Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-naca001035-il-100000-n5 Airfoil,naca001035-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,27.1275 Max Cl/Cd alpha,2.75 Url,http://airfoiltools.com/polar/csv?polar=xf-naca001035-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.500,-0.4781,0.09346,0.08872,-0.0380,1.0000,0.0211 -10.250,-0.4855,0.08885,0.08415,-0.0389,1.0000,0.0207 -10.000,-0.4952,0.08377,0.07911,-0.0404,1.0000,0.0203 -9.750,-0.5081,0.07808,0.07344,-0.0429,1.0000,0.0201 -9.250,-0.6367,0.07904,0.07399,-0.0413,1.0000,0.0210 -9.000,-0.6541,0.07618,0.07111,-0.0384,1.0000,0.0207 -8.750,-0.6730,0.07373,0.06863,-0.0342,1.0000,0.0205 -8.500,-0.6883,0.07093,0.06577,-0.0302,1.0000,0.0202 -8.250,-0.7015,0.06803,0.06279,-0.0262,1.0000,0.0198 -8.000,-0.7127,0.06504,0.05968,-0.0221,1.0000,0.0194 -7.750,-0.7217,0.06199,0.05648,-0.0179,1.0000,0.0190 -7.500,-0.7285,0.05887,0.05318,-0.0137,1.0000,0.0186 -7.250,-0.7331,0.05570,0.04979,-0.0094,1.0000,0.0182 -7.000,-0.7353,0.05250,0.04634,-0.0052,1.0000,0.0177 -6.750,-0.7352,0.04930,0.04284,-0.0010,1.0000,0.0173 -6.500,-0.7326,0.04611,0.03933,0.0032,1.0000,0.0170 -6.250,-0.7275,0.04299,0.03583,0.0071,1.0000,0.0167 -6.000,-0.7194,0.04002,0.03247,0.0108,1.0000,0.0166 -5.750,-0.7085,0.03743,0.02947,0.0141,1.0000,0.0173 -5.500,-0.6948,0.03501,0.02661,0.0170,1.0000,0.0184 -5.250,-0.6781,0.03260,0.02374,0.0196,1.0000,0.0192 -5.000,-0.6582,0.03020,0.02090,0.0218,1.0000,0.0195 -4.750,-0.6351,0.02801,0.01826,0.0233,1.0000,0.0200 -4.500,-0.6103,0.02612,0.01604,0.0245,1.0000,0.0208 -4.250,-0.5868,0.02444,0.01418,0.0255,1.0000,0.0232 -4.000,-0.5665,0.02314,0.01284,0.0269,1.0000,0.0263 -3.750,-0.5477,0.02195,0.01153,0.0288,1.0000,0.0289 -3.500,-0.5305,0.02096,0.01041,0.0308,1.0000,0.0337 -3.250,-0.5127,0.02015,0.00948,0.0328,1.0000,0.0410 -3.000,-0.4948,0.01926,0.00854,0.0346,1.0000,0.0573 -2.750,-0.4789,0.01766,0.00773,0.0365,1.0000,0.1956 -2.500,-0.3079,0.01938,0.01180,0.0143,1.0000,0.9494 -2.250,-0.2746,0.01938,0.01156,0.0126,1.0000,0.9572 -2.000,-0.2412,0.01936,0.01134,0.0108,1.0000,0.9644 -1.750,-0.2049,0.01933,0.01111,0.0084,1.0000,0.9706 -1.500,-0.1714,0.01933,0.01096,0.0065,1.0000,0.9778 -1.250,-0.1355,0.01925,0.01075,0.0040,1.0000,0.9827 -1.000,-0.1032,0.01921,0.01062,0.0021,1.0000,0.9880 -0.750,-0.0700,0.01915,0.01050,0.0001,1.0000,0.9925 -0.500,-0.0372,0.01912,0.01041,-0.0019,1.0000,0.9969 -0.250,-0.0101,0.01909,0.01037,-0.0027,1.0000,1.0000 0.000,0.0000,0.01908,0.01035,0.0000,1.0000,1.0000 0.250,0.0101,0.01909,0.01037,0.0027,1.0000,1.0000 0.500,0.0372,0.01911,0.01041,0.0019,0.9969,1.0000 0.750,0.0699,0.01915,0.01050,-0.0001,0.9926,1.0000 1.000,0.1031,0.01921,0.01062,-0.0021,0.9880,1.0000 1.250,0.1355,0.01925,0.01075,-0.0039,0.9827,1.0000 1.500,0.1713,0.01932,0.01095,-0.0064,0.9779,1.0000 1.750,0.2048,0.01933,0.01110,-0.0084,0.9706,1.0000 2.000,0.2412,0.01936,0.01134,-0.0108,0.9645,1.0000 2.250,0.2746,0.01937,0.01156,-0.0126,0.9572,1.0000 2.500,0.3079,0.01937,0.01180,-0.0143,0.9494,1.0000 2.750,0.4788,0.01765,0.00773,-0.0365,0.1959,1.0000 3.000,0.4947,0.01925,0.00854,-0.0346,0.0574,1.0000 3.250,0.5126,0.02015,0.00947,-0.0327,0.0410,1.0000 3.500,0.5304,0.02096,0.01041,-0.0308,0.0337,1.0000 3.750,0.5476,0.02195,0.01153,-0.0288,0.0289,1.0000 4.000,0.5664,0.02313,0.01283,-0.0269,0.0263,1.0000 4.250,0.5867,0.02444,0.01418,-0.0255,0.0232,1.0000 4.500,0.6102,0.02612,0.01604,-0.0245,0.0208,1.0000 4.750,0.6350,0.02801,0.01826,-0.0233,0.0200,1.0000 5.000,0.6581,0.03020,0.02089,-0.0217,0.0195,1.0000 5.250,0.6780,0.03259,0.02374,-0.0196,0.0192,1.0000 5.500,0.6948,0.03500,0.02660,-0.0170,0.0184,1.0000 5.750,0.7085,0.03742,0.02945,-0.0141,0.0173,1.0000 6.000,0.7194,0.04002,0.03246,-0.0108,0.0166,1.0000 6.250,0.7274,0.04298,0.03582,-0.0071,0.0167,1.0000 6.500,0.7326,0.04611,0.03932,-0.0032,0.0170,1.0000 6.750,0.7352,0.04929,0.04283,0.0010,0.0173,1.0000 7.000,0.7353,0.05250,0.04633,0.0052,0.0177,1.0000 7.250,0.7331,0.05569,0.04978,0.0095,0.0182,1.0000 7.500,0.7285,0.05887,0.05317,0.0137,0.0186,1.0000 7.750,0.7217,0.06199,0.05648,0.0180,0.0190,1.0000 8.000,0.7127,0.06504,0.05968,0.0221,0.0194,1.0000 8.250,0.7016,0.06802,0.06278,0.0262,0.0198,1.0000 8.500,0.6885,0.07092,0.06577,0.0302,0.0202,1.0000 8.750,0.6732,0.07373,0.06863,0.0341,0.0205,1.0000 9.000,0.6543,0.07619,0.07112,0.0383,0.0207,1.0000 9.250,0.6370,0.07905,0.07400,0.0413,0.0210,1.0000 9.500,0.5249,0.07259,0.06794,0.0448,0.0199,1.0000 9.750,0.5077,0.07792,0.07328,0.0429,0.0201,1.0000 10.000,0.4948,0.08361,0.07894,0.0404,0.0203,1.0000 10.250,0.4851,0.08870,0.08400,0.0389,0.0207,1.0000