Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-sc20706-il-50000-n5 Airfoil,sc20706-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,25.2926 Max Cl/Cd alpha,2 Url,http://airfoiltools.com/polar/csv?polar=xf-sc20706-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.500,-0.4817,0.10788,0.10088,-0.0133,1.0000,0.1244 -10.250,-0.5012,0.09868,0.09173,-0.0207,1.0000,0.0657 -9.750,-0.6046,0.09807,0.09080,-0.0209,1.0000,0.0512 -9.500,-0.6040,0.09385,0.08663,-0.0218,1.0000,0.0509 -9.250,-0.6036,0.08942,0.08225,-0.0234,1.0000,0.0506 -9.000,-0.6027,0.08450,0.07737,-0.0266,1.0000,0.0502 -8.750,-0.6014,0.07960,0.07248,-0.0298,1.0000,0.0497 -8.500,-0.5993,0.07467,0.06751,-0.0329,1.0000,0.0492 -8.250,-0.5952,0.06965,0.06241,-0.0360,1.0000,0.0486 -8.000,-0.5883,0.06450,0.05712,-0.0391,1.0000,0.0477 -7.750,-0.5775,0.05920,0.05158,-0.0425,1.0000,0.0468 -7.500,-0.5621,0.05385,0.04588,-0.0459,1.0000,0.0459 -7.250,-0.5416,0.04865,0.04020,-0.0492,1.0000,0.0453 -7.000,-0.5169,0.04387,0.03487,-0.0521,1.0000,0.0451 -6.750,-0.4892,0.03961,0.03001,-0.0545,1.0000,0.0453 -6.500,-0.4600,0.03592,0.02565,-0.0562,1.0000,0.0461 -6.250,-0.4301,0.03303,0.02212,-0.0574,1.0000,0.0494 -6.000,-0.4020,0.03048,0.01916,-0.0580,1.0000,0.0535 -5.750,-0.3755,0.02839,0.01683,-0.0579,1.0000,0.0566 -5.500,-0.3498,0.02657,0.01475,-0.0570,1.0000,0.0601 -5.250,-0.3250,0.02505,0.01303,-0.0560,1.0000,0.0667 -5.000,-0.2998,0.02383,0.01158,-0.0553,1.0000,0.0777 -4.750,-0.2741,0.02243,0.01016,-0.0549,1.0000,0.0876 -4.500,-0.2447,0.02108,0.00886,-0.0558,1.0000,0.1134 -4.250,-0.2043,0.01842,0.00729,-0.0605,1.0000,0.2780 -4.000,-0.1903,0.01753,0.00797,-0.0562,1.0000,0.6256 -3.750,-0.1784,0.01784,0.00831,-0.0510,1.0000,0.7153 -3.500,-0.1736,0.01812,0.00856,-0.0439,1.0000,0.7755 -3.250,-0.1677,0.01812,0.00851,-0.0374,1.0000,0.8203 -3.000,-0.1562,0.01788,0.00814,-0.0330,1.0000,0.8538 -2.750,-0.1409,0.01749,0.00762,-0.0298,1.0000,0.8807 -2.500,-0.1214,0.01706,0.00704,-0.0279,1.0000,0.9026 -2.250,-0.0986,0.01663,0.00648,-0.0270,1.0000,0.9223 -2.000,-0.0735,0.01622,0.00591,-0.0266,1.0000,0.9421 -1.750,-0.0446,0.01585,0.00545,-0.0273,1.0000,0.9629 -1.500,-0.0177,0.01552,0.00509,-0.0277,1.0000,0.9931 -1.250,0.0127,0.01548,0.00497,-0.0291,1.0000,1.0000 -1.000,0.0452,0.01553,0.00495,-0.0310,1.0000,1.0000 -0.750,0.0778,0.01561,0.00500,-0.0327,1.0000,1.0000 -0.500,0.1102,0.01571,0.00510,-0.0345,1.0000,1.0000 -0.250,0.1424,0.01584,0.00527,-0.0361,1.0000,1.0000 0.000,0.1743,0.01599,0.00550,-0.0376,1.0000,1.0000 0.250,0.2058,0.01616,0.00577,-0.0390,1.0000,1.0000 0.500,0.2370,0.01635,0.00609,-0.0403,1.0000,1.0000 0.750,0.2678,0.01657,0.00648,-0.0415,1.0000,1.0000 1.000,0.2981,0.01682,0.00698,-0.0426,1.0000,1.0000 1.250,0.3281,0.01709,0.00750,-0.0436,1.0000,1.0000 1.500,0.3577,0.01739,0.00810,-0.0446,1.0000,1.0000 1.750,0.3870,0.01772,0.00880,-0.0454,1.0000,1.0000 2.000,0.5013,0.01982,0.00808,-0.0574,0.1595,1.0000 2.250,0.5299,0.02173,0.00957,-0.0578,0.1030,1.0000 2.500,0.5607,0.02315,0.01106,-0.0584,0.0806,1.0000 2.750,0.5937,0.02483,0.01290,-0.0590,0.0714,1.0000 3.000,0.6254,0.02657,0.01475,-0.0597,0.0607,1.0000 3.250,0.6581,0.02849,0.01701,-0.0599,0.0551,1.0000 3.500,0.6895,0.03080,0.01959,-0.0601,0.0522,1.0000 3.750,0.7183,0.03343,0.02243,-0.0603,0.0493,1.0000 4.000,0.7461,0.03609,0.02567,-0.0599,0.0459,1.0000 4.250,0.7722,0.03903,0.02922,-0.0593,0.0434,1.0000 4.500,0.7960,0.04252,0.03336,-0.0585,0.0429,1.0000 4.750,0.8173,0.04633,0.03773,-0.0576,0.0429,1.0000 5.000,0.8359,0.05046,0.04241,-0.0567,0.0431,1.0000 5.250,0.8518,0.05489,0.04733,-0.0559,0.0436,1.0000 5.500,0.8652,0.05954,0.05242,-0.0552,0.0442,1.0000 5.750,0.8762,0.06435,0.05760,-0.0547,0.0451,1.0000 6.000,0.8849,0.06926,0.06279,-0.0545,0.0460,1.0000 6.250,0.8915,0.07423,0.06799,-0.0545,0.0467,1.0000 6.500,0.8960,0.07923,0.07319,-0.0547,0.0472,1.0000 6.750,0.8985,0.08428,0.07840,-0.0551,0.0475,1.0000 7.000,0.8991,0.08936,0.08361,-0.0558,0.0477,1.0000 7.250,0.8988,0.09443,0.08877,-0.0566,0.0480,1.0000 7.500,0.8989,0.09953,0.09392,-0.0574,0.0483,1.0000 8.000,0.7336,0.10502,0.09977,-0.0545,0.0578,1.0000 8.250,0.7388,0.10958,0.10432,-0.0537,0.0608,1.0000