Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-raf30-il-200000 Airfoil,raf30-il Reynolds number,200000 Ncrit,9 Mach,0 Max Cl/Cd,52.2842 Max Cl/Cd alpha,5 Url,http://airfoiltools.com/polar/csv?polar=xf-raf30-il-200000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -14.000,-0.7279,0.10867,0.10473,-0.0199,1.0000,0.0491 -13.750,-0.7197,0.10703,0.10310,-0.0197,1.0000,0.0497 -13.500,-0.9410,0.06599,0.06111,-0.0481,1.0000,0.0407 -13.250,-0.9636,0.06193,0.05684,-0.0487,1.0000,0.0405 -13.000,-0.9843,0.05776,0.05248,-0.0482,1.0000,0.0407 -12.750,-1.0018,0.05457,0.04908,-0.0467,1.0000,0.0407 -12.500,-1.0170,0.05133,0.04562,-0.0445,1.0000,0.0408 -12.250,-1.0273,0.04853,0.04263,-0.0417,1.0000,0.0410 -12.000,-1.0323,0.04587,0.03983,-0.0390,1.0000,0.0415 -11.750,-1.0362,0.04357,0.03735,-0.0358,1.0000,0.0417 -11.500,-1.0335,0.04144,0.03505,-0.0334,1.0000,0.0423 -11.250,-1.0262,0.03949,0.03297,-0.0313,1.0000,0.0430 -11.000,-1.0185,0.03776,0.03108,-0.0291,1.0000,0.0440 -10.750,-1.0105,0.03607,0.02918,-0.0268,1.0000,0.0451 -10.500,-1.0013,0.03443,0.02730,-0.0244,1.0000,0.0462 -10.250,-0.9900,0.03283,0.02544,-0.0222,1.0000,0.0471 -10.000,-0.9770,0.03143,0.02378,-0.0201,1.0000,0.0478 -9.750,-0.9581,0.02898,0.02121,-0.0192,1.0000,0.0492 -9.500,-0.9393,0.02764,0.01989,-0.0181,1.0000,0.0510 -9.250,-0.9215,0.02653,0.01872,-0.0167,1.0000,0.0526 -9.000,-0.9030,0.02542,0.01751,-0.0152,1.0000,0.0541 -8.750,-0.8845,0.02441,0.01640,-0.0137,1.0000,0.0557 -8.500,-0.8664,0.02364,0.01550,-0.0121,1.0000,0.0571 -8.250,-0.8495,0.02213,0.01407,-0.0105,1.0000,0.0594 -8.000,-0.8334,0.02127,0.01322,-0.0086,1.0000,0.0615 -7.750,-0.8174,0.02049,0.01242,-0.0066,1.0000,0.0637 -7.500,-0.8013,0.01982,0.01169,-0.0045,1.0000,0.0663 -7.250,-0.7883,0.01892,0.01082,-0.0020,1.0000,0.0694 -7.000,-0.7745,0.01823,0.01015,0.0004,1.0000,0.0732 -6.750,-0.7597,0.01764,0.00952,0.0028,1.0000,0.0778 -6.500,-0.7482,0.01687,0.00884,0.0056,1.0000,0.0846 -6.250,-0.7363,0.01617,0.00823,0.0083,1.0000,0.0974 -6.000,-0.7277,0.01526,0.00754,0.0116,1.0000,0.1306 -5.750,-0.7192,0.01444,0.00700,0.0147,1.0000,0.1770 -5.500,-0.7089,0.01384,0.00667,0.0175,1.0000,0.2238 -5.250,-0.6969,0.01343,0.00645,0.0201,1.0000,0.2688 -5.000,-0.6846,0.01309,0.00628,0.0225,1.0000,0.3082 -4.500,-0.6282,0.01246,0.00601,0.0211,0.9925,0.3999 -4.250,-0.5903,0.01217,0.00592,0.0187,0.9854,0.4514 -4.000,-0.5530,0.01195,0.00585,0.0166,0.9778,0.4972 -3.750,-0.5134,0.01180,0.00580,0.0141,0.9712,0.5385 -3.500,-0.4786,0.01165,0.00575,0.0127,0.9623,0.5739 -3.250,-0.4375,0.01154,0.00570,0.0101,0.9568,0.6050 -3.000,-0.4031,0.01141,0.00561,0.0089,0.9477,0.6285 -2.750,-0.3608,0.01128,0.00549,0.0062,0.9426,0.6507 -2.500,-0.3246,0.01117,0.00544,0.0047,0.9345,0.6718 -2.250,-0.2851,0.01108,0.00537,0.0028,0.9282,0.6973 -2.000,-0.2491,0.01098,0.00533,0.0016,0.9198,0.7164 -1.750,-0.2110,0.01085,0.00521,-0.0001,0.9119,0.7321 -1.500,-0.1784,0.01075,0.00511,-0.0007,0.9009,0.7467 -1.250,-0.1428,0.01064,0.00501,-0.0018,0.8907,0.7600 -1.000,-0.1106,0.01054,0.00492,-0.0021,0.8779,0.7728 -0.750,-0.0825,0.01049,0.00486,-0.0016,0.8636,0.7856 -0.500,-0.0553,0.01046,0.00483,-0.0010,0.8500,0.7988 -0.250,-0.0285,0.01044,0.00480,-0.0004,0.8370,0.8124 0.000,0.0000,0.01044,0.00480,0.0000,0.8248,0.8248 0.250,0.0285,0.01044,0.00480,0.0004,0.8124,0.8370 0.500,0.0553,0.01046,0.00483,0.0010,0.7988,0.8500 0.750,0.0825,0.01049,0.00486,0.0016,0.7856,0.8636 1.000,0.1106,0.01054,0.00492,0.0021,0.7728,0.8779 1.250,0.1428,0.01064,0.00501,0.0018,0.7601,0.8907 1.500,0.1784,0.01075,0.00512,0.0007,0.7467,0.9009 1.750,0.2111,0.01085,0.00521,0.0001,0.7320,0.9119 2.000,0.2491,0.01098,0.00534,-0.0016,0.7166,0.9198 2.250,0.2850,0.01107,0.00537,-0.0028,0.6971,0.9282 2.500,0.3245,0.01116,0.00543,-0.0047,0.6718,0.9345 2.750,0.3609,0.01128,0.00549,-0.0062,0.6509,0.9426 3.000,0.4031,0.01142,0.00561,-0.0089,0.6285,0.9477 3.250,0.4376,0.01154,0.00570,-0.0101,0.6049,0.9568 3.500,0.4787,0.01165,0.00574,-0.0127,0.5734,0.9624 3.750,0.5133,0.01180,0.00580,-0.0141,0.5385,0.9711 4.000,0.5531,0.01195,0.00585,-0.0166,0.4973,0.9778 4.250,0.5904,0.01217,0.00592,-0.0187,0.4514,0.9854 4.500,0.6283,0.01246,0.00601,-0.0212,0.3996,0.9926 4.750,0.6675,0.01280,0.00612,-0.0240,0.3472,0.9991 5.000,0.6844,0.01309,0.00627,-0.0225,0.3071,1.0000 5.250,0.6968,0.01343,0.00645,-0.0200,0.2683,1.0000 5.500,0.7088,0.01384,0.00667,-0.0175,0.2238,1.0000 5.750,0.7190,0.01444,0.00701,-0.0147,0.1764,1.0000 6.000,0.7276,0.01526,0.00755,-0.0116,0.1302,1.0000 6.250,0.7362,0.01617,0.00823,-0.0083,0.0974,1.0000 6.500,0.7481,0.01687,0.00884,-0.0055,0.0845,1.0000 6.750,0.7596,0.01764,0.00952,-0.0027,0.0778,1.0000 7.000,0.7744,0.01823,0.01015,-0.0004,0.0732,1.0000 7.250,0.7882,0.01893,0.01083,0.0020,0.0694,1.0000 7.500,0.8012,0.01983,0.01170,0.0045,0.0664,1.0000 7.750,0.8175,0.02049,0.01242,0.0066,0.0638,1.0000 8.000,0.8334,0.02127,0.01322,0.0086,0.0615,1.0000 8.250,0.8495,0.02212,0.01406,0.0105,0.0595,1.0000 8.500,0.8665,0.02365,0.01551,0.0120,0.0571,1.0000 8.750,0.8846,0.02443,0.01641,0.0137,0.0557,1.0000 9.000,0.9031,0.02544,0.01753,0.0152,0.0541,1.0000 9.250,0.9215,0.02652,0.01870,0.0167,0.0525,1.0000 9.500,0.9393,0.02762,0.01987,0.0181,0.0509,1.0000 9.750,0.9582,0.02899,0.02122,0.0192,0.0493,1.0000 10.000,0.9772,0.03145,0.02380,0.0200,0.0479,1.0000 10.250,0.9903,0.03283,0.02543,0.0221,0.0471,1.0000 10.500,1.0014,0.03443,0.02730,0.0244,0.0462,1.0000 10.750,1.0105,0.03611,0.02923,0.0268,0.0451,1.0000 11.000,1.0186,0.03778,0.03110,0.0291,0.0440,1.0000 11.250,1.0267,0.03947,0.03294,0.0312,0.0430,1.0000 11.500,1.0332,0.04147,0.03509,0.0334,0.0423,1.0000 11.750,1.0357,0.04364,0.03743,0.0359,0.0418,1.0000 12.000,1.0315,0.04592,0.03989,0.0391,0.0416,1.0000 12.250,1.0274,0.04837,0.04249,0.0418,0.0411,1.0000 12.500,1.0161,0.05122,0.04554,0.0446,0.0409,1.0000 12.750,1.0025,0.05453,0.04904,0.0466,0.0407,1.0000 13.000,0.9847,0.05829,0.05299,0.0480,0.0405,1.0000 13.250,0.9627,0.06245,0.05737,0.0485,0.0404,1.0000 13.500,0.9392,0.06604,0.06119,0.0479,0.0408,1.0000 13.750,0.6283,0.09894,0.09524,0.0262,0.0498,1.0000 14.000,0.6277,0.10251,0.09881,0.0251,0.0491,1.0000