Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-mh30-il-50000-n5 Airfoil,mh30-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,35.7193 Max Cl/Cd alpha,5 Url,http://www.airfoiltools.com/polar/csv?polar=xf-mh30-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.750,-0.4930,0.11274,0.10564,-0.0126,1.0000,0.0477 -9.500,-0.4885,0.10873,0.10168,-0.0136,1.0000,0.0460 -9.250,-0.4854,0.10471,0.09771,-0.0151,1.0000,0.0434 -8.750,-0.4924,0.09458,0.08776,-0.0236,1.0000,0.0368 -8.500,-0.4891,0.09081,0.08404,-0.0242,1.0000,0.0362 -8.250,-0.4902,0.08653,0.07984,-0.0265,1.0000,0.0361 -8.000,-0.4905,0.08266,0.07605,-0.0280,1.0000,0.0355 -7.750,-0.4922,0.07813,0.07159,-0.0310,1.0000,0.0351 -7.500,-0.4920,0.07357,0.06705,-0.0337,1.0000,0.0346 -7.250,-0.4913,0.06904,0.06251,-0.0359,1.0000,0.0339 -7.000,-0.4899,0.06460,0.05800,-0.0377,1.0000,0.0333 -6.750,-0.4878,0.06001,0.05330,-0.0392,1.0000,0.0329 -6.500,-0.4838,0.05556,0.04867,-0.0401,1.0000,0.0324 -6.250,-0.4775,0.05130,0.04415,-0.0405,1.0000,0.0319 -6.000,-0.4689,0.04715,0.03967,-0.0403,1.0000,0.0317 -5.750,-0.4576,0.04329,0.03542,-0.0398,1.0000,0.0316 -5.500,-0.4437,0.03967,0.03120,-0.0390,1.0000,0.0317 -5.250,-0.4275,0.03637,0.02740,-0.0379,1.0000,0.0320 -5.000,-0.4090,0.03341,0.02394,-0.0367,1.0000,0.0328 -4.750,-0.3887,0.03075,0.02077,-0.0352,1.0000,0.0345 -4.500,-0.3683,0.02857,0.01821,-0.0340,1.0000,0.0391 -4.250,-0.3478,0.02693,0.01638,-0.0327,1.0000,0.0457 -4.000,-0.3256,0.02499,0.01411,-0.0310,1.0000,0.0510 -3.750,-0.3048,0.02353,0.01259,-0.0297,1.0000,0.0650 -3.500,-0.2826,0.02204,0.01103,-0.0285,1.0000,0.0856 -3.250,-0.2603,0.02050,0.00970,-0.0276,1.0000,0.1336 -3.000,-0.2396,0.01893,0.00883,-0.0270,1.0000,0.2616 -2.750,-0.2220,0.01769,0.00843,-0.0254,1.0000,0.4387 -2.500,-0.2080,0.01680,0.00815,-0.0220,1.0000,0.6124 -2.250,-0.1912,0.01624,0.00803,-0.0180,1.0000,0.7841 -2.000,-0.1229,0.01594,0.00741,-0.0249,1.0000,1.0000 -1.750,-0.1059,0.01595,0.00706,-0.0235,1.0000,1.0000 -1.500,-0.0877,0.01600,0.00679,-0.0224,1.0000,1.0000 -1.250,-0.0688,0.01608,0.00659,-0.0213,1.0000,1.0000 -1.000,-0.0495,0.01620,0.00641,-0.0203,1.0000,1.0000 -0.750,-0.0300,0.01636,0.00634,-0.0194,1.0000,1.0000 -0.500,-0.0103,0.01654,0.00633,-0.0186,1.0000,1.0000 -0.250,0.0132,0.01678,0.00640,-0.0186,0.9981,1.0000 0.000,0.0554,0.01716,0.00660,-0.0221,0.9868,1.0000 0.250,0.0973,0.01753,0.00679,-0.0256,0.9753,1.0000 0.500,0.1392,0.01787,0.00704,-0.0289,0.9632,1.0000 0.750,0.1807,0.01818,0.00729,-0.0320,0.9505,1.0000 1.000,0.2217,0.01844,0.00753,-0.0349,0.9372,1.0000 1.250,0.2624,0.01865,0.00774,-0.0377,0.9231,1.0000 1.500,0.3034,0.01882,0.00795,-0.0403,0.9084,1.0000 1.750,0.3437,0.01894,0.00813,-0.0426,0.8929,1.0000 2.000,0.3828,0.01898,0.00828,-0.0445,0.8764,1.0000 2.250,0.4173,0.01900,0.00839,-0.0453,0.8575,1.0000 2.500,0.4506,0.01897,0.00847,-0.0457,0.8373,1.0000 2.750,0.4814,0.01894,0.00854,-0.0456,0.8152,1.0000 3.000,0.5123,0.01886,0.00867,-0.0452,0.7921,1.0000 3.250,0.5411,0.01879,0.00873,-0.0445,0.7663,1.0000 3.500,0.5679,0.01876,0.00882,-0.0434,0.7368,1.0000 3.750,0.5948,0.01875,0.00890,-0.0421,0.7044,1.0000 4.000,0.6211,0.01877,0.00899,-0.0408,0.6686,1.0000 4.250,0.6464,0.01889,0.00921,-0.0392,0.6289,1.0000 4.500,0.6705,0.01914,0.00944,-0.0376,0.5854,1.0000 4.750,0.6935,0.01951,0.00975,-0.0360,0.5393,1.0000 5.000,0.7151,0.02002,0.01021,-0.0343,0.4900,1.0000 5.250,0.7358,0.02064,0.01074,-0.0326,0.4404,1.0000 5.500,0.7557,0.02139,0.01137,-0.0310,0.3906,1.0000 5.750,0.7750,0.02224,0.01213,-0.0295,0.3409,1.0000 6.000,0.7937,0.02321,0.01314,-0.0281,0.2927,1.0000 6.250,0.8120,0.02430,0.01414,-0.0267,0.2461,1.0000 6.500,0.8296,0.02555,0.01526,-0.0254,0.2025,1.0000 6.750,0.8471,0.02695,0.01654,-0.0242,0.1622,1.0000 7.000,0.8647,0.02855,0.01811,-0.0230,0.1271,1.0000 7.250,0.8810,0.03023,0.01971,-0.0217,0.0987,1.0000 7.500,0.8989,0.03228,0.02181,-0.0203,0.0814,1.0000 7.750,0.9164,0.03426,0.02394,-0.0189,0.0664,1.0000 8.000,0.9333,0.03642,0.02623,-0.0176,0.0559,1.0000 8.250,0.9524,0.03908,0.02916,-0.0163,0.0496,1.0000 8.500,0.9701,0.04241,0.03273,-0.0150,0.0453,1.0000 8.750,0.9822,0.04518,0.03600,-0.0135,0.0393,1.0000 9.000,0.9904,0.04801,0.03884,-0.0123,0.0350,1.0000 9.250,0.9957,0.05207,0.04355,-0.0104,0.0336,1.0000 9.500,0.9946,0.05632,0.04831,-0.0085,0.0327,1.0000 9.750,0.9877,0.06057,0.05298,-0.0068,0.0321,1.0000 10.000,0.9750,0.06454,0.05726,-0.0051,0.0319,1.0000 10.250,0.9583,0.06872,0.06167,-0.0042,0.0319,1.0000 10.500,0.9407,0.07329,0.06644,-0.0048,0.0321,1.0000 10.750,0.9228,0.07852,0.07183,-0.0069,0.0324,1.0000 11.000,0.9040,0.08476,0.07818,-0.0105,0.0328,1.0000 11.250,0.8869,0.09182,0.08532,-0.0153,0.0332,1.0000