Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-ah81k144wfklappe-il-100000-n5 Airfoil,ah81k144wfklappe-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,9.98484 Max Cl/Cd alpha,4 Url,http://airfoiltools.com/polar/csv?polar=xf-ah81k144wfklappe-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -12.500,-0.3697,0.11643,0.10790,-0.0151,0.3540,0.1779 -12.250,-0.3832,0.11274,0.10416,-0.0184,0.3532,0.1895 -12.000,-0.3484,0.11222,0.10357,-0.0191,0.3466,0.1909 -11.750,-0.3163,0.11142,0.10268,-0.0203,0.3414,0.1934 -11.250,-0.3077,0.10592,0.09702,-0.0257,0.3368,0.2060 -11.000,-0.2755,0.10487,0.09592,-0.0265,0.3324,0.2076 -10.750,-0.2481,0.10382,0.09480,-0.0274,0.3281,0.2102 -10.250,-0.2471,0.09895,0.08980,-0.0318,0.3245,0.2225 -10.000,-0.2097,0.09824,0.08899,-0.0322,0.3208,0.2243 -9.750,-0.1786,0.09729,0.08793,-0.0333,0.3177,0.2272 -9.250,-0.1760,0.09347,0.08408,-0.0367,0.3151,0.2402 -9.000,-0.1428,0.09239,0.08298,-0.0368,0.3117,0.2419 -8.750,-0.1200,0.09090,0.08146,-0.0374,0.3092,0.2435 -8.500,-0.0986,0.08953,0.08005,-0.0381,0.3070,0.2460 -8.250,-0.0831,0.08790,0.07837,-0.0391,0.3050,0.2482 -8.000,-0.0721,0.08594,0.07634,-0.0402,0.3034,0.2493 -7.750,-0.0616,0.08392,0.07427,-0.0414,0.3019,0.2499 -7.500,-0.0514,0.08195,0.07223,-0.0425,0.3005,0.2506 -7.250,-0.0436,0.08004,0.07025,-0.0437,0.2992,0.2522 -7.000,-0.0419,0.07791,0.06809,-0.0448,0.2983,0.2540 -6.750,-0.0373,0.07574,0.06595,-0.0454,0.2972,0.2544 -6.500,-0.0344,0.07352,0.06375,-0.0460,0.2961,0.2548 -6.250,-0.0315,0.07132,0.06156,-0.0464,0.2946,0.2550 -6.000,-0.0335,0.06889,0.05916,-0.0468,0.2933,0.2554 -5.750,-0.1167,0.06119,0.05140,-0.0489,0.2958,0.2574 -5.500,-0.1586,0.05681,0.04696,-0.0469,0.2960,0.2575 -5.250,-0.1809,0.05340,0.04349,-0.0449,0.2956,0.2577 -5.000,-0.1833,0.05130,0.04137,-0.0431,0.2942,0.2580 -4.750,-0.1757,0.04993,0.04000,-0.0414,0.2925,0.2586 -4.500,-0.1629,0.04899,0.03907,-0.0399,0.2905,0.2592 -4.250,-0.1532,0.04786,0.03792,-0.0383,0.2886,0.2597 -4.000,-0.1510,0.04615,0.03612,-0.0364,0.2871,0.2600 -3.750,-0.1475,0.04450,0.03436,-0.0344,0.2858,0.2602 -3.500,-0.1399,0.04313,0.03288,-0.0326,0.2845,0.2604 -3.250,-0.1294,0.04197,0.03162,-0.0308,0.2832,0.2606 -3.000,-0.1167,0.04100,0.03053,-0.0292,0.2820,0.2609 -2.750,-0.1024,0.04017,0.02959,-0.0276,0.2809,0.2612 -2.500,-0.0870,0.03948,0.02877,-0.0261,0.2798,0.2615 -2.250,-0.0712,0.03886,0.02810,-0.0245,0.2787,0.2618 -2.000,-0.0548,0.03831,0.02755,-0.0228,0.2774,0.2621 -1.750,-0.0380,0.03784,0.02709,-0.0211,0.2761,0.2624 -1.500,-0.0205,0.03748,0.02673,-0.0195,0.2746,0.2628 -1.250,-0.0028,0.03717,0.02642,-0.0179,0.2732,0.2631 -1.000,0.0153,0.03690,0.02614,-0.0163,0.2718,0.2635 -0.750,0.0339,0.03668,0.02590,-0.0147,0.2701,0.2640 -0.500,0.0528,0.03646,0.02564,-0.0132,0.2684,0.2644 -0.250,0.0721,0.03626,0.02541,-0.0116,0.2668,0.2649 0.000,0.0919,0.03611,0.02521,-0.0102,0.2653,0.2655 0.250,0.1122,0.03606,0.02511,-0.0087,0.2641,0.2663 0.500,0.1325,0.03604,0.02504,-0.0073,0.2630,0.2671 0.750,0.1530,0.03609,0.02504,-0.0059,0.2620,0.2682 1.000,0.1736,0.03616,0.02504,-0.0046,0.2610,0.2691 1.250,0.1929,0.03638,0.02523,-0.0031,0.2599,0.2698 1.500,0.2073,0.03679,0.02580,-0.0009,0.2580,0.2705 1.750,0.2217,0.03725,0.02638,0.0012,0.2557,0.2710 2.000,0.2371,0.03769,0.02689,0.0031,0.2536,0.2717 2.250,0.2531,0.03814,0.02738,0.0049,0.2517,0.2722 2.500,0.2700,0.03853,0.02779,0.0066,0.2499,0.2729 2.750,0.2882,0.03882,0.02807,0.0082,0.2482,0.2737 3.000,0.3059,0.03923,0.02848,0.0097,0.2469,0.2745 3.250,0.3267,0.03933,0.02851,0.0110,0.2454,0.2753 3.500,0.3476,0.03952,0.02864,0.0123,0.2442,0.2762 3.750,0.3708,0.03957,0.02860,0.0133,0.2431,0.2771 4.000,0.3953,0.03959,0.02857,0.0141,0.2420,0.2782 4.250,0.3799,0.04226,0.03166,0.0182,0.2384,0.2783 4.500,0.3675,0.04477,0.03444,0.0215,0.2350,0.2789 4.750,0.3648,0.04654,0.03635,0.0238,0.2322,0.2795 5.000,0.3639,0.04826,0.03818,0.0257,0.2302,0.2802 5.250,0.3804,0.04873,0.03868,0.0266,0.2285,0.2814 5.500,0.3881,0.04975,0.03974,0.0281,0.2272,0.2824 5.750,0.4044,0.05030,0.04030,0.0290,0.2261,0.2839 6.000,0.4322,0.05018,0.04016,0.0292,0.2251,0.2853 6.250,0.4600,0.05021,0.04017,0.0294,0.2244,0.2872 6.750,0.3192,0.07372,0.06405,0.0143,0.2089,0.2842 7.000,0.3442,0.07449,0.06483,0.0135,0.2080,0.2860 7.500,0.3059,0.08738,0.07785,0.0042,0.1976,0.2864 8.500,0.3610,0.09649,0.08706,-0.0032,0.1864,0.2923 9.000,0.3878,0.10120,0.09182,-0.0069,0.1798,0.2952 9.250,0.4087,0.10256,0.09317,-0.0081,0.1783,0.2977 9.500,0.4365,0.10322,0.09390,-0.0093,0.1770,0.2999 10.000,0.4323,0.11228,0.10311,-0.0155,0.1660,0.3020 10.250,0.4531,0.11385,0.10474,-0.0171,0.1642,0.3046 10.500,0.4767,0.11496,0.10588,-0.0182,0.1628,0.3077 11.000,0.4730,0.12456,0.11558,-0.0242,0.1527,0.3102 11.250,0.4897,0.12669,0.11772,-0.0257,0.1510,0.3139 11.500,0.5087,0.12843,0.11946,-0.0270,0.1498,0.3174 11.750,0.5315,0.12967,0.12074,-0.0283,0.1487,0.3222 12.250,0.5193,0.14183,0.13302,-0.0354,0.1424,0.3245 12.500,0.5279,0.14568,0.13693,-0.0380,0.1411,0.3281