Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-naca22112-jf-500000 Airfoil,naca22112-jf Reynolds number,500000 Ncrit,9 Mach,0 Max Cl/Cd,67.6583 Max Cl/Cd alpha,9.75 Url,http://airfoiltools.com/polar/csv?polar=xf-naca22112-jf-500000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -14.750,-0.4730,0.14524,0.14292,0.0021,1.0000,0.0244 -8.500,-0.7876,0.03141,0.02619,-0.0104,1.0000,0.0242 -8.250,-0.7756,0.02865,0.02316,-0.0080,1.0000,0.0241 -8.000,-0.7617,0.02641,0.02062,-0.0056,1.0000,0.0242 -7.750,-0.7473,0.02396,0.01789,-0.0034,1.0000,0.0247 -7.500,-0.7286,0.02283,0.01677,-0.0020,1.0000,0.0252 -7.250,-0.7091,0.02240,0.01638,-0.0006,1.0000,0.0258 -7.000,-0.6904,0.02144,0.01533,0.0011,1.0000,0.0264 -6.750,-0.6716,0.02022,0.01398,0.0030,1.0000,0.0268 -6.500,-0.6524,0.01912,0.01277,0.0047,1.0000,0.0273 -6.250,-0.6331,0.01817,0.01172,0.0065,1.0000,0.0280 -6.000,-0.6139,0.01745,0.01089,0.0083,1.0000,0.0286 -5.750,-0.5854,0.01633,0.00971,0.0080,0.9987,0.0294 -5.500,-0.5488,0.01559,0.00903,0.0060,0.9960,0.0307 -5.250,-0.5110,0.01500,0.00844,0.0039,0.9935,0.0320 -5.000,-0.4752,0.01435,0.00776,0.0022,0.9896,0.0333 -4.750,-0.4369,0.01389,0.00726,0.0002,0.9860,0.0343 -4.500,-0.4004,0.01287,0.00630,-0.0019,0.9832,0.0363 -4.250,-0.3651,0.01244,0.00589,-0.0034,0.9773,0.0384 -4.000,-0.3275,0.01201,0.00545,-0.0054,0.9726,0.0403 -3.750,-0.2960,0.01133,0.00478,-0.0061,0.9643,0.0426 -3.500,-0.2623,0.01094,0.00441,-0.0072,0.9561,0.0456 -3.250,-0.2336,0.01068,0.00413,-0.0070,0.9429,0.0483 -3.000,-0.2073,0.01021,0.00365,-0.0064,0.9279,0.0524 -2.750,-0.1809,0.00996,0.00338,-0.0057,0.9111,0.0568 -2.500,-0.1556,0.00965,0.00304,-0.0048,0.8923,0.0644 -2.250,-0.1306,0.00937,0.00274,-0.0039,0.8709,0.0810 -2.000,-0.1182,0.00749,0.00224,-0.0015,0.8463,0.4441 -1.750,-0.0980,0.00694,0.00209,0.0002,0.8172,0.5745 -1.500,-0.0759,0.00667,0.00201,0.0018,0.7847,0.6534 -1.250,-0.0523,0.00654,0.00197,0.0031,0.7556,0.7106 -1.000,-0.0276,0.00646,0.00196,0.0041,0.7298,0.7562 -0.750,-0.0028,0.00644,0.00196,0.0052,0.7036,0.7959 -0.500,0.0222,0.00648,0.00199,0.0062,0.6755,0.8292 -0.250,0.0477,0.00655,0.00202,0.0072,0.6485,0.8569 0.250,0.0982,0.00679,0.00218,0.0093,0.5968,0.9055 0.500,0.1244,0.00697,0.00225,0.0100,0.5696,0.9207 0.750,0.1520,0.00715,0.00231,0.0104,0.5408,0.9316 1.000,0.1792,0.00733,0.00238,0.0108,0.5131,0.9426 1.250,0.2095,0.00754,0.00247,0.0106,0.4857,0.9508 1.500,0.2397,0.00776,0.00255,0.0103,0.4575,0.9587 1.750,0.2740,0.00800,0.00266,0.0090,0.4264,0.9641 2.000,0.3054,0.00825,0.00276,0.0083,0.3951,0.9710 2.250,0.3443,0.00852,0.00288,0.0059,0.3618,0.9734 2.500,0.3824,0.00880,0.00300,0.0037,0.3288,0.9765 2.750,0.4174,0.00910,0.00313,0.0020,0.2961,0.9810 3.000,0.4535,0.00941,0.00327,0.0001,0.2633,0.9844 3.250,0.4915,0.00971,0.00342,-0.0022,0.2349,0.9870 3.500,0.5281,0.01002,0.00359,-0.0043,0.2137,0.9902 3.750,0.5634,0.01030,0.00377,-0.0060,0.1988,0.9938 4.000,0.6015,0.01051,0.00393,-0.0083,0.1873,0.9959 4.250,0.6387,0.01075,0.00412,-0.0105,0.1785,0.9984 4.500,0.6713,0.01096,0.00429,-0.0117,0.1718,1.0000 4.750,0.6933,0.01122,0.00450,-0.0107,0.1661,1.0000 5.000,0.7161,0.01135,0.00466,-0.0098,0.1620,1.0000 5.250,0.7383,0.01155,0.00484,-0.0089,0.1576,1.0000 5.500,0.7596,0.01186,0.00511,-0.0077,0.1531,1.0000 5.750,0.7816,0.01208,0.00536,-0.0067,0.1500,1.0000 6.000,0.8039,0.01226,0.00556,-0.0056,0.1467,1.0000 6.250,0.8257,0.01248,0.00579,-0.0046,0.1432,1.0000 6.500,0.8465,0.01283,0.00610,-0.0033,0.1397,1.0000 6.750,0.8674,0.01318,0.00647,-0.0021,0.1365,1.0000 7.000,0.8899,0.01337,0.00670,-0.0011,0.1338,1.0000 7.250,0.9120,0.01360,0.00697,-0.0001,0.1309,1.0000 7.500,0.9337,0.01388,0.00725,0.0010,0.1279,1.0000 7.750,0.9535,0.01440,0.00773,0.0023,0.1241,1.0000 8.000,0.9758,0.01465,0.00805,0.0033,0.1219,1.0000 8.250,0.9986,0.01487,0.00832,0.0042,0.1192,1.0000 8.500,1.0211,0.01511,0.00859,0.0051,0.1163,1.0000 8.750,1.0429,0.01545,0.00892,0.0060,0.1133,1.0000 9.000,1.0629,0.01602,0.00949,0.0072,0.1099,1.0000 9.250,1.0866,0.01620,0.00976,0.0078,0.1076,1.0000 9.500,1.1100,0.01644,0.01005,0.0085,0.1046,1.0000 9.750,1.1326,0.01674,0.01036,0.0092,0.1016,1.0000 10.000,1.1522,0.01737,0.01098,0.0103,0.0980,1.0000 10.250,1.1762,0.01756,0.01127,0.0108,0.0956,1.0000 10.500,1.1995,0.01782,0.01159,0.0114,0.0925,1.0000 10.750,1.2212,0.01820,0.01197,0.0121,0.0892,1.0000 11.000,1.2409,0.01878,0.01257,0.0131,0.0860,1.0000 11.250,1.2637,0.01906,0.01295,0.0137,0.0831,1.0000 11.500,1.2851,0.01944,0.01336,0.0144,0.0798,1.0000 11.750,1.3021,0.02016,0.01406,0.0156,0.0761,1.0000 12.000,1.3241,0.02048,0.01450,0.0162,0.0733,1.0000 12.250,1.3436,0.02096,0.01502,0.0171,0.0700,1.0000 12.500,1.3578,0.02178,0.01582,0.0186,0.0665,1.0000 12.750,1.3765,0.02223,0.01640,0.0196,0.0638,1.0000 13.000,1.3906,0.02287,0.01708,0.0212,0.0607,1.0000 13.250,1.3992,0.02386,0.01808,0.0233,0.0577,1.0000 13.500,1.4138,0.02455,0.01888,0.0246,0.0550,1.0000 13.750,1.4240,0.02555,0.01992,0.0261,0.0522,1.0000 14.000,1.4293,0.02694,0.02136,0.0277,0.0496,1.0000 14.250,1.4403,0.02802,0.02256,0.0287,0.0472,1.0000 14.500,1.4462,0.02957,0.02416,0.0297,0.0449,1.0000 14.750,1.4458,0.03176,0.02641,0.0305,0.0428,1.0000 15.000,1.4527,0.03350,0.02828,0.0308,0.0410,1.0000 15.250,1.4546,0.03583,0.03071,0.0308,0.0393,1.0000 15.500,1.4507,0.03900,0.03395,0.0303,0.0378,1.0000 15.750,1.4429,0.04286,0.03793,0.0291,0.0365,1.0000 16.000,1.4407,0.04629,0.04151,0.0278,0.0354,1.0000 16.250,1.4339,0.05046,0.04582,0.0261,0.0343,1.0000 16.500,1.4218,0.05551,0.05100,0.0237,0.0335,1.0000 16.750,1.4049,0.06139,0.05700,0.0209,0.0329,1.0000 17.000,1.3835,0.06807,0.06381,0.0176,0.0324,1.0000 17.250,1.3589,0.07531,0.07118,0.0141,0.0321,1.0000 17.500,1.3327,0.08297,0.07896,0.0104,0.0318,1.0000