Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-raf30md-il-1000000-n5 Airfoil,raf30md-il Reynolds number,1000000 Ncrit,5 Mach,0 Max Cl/Cd,65.3846 Max Cl/Cd alpha,6 Url,http://airfoiltools.com/polar/csv?polar=xf-raf30md-il-1000000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -12.750,-1.0078,0.05357,0.05172,-0.0215,1.0000,0.0021 -12.500,-1.0309,0.04641,0.04439,-0.0270,1.0000,0.0021 -12.250,-1.0552,0.04134,0.03912,-0.0282,1.0000,0.0021 -12.000,-1.0770,0.03774,0.03531,-0.0259,1.0000,0.0021 -11.750,-1.0922,0.03454,0.03185,-0.0225,1.0000,0.0021 -11.500,-1.1000,0.03097,0.02795,-0.0199,1.0000,0.0022 -11.250,-1.0969,0.02832,0.02502,-0.0179,1.0000,0.0022 -11.000,-1.0893,0.02599,0.02242,-0.0161,1.0000,0.0023 -10.750,-1.0760,0.02434,0.02057,-0.0147,1.0000,0.0024 -10.500,-1.0602,0.02292,0.01894,-0.0135,1.0000,0.0024 -10.250,-1.0424,0.02175,0.01762,-0.0125,1.0000,0.0025 -10.000,-1.0232,0.02075,0.01649,-0.0115,1.0000,0.0026 -9.750,-1.0041,0.01967,0.01526,-0.0105,1.0000,0.0027 -9.500,-0.9837,0.01878,0.01425,-0.0096,1.0000,0.0028 -9.250,-0.9626,0.01798,0.01334,-0.0088,1.0000,0.0030 -9.000,-0.9413,0.01718,0.01243,-0.0079,1.0000,0.0031 -8.750,-0.9195,0.01645,0.01158,-0.0071,1.0000,0.0033 -8.500,-0.8980,0.01565,0.01066,-0.0062,1.0000,0.0034 -8.250,-0.8757,0.01500,0.00990,-0.0054,1.0000,0.0035 -8.000,-0.8542,0.01422,0.00900,-0.0044,1.0000,0.0036 -7.750,-0.8331,0.01337,0.00805,-0.0033,1.0000,0.0040 -7.500,-0.8104,0.01282,0.00741,-0.0025,1.0000,0.0043 -7.250,-0.7874,0.01234,0.00688,-0.0016,1.0000,0.0045 -7.000,-0.7643,0.01190,0.00638,-0.0008,1.0000,0.0049 -6.750,-0.7411,0.01147,0.00589,0.0000,1.0000,0.0052 -6.500,-0.7176,0.01110,0.00546,0.0008,1.0000,0.0056 -6.250,-0.6946,0.01064,0.00494,0.0017,1.0000,0.0061 -6.000,-0.6713,0.01026,0.00456,0.0025,1.0000,0.0071 -5.750,-0.6478,0.00994,0.00421,0.0034,1.0000,0.0080 -5.500,-0.6241,0.00965,0.00386,0.0042,1.0000,0.0087 -5.250,-0.6007,0.00932,0.00351,0.0051,1.0000,0.0106 -5.000,-0.5729,0.00904,0.00327,0.0049,0.9991,0.0135 -4.750,-0.5410,0.00877,0.00305,0.0039,0.9966,0.0198 -4.500,-0.5092,0.00860,0.00285,0.0029,0.9937,0.0236 -4.250,-0.4777,0.00846,0.00270,0.0020,0.9902,0.0252 -4.000,-0.4447,0.00833,0.00256,0.0008,0.9869,0.0259 -3.750,-0.4136,0.00818,0.00241,0.0000,0.9817,0.0262 -3.500,-0.3801,0.00793,0.00211,-0.0013,0.9769,0.0279 -3.250,-0.3467,0.00772,0.00188,-0.0026,0.9694,0.0309 -3.000,-0.3123,0.00753,0.00168,-0.0041,0.9590,0.0332 -2.750,-0.2784,0.00737,0.00151,-0.0054,0.9423,0.0367 -2.500,-0.2487,0.00709,0.00132,-0.0058,0.9163,0.0738 -2.250,-0.2228,0.00690,0.00117,-0.0054,0.8844,0.1101 -1.500,-0.1488,0.00631,0.00081,-0.0035,0.8008,0.2631 -1.250,-0.1240,0.00605,0.00072,-0.0029,0.7800,0.3330 -1.000,-0.0984,0.00589,0.00066,-0.0025,0.7597,0.3792 -0.750,-0.0729,0.00574,0.00060,-0.0021,0.7398,0.4310 -0.500,-0.0484,0.00550,0.00056,-0.0015,0.7147,0.5100 -0.250,-0.0243,0.00544,0.00054,-0.0007,0.6682,0.5686 0.000,0.0001,0.00545,0.00053,0.0000,0.6171,0.6154 0.250,0.0243,0.00542,0.00054,0.0007,0.5701,0.6703 0.500,0.0484,0.00550,0.00056,0.0015,0.5087,0.7150 0.750,0.0730,0.00573,0.00060,0.0021,0.4323,0.7396 1.000,0.0985,0.00589,0.00066,0.0025,0.3798,0.7599 1.250,0.1241,0.00606,0.00072,0.0029,0.3314,0.7800 1.500,0.1490,0.00629,0.00081,0.0034,0.2661,0.8008 1.750,0.1735,0.00656,0.00091,0.0040,0.1984,0.8248 2.000,0.1980,0.00676,0.00103,0.0047,0.1463,0.8531 2.250,0.2228,0.00691,0.00117,0.0054,0.1088,0.8842 2.500,0.2488,0.00709,0.00132,0.0058,0.0737,0.9161 2.750,0.2784,0.00737,0.00151,0.0054,0.0367,0.9421 3.000,0.3123,0.00753,0.00169,0.0041,0.0330,0.9590 3.250,0.3466,0.00771,0.00188,0.0026,0.0310,0.9694 3.500,0.3798,0.00793,0.00211,0.0014,0.0280,0.9768 3.750,0.4134,0.00818,0.00240,0.0001,0.0261,0.9816 4.000,0.4445,0.00833,0.00256,-0.0007,0.0259,0.9868 4.250,0.4775,0.00845,0.00269,-0.0019,0.0252,0.9901 4.500,0.5090,0.00860,0.00285,-0.0028,0.0236,0.9936 4.750,0.5408,0.00877,0.00304,-0.0038,0.0196,0.9965 5.000,0.5726,0.00904,0.00327,-0.0048,0.0135,0.9989 5.250,0.6009,0.00933,0.00351,-0.0051,0.0106,1.0000 5.500,0.6243,0.00965,0.00385,-0.0042,0.0087,1.0000 5.750,0.6480,0.00994,0.00421,-0.0034,0.0079,1.0000 6.000,0.6715,0.01027,0.00456,-0.0026,0.0072,1.0000 6.250,0.6948,0.01064,0.00495,-0.0017,0.0063,1.0000 6.500,0.7177,0.01110,0.00546,-0.0008,0.0056,1.0000 6.750,0.7411,0.01148,0.00590,0.0000,0.0052,1.0000 7.000,0.7643,0.01192,0.00640,0.0008,0.0049,1.0000 7.250,0.7874,0.01236,0.00690,0.0017,0.0046,1.0000 7.500,0.8104,0.01284,0.00743,0.0025,0.0043,1.0000 7.750,0.8331,0.01338,0.00806,0.0033,0.0040,1.0000 8.000,0.8546,0.01414,0.00892,0.0043,0.0037,1.0000 8.250,0.8754,0.01503,0.00994,0.0054,0.0036,1.0000 8.500,0.8977,0.01569,0.01070,0.0062,0.0034,1.0000 8.750,0.9194,0.01644,0.01157,0.0071,0.0033,1.0000 9.000,0.9410,0.01720,0.01244,0.0080,0.0031,1.0000 9.250,0.9622,0.01802,0.01339,0.0089,0.0030,1.0000 9.500,0.9834,0.01881,0.01429,0.0097,0.0028,1.0000 9.750,1.0033,0.01979,0.01540,0.0106,0.0027,1.0000 10.000,1.0234,0.02069,0.01642,0.0115,0.0026,1.0000 10.250,1.0415,0.02188,0.01777,0.0126,0.0025,1.0000 10.500,1.0591,0.02307,0.01911,0.0137,0.0024,1.0000 10.750,1.0758,0.02433,0.02056,0.0148,0.0024,1.0000 11.000,1.0890,0.02601,0.02245,0.0162,0.0023,1.0000 11.250,1.0985,0.02805,0.02472,0.0178,0.0022,1.0000 11.500,1.0991,0.03105,0.02804,0.0200,0.0022,1.0000 11.750,1.0935,0.03436,0.03166,0.0225,0.0021,1.0000 12.000,1.0809,0.03741,0.03495,0.0256,0.0021,1.0000 12.250,1.0606,0.04083,0.03857,0.0282,0.0021,1.0000