Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-lwk80080-il-100000-n5 Airfoil,lwk80080-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,33.9468 Max Cl/Cd alpha,3 Url,http://www.airfoiltools.com/polar/csv?polar=xf-lwk80080-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.750,-0.6507,0.08724,0.08231,-0.0131,1.0000,0.0196 -9.500,-0.6601,0.07970,0.07481,-0.0192,1.0000,0.0196 -9.250,-0.6720,0.07380,0.06888,-0.0231,1.0000,0.0192 -9.000,-0.6855,0.06908,0.06410,-0.0248,1.0000,0.0190 -8.750,-0.6996,0.06476,0.05969,-0.0245,1.0000,0.0190 -8.500,-0.7092,0.06021,0.05498,-0.0240,1.0000,0.0190 -8.250,-0.7144,0.05589,0.05042,-0.0230,1.0000,0.0193 -8.000,-0.7165,0.05163,0.04590,-0.0215,1.0000,0.0191 -7.750,-0.7151,0.04745,0.04127,-0.0197,1.0000,0.0205 -7.500,-0.7100,0.04374,0.03713,-0.0177,1.0000,0.0209 -7.250,-0.7012,0.04055,0.03344,-0.0156,1.0000,0.0214 -7.000,-0.6935,0.03641,0.02881,-0.0133,1.0000,0.0220 -6.750,-0.6809,0.03300,0.02498,-0.0114,1.0000,0.0224 -6.500,-0.6646,0.03031,0.02193,-0.0097,1.0000,0.0229 -6.250,-0.6462,0.02799,0.01931,-0.0083,1.0000,0.0238 -6.000,-0.6262,0.02603,0.01709,-0.0069,1.0000,0.0250 -5.750,-0.6052,0.02425,0.01509,-0.0055,1.0000,0.0268 -5.500,-0.5840,0.02291,0.01346,-0.0042,1.0000,0.0303 -5.250,-0.5640,0.02149,0.01191,-0.0028,1.0000,0.0340 -5.000,-0.5456,0.02032,0.01074,-0.0012,1.0000,0.0381 -4.750,-0.5269,0.01936,0.00964,0.0006,1.0000,0.0449 -4.500,-0.5106,0.01843,0.00874,0.0025,1.0000,0.0538 -4.250,-0.4953,0.01754,0.00781,0.0047,1.0000,0.0621 -4.000,-0.4798,0.01684,0.00714,0.0068,1.0000,0.0789 -3.750,-0.4652,0.01612,0.00649,0.0091,1.0000,0.1024 -3.500,-0.4512,0.01536,0.00592,0.0113,1.0000,0.1475 -3.250,-0.4404,0.01431,0.00548,0.0139,1.0000,0.2658 -3.000,-0.4327,0.01281,0.00518,0.0172,0.9980,0.5076 -2.750,-0.4101,0.01246,0.00560,0.0193,0.9922,0.7179 -2.500,-0.3822,0.01258,0.00569,0.0200,0.9863,0.7801 -2.250,-0.3524,0.01273,0.00572,0.0203,0.9814,0.8231 -2.000,-0.3235,0.01288,0.00582,0.0210,0.9767,0.8605 -1.750,-0.2878,0.01314,0.00601,0.0206,0.9744,0.8962 -1.500,-0.2454,0.01332,0.00608,0.0182,0.9730,0.9166 -1.250,-0.2049,0.01338,0.00597,0.0155,0.9702,0.9275 -1.000,-0.1609,0.01341,0.00590,0.0119,0.9682,0.9331 -0.750,-0.1247,0.01340,0.00581,0.0098,0.9632,0.9404 -0.500,-0.0825,0.01341,0.00577,0.0064,0.9599,0.9444 -0.250,-0.0400,0.01341,0.00572,0.0030,0.9568,0.9483 0.000,0.0001,0.01340,0.00570,0.0000,0.9529,0.9530 0.250,0.0400,0.01340,0.00572,-0.0030,0.9483,0.9568 0.500,0.0826,0.01340,0.00577,-0.0064,0.9444,0.9599 0.750,0.1247,0.01340,0.00582,-0.0098,0.9404,0.9631 1.000,0.1608,0.01341,0.00590,-0.0119,0.9331,0.9681 1.250,0.2050,0.01338,0.00598,-0.0155,0.9274,0.9702 1.500,0.2459,0.01331,0.00607,-0.0183,0.9162,0.9729 1.750,0.2879,0.01313,0.00600,-0.0206,0.8953,0.9745 2.000,0.3237,0.01288,0.00582,-0.0210,0.8601,0.9767 2.250,0.3522,0.01271,0.00570,-0.0202,0.8211,0.9814 2.500,0.3824,0.01258,0.00571,-0.0200,0.7817,0.9863 2.750,0.4105,0.01247,0.00562,-0.0195,0.7226,0.9922 3.000,0.4335,0.01277,0.00521,-0.0173,0.5164,0.9981 3.250,0.4400,0.01434,0.00548,-0.0138,0.2608,1.0000 3.500,0.4510,0.01538,0.00591,-0.0113,0.1454,1.0000 3.750,0.4651,0.01611,0.00650,-0.0091,0.1022,1.0000 4.000,0.4798,0.01684,0.00715,-0.0068,0.0791,1.0000 4.250,0.4952,0.01756,0.00784,-0.0047,0.0618,1.0000 4.500,0.5107,0.01843,0.00875,-0.0025,0.0525,1.0000 4.750,0.5275,0.01929,0.00960,-0.0007,0.0427,1.0000 5.000,0.5455,0.02035,0.01075,0.0012,0.0373,1.0000 5.250,0.5634,0.02165,0.01204,0.0028,0.0331,1.0000 5.500,0.5842,0.02275,0.01334,0.0042,0.0280,1.0000 5.750,0.6052,0.02429,0.01507,0.0056,0.0263,1.0000 6.000,0.6258,0.02602,0.01707,0.0069,0.0243,1.0000 6.250,0.6459,0.02802,0.01932,0.0083,0.0234,1.0000 6.500,0.6641,0.03041,0.02202,0.0097,0.0226,1.0000 6.750,0.6795,0.03344,0.02542,0.0115,0.0221,1.0000 7.000,0.6920,0.03688,0.02931,0.0134,0.0218,1.0000 7.250,0.7006,0.04084,0.03374,0.0155,0.0216,1.0000 7.500,0.7084,0.04429,0.03760,0.0176,0.0214,1.0000 7.750,0.7139,0.04791,0.04158,0.0194,0.0214,1.0000 8.000,0.7168,0.05148,0.04552,0.0211,0.0212,1.0000 8.250,0.7157,0.05548,0.04992,0.0228,0.0204,1.0000 8.500,0.7087,0.06031,0.05506,0.0240,0.0194,1.0000 8.750,0.7014,0.06437,0.05926,0.0246,0.0197,1.0000 9.000,0.6878,0.06865,0.06365,0.0249,0.0196,1.0000 9.250,0.6740,0.07328,0.06834,0.0236,0.0199,1.0000 9.500,0.6620,0.07893,0.07403,0.0200,0.0201,1.0000 9.750,0.6539,0.08510,0.08017,0.0156,0.0208,1.0000 10.000,0.6472,0.09280,0.08782,0.0096,0.0202,1.0000