.3312 0.04626 -0.0466 0.3898 30000 0.4158 0.04402 -0.0585 0.3901 35000 0.5369 0.04164 -0.0738 0.3871 40000 0.5551 0.03716 -0.0726 0.3805 45000 0.6549 0.03019 -0.0815 0.3743 50000 0.7357 0.02443 -0.0893 0.3713 55000 0.7468 0.02211 -0.0889 0.3690 60000 0.7552 0.02032 -0.0887 0.3674 
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Re Cl Cd Cm x/c 5000 0.3679 0.07293 -0.0293 0.3286 10000 0.3380 0.06263 -0.0273 0.3298 15000 0.3258 0.05952 -0.0282 0.3356 20000 0.3218 0.05877 -0.0305 0.3437 25000 0.4959 0.06225 -0.0614 0.3730 30000 0.6406 0.05744 -0.0728 0.3632 35000 0.6929 0.04919 -0.0707 0.3518 40000 0.8532 0.03855 -0.0813 0.3452 45000 0.8761 0.03342 -0.0809 0.3424 50000 0.9036 0.02930 -0.0817 0.3405 55000 0.9292 0.02591 -0.0830 0.3394 60000 0.9458 0.02372 -0.0839 0.3388 
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