Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-ah81k144wfklappe-il-200000-n5 Airfoil,ah81k144wfklappe-il Reynolds number,200000 Ncrit,5 Mach,0 Max Cl/Cd,35.4456 Max Cl/Cd alpha,10 Url,http://airfoiltools.com/polar/csv?polar=xf-ah81k144wfklappe-il-200000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -13.000,-0.4915,0.10425,0.09724,-0.0166,0.3178,0.1620 -12.750,-0.4686,0.10374,0.09671,-0.0171,0.3148,0.1637 -12.500,-0.4861,0.09787,0.09077,-0.0213,0.3142,0.1748 -12.250,-0.4599,0.09771,0.09058,-0.0216,0.3111,0.1757 -12.000,-0.4346,0.09736,0.09018,-0.0221,0.3078,0.1769 -11.500,-0.4401,0.09002,0.08272,-0.0279,0.3056,0.1896 -11.250,-0.4149,0.08951,0.08214,-0.0284,0.3027,0.1903 -11.000,-0.3858,0.08929,0.08184,-0.0291,0.2999,0.1911 -10.750,-0.3587,0.08905,0.08156,-0.0294,0.2975,0.1922 -10.500,-0.3361,0.08836,0.08086,-0.0297,0.2956,0.1934 -10.000,-0.3510,0.08026,0.07267,-0.0364,0.2940,0.2056 -9.750,-0.3248,0.07990,0.07228,-0.0363,0.2912,0.2063 -9.500,-0.2950,0.07996,0.07232,-0.0360,0.2887,0.2072 -9.250,-0.2687,0.07955,0.07188,-0.0361,0.2862,0.2081 -9.000,-0.2447,0.07883,0.07111,-0.0365,0.2840,0.2092 -8.750,-0.2209,0.07809,0.07031,-0.0370,0.2821,0.2108 -8.500,-0.2046,0.07632,0.06848,-0.0384,0.2806,0.2123 -8.250,-0.2834,0.06442,0.05656,-0.0485,0.2828,0.2217 -8.000,-0.2666,0.06277,0.05485,-0.0492,0.2811,0.2222 -7.750,-0.2495,0.06114,0.05316,-0.0502,0.2794,0.2227 -7.500,-0.2346,0.05963,0.05165,-0.0505,0.2781,0.2232 -7.250,-0.2202,0.05812,0.05014,-0.0509,0.2766,0.2237 -7.000,-0.2076,0.05648,0.04850,-0.0514,0.2753,0.2242 -6.750,-0.1932,0.05516,0.04718,-0.0516,0.2737,0.2249 -6.500,-0.1804,0.05381,0.04583,-0.0517,0.2721,0.2258 -6.250,-0.3642,0.03787,0.02953,-0.0495,0.2770,0.2302 -6.000,-0.3699,0.03588,0.02739,-0.0465,0.2761,0.2315 -5.750,-0.3710,0.03401,0.02535,-0.0436,0.2750,0.2322 -5.500,-0.3651,0.03257,0.02376,-0.0411,0.2736,0.2328 -5.250,-0.3549,0.03139,0.02244,-0.0389,0.2720,0.2331 -5.000,-0.3418,0.03041,0.02133,-0.0368,0.2702,0.2335 -4.750,-0.3269,0.02954,0.02033,-0.0349,0.2685,0.2339 -4.500,-0.3103,0.02878,0.01945,-0.0331,0.2668,0.2342 -4.250,-0.2926,0.02811,0.01865,-0.0314,0.2652,0.2346 -4.000,-0.2740,0.02750,0.01792,-0.0297,0.2637,0.2349 -3.750,-0.2544,0.02700,0.01729,-0.0282,0.2623,0.2351 -3.500,-0.2340,0.02658,0.01675,-0.0267,0.2610,0.2354 -3.250,-0.2130,0.02619,0.01626,-0.0253,0.2597,0.2357 -3.000,-0.1916,0.02579,0.01581,-0.0239,0.2586,0.2360 -2.750,-0.1696,0.02545,0.01542,-0.0225,0.2573,0.2362 -2.500,-0.1473,0.02515,0.01507,-0.0212,0.2559,0.2365 -2.250,-0.1247,0.02486,0.01474,-0.0199,0.2544,0.2367 -2.000,-0.1019,0.02459,0.01441,-0.0186,0.2526,0.2370 -1.750,-0.0787,0.02435,0.01412,-0.0174,0.2511,0.2372 -1.500,-0.0554,0.02412,0.01383,-0.0162,0.2495,0.2375 -1.250,-0.0319,0.02389,0.01353,-0.0149,0.2479,0.2378 -1.000,-0.0082,0.02365,0.01322,-0.0137,0.2463,0.2380 -0.750,0.0157,0.02347,0.01297,-0.0126,0.2449,0.2383 -0.500,0.0397,0.02331,0.01274,-0.0114,0.2436,0.2386 -0.250,0.0641,0.02327,0.01262,-0.0104,0.2425,0.2388 0.000,0.0884,0.02315,0.01250,-0.0093,0.2412,0.2393 0.250,0.1126,0.02302,0.01241,-0.0082,0.2399,0.2399 0.500,0.1369,0.02293,0.01236,-0.0071,0.2385,0.2405 0.750,0.1614,0.02292,0.01241,-0.0061,0.2371,0.2413 1.000,0.1859,0.02294,0.01246,-0.0050,0.2358,0.2419 1.250,0.2104,0.02295,0.01250,-0.0040,0.2345,0.2424 1.500,0.2350,0.02294,0.01252,-0.0030,0.2331,0.2429 1.750,0.2597,0.02292,0.01250,-0.0019,0.2316,0.2435 2.000,0.2844,0.02290,0.01249,-0.0009,0.2304,0.2442 2.250,0.3093,0.02289,0.01248,0.0001,0.2292,0.2447 2.500,0.3342,0.02288,0.01248,0.0011,0.2282,0.2454 2.750,0.3592,0.02287,0.01245,0.0021,0.2271,0.2463 3.000,0.3842,0.02289,0.01246,0.0030,0.2261,0.2471 3.250,0.4094,0.02291,0.01245,0.0039,0.2249,0.2480 3.500,0.4340,0.02305,0.01260,0.0049,0.2238,0.2490 3.750,0.4579,0.02325,0.01289,0.0059,0.2227,0.2501 4.000,0.4817,0.02347,0.01318,0.0069,0.2215,0.2513 4.250,0.5057,0.02366,0.01345,0.0079,0.2200,0.2521 4.500,0.5297,0.02388,0.01373,0.0089,0.2186,0.2535 4.750,0.5541,0.02402,0.01392,0.0098,0.2170,0.2546 5.000,0.5785,0.02422,0.01415,0.0107,0.2158,0.2558 5.250,0.6035,0.02434,0.01429,0.0115,0.2144,0.2569 5.500,0.6286,0.02450,0.01449,0.0122,0.2134,0.2581 5.750,0.6549,0.02459,0.01465,0.0127,0.2124,0.2601 6.000,0.6811,0.02467,0.01478,0.0132,0.2113,0.2616 6.250,0.7070,0.02481,0.01496,0.0137,0.2104,0.2634 6.500,0.7333,0.02493,0.01510,0.0142,0.2094,0.2655 6.750,0.7596,0.02512,0.01530,0.0146,0.2085,0.2676 7.000,0.7857,0.02542,0.01562,0.0150,0.2077,0.2698 7.250,0.8087,0.02591,0.01624,0.0157,0.2065,0.2721 7.500,0.8308,0.02652,0.01699,0.0164,0.2053,0.2744 7.750,0.8525,0.02717,0.01778,0.0171,0.2039,0.2762 8.000,0.8749,0.02782,0.01857,0.0176,0.2024,0.2783 8.250,0.8990,0.02837,0.01928,0.0177,0.2010,0.2813 8.500,0.9229,0.02888,0.01991,0.0179,0.1995,0.2840 8.750,0.9478,0.02927,0.02039,0.0180,0.1980,0.2871 9.000,0.9735,0.02952,0.02069,0.0181,0.1966,0.2900 9.250,0.9989,0.02980,0.02101,0.0183,0.1954,0.2938 9.500,1.0234,0.03015,0.02140,0.0185,0.1944,0.2966 9.750,1.0492,0.03041,0.02170,0.0185,0.1934,0.3004 10.000,1.0779,0.03041,0.02170,0.0184,0.1921,0.3051 10.250,1.0981,0.03107,0.02246,0.0187,0.1907,0.3100 10.500,1.1037,0.03291,0.02459,0.0195,0.1887,0.3137 10.750,1.1032,0.03543,0.02741,0.0194,0.1864,0.3175