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| Original file line number | Diff line number | Diff line change |
|---|---|---|
| @@ -0,0 +1,132 @@ | ||
| Xfoil polar. Reynolds number fixed. Mach number fixed | ||
| Polar key,xf-n64015a-il-100000-n5 | ||
| Airfoil,n64015a-il | ||
| Reynolds number,100000 | ||
| Ncrit,5 | ||
| Mach,0 | ||
| Max Cl/Cd,36.8079 | ||
| Max Cl/Cd alpha,5.75 | ||
| Url,http://airfoiltools.com/polar/csv?polar=xf-n64015a-il-100000-n5 | ||
|
|
||
| Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr | ||
| -15.000,-0.7511,0.11842,0.11288,-0.0148,1.0000,0.0333 | ||
| -14.750,-0.7867,0.10562,0.09996,-0.0228,1.0000,0.0330 | ||
| -14.500,-0.8199,0.09535,0.08953,-0.0293,1.0000,0.0327 | ||
| -14.250,-0.8495,0.08708,0.08106,-0.0340,1.0000,0.0325 | ||
| -14.000,-0.8757,0.08015,0.07393,-0.0373,1.0000,0.0324 | ||
| -13.750,-0.8987,0.07420,0.06775,-0.0396,1.0000,0.0323 | ||
| -13.500,-0.9188,0.06903,0.06232,-0.0410,1.0000,0.0323 | ||
| -13.250,-0.9358,0.06449,0.05752,-0.0416,1.0000,0.0324 | ||
| -13.000,-0.9498,0.06046,0.05322,-0.0415,1.0000,0.0325 | ||
| -12.750,-0.9606,0.05686,0.04931,-0.0410,1.0000,0.0327 | ||
| -12.500,-0.9681,0.05362,0.04577,-0.0399,1.0000,0.0329 | ||
| -12.250,-0.9722,0.05071,0.04254,-0.0387,1.0000,0.0332 | ||
| -12.000,-0.9719,0.04808,0.03963,-0.0372,1.0000,0.0336 | ||
| -11.750,-0.9620,0.04587,0.03732,-0.0364,1.0000,0.0341 | ||
| -11.500,-0.9522,0.04404,0.03540,-0.0354,1.0000,0.0348 | ||
| -11.250,-0.9424,0.04240,0.03366,-0.0343,1.0000,0.0357 | ||
| -11.000,-0.9316,0.04079,0.03191,-0.0331,1.0000,0.0368 | ||
| -10.750,-0.9186,0.03916,0.03008,-0.0319,1.0000,0.0381 | ||
| -10.500,-0.9023,0.03751,0.02823,-0.0310,1.0000,0.0394 | ||
| -10.250,-0.8834,0.03595,0.02644,-0.0301,1.0000,0.0405 | ||
| -10.000,-0.8641,0.03443,0.02495,-0.0295,1.0000,0.0417 | ||
| -9.750,-0.8476,0.03317,0.02369,-0.0286,1.0000,0.0431 | ||
| -9.500,-0.8321,0.03203,0.02250,-0.0274,1.0000,0.0451 | ||
| -9.250,-0.8163,0.03096,0.02132,-0.0261,1.0000,0.0476 | ||
| -9.000,-0.8020,0.02982,0.02015,-0.0246,1.0000,0.0499 | ||
| -8.750,-0.7908,0.02879,0.01915,-0.0227,1.0000,0.0522 | ||
| -8.500,-0.7799,0.02784,0.01818,-0.0206,1.0000,0.0549 | ||
| -8.250,-0.7688,0.02702,0.01725,-0.0183,1.0000,0.0584 | ||
| -8.000,-0.7616,0.02606,0.01638,-0.0156,1.0000,0.0620 | ||
| -7.750,-0.7532,0.02530,0.01560,-0.0128,1.0000,0.0665 | ||
| -7.500,-0.7476,0.02453,0.01485,-0.0095,1.0000,0.0713 | ||
| -7.250,-0.7432,0.02385,0.01420,-0.0060,1.0000,0.0772 | ||
| -7.000,-0.7404,0.02323,0.01360,-0.0022,1.0000,0.0840 | ||
| -6.750,-0.7294,0.02252,0.01292,-0.0001,0.9968,0.0951 | ||
| -6.500,-0.7004,0.02138,0.01195,-0.0017,0.9866,0.1203 | ||
| -6.250,-0.6737,0.02012,0.01099,-0.0030,0.9760,0.1690 | ||
| -6.000,-0.6517,0.01859,0.01001,-0.0037,0.9646,0.2620 | ||
| -5.750,-0.6341,0.01723,0.00949,-0.0029,0.9524,0.3973 | ||
| -5.500,-0.6063,0.01690,0.00945,-0.0031,0.9429,0.4872 | ||
| -5.250,-0.5777,0.01681,0.00936,-0.0032,0.9324,0.5301 | ||
| -5.000,-0.5490,0.01678,0.00928,-0.0033,0.9223,0.5593 | ||
| -4.750,-0.5182,0.01679,0.00920,-0.0037,0.9137,0.5842 | ||
| -4.500,-0.4915,0.01690,0.00927,-0.0031,0.9029,0.6069 | ||
| -4.250,-0.4622,0.01708,0.00941,-0.0028,0.8947,0.6293 | ||
| -4.000,-0.4353,0.01720,0.00948,-0.0022,0.8845,0.6456 | ||
| -3.750,-0.4070,0.01723,0.00942,-0.0020,0.8756,0.6573 | ||
| -3.500,-0.3802,0.01714,0.00920,-0.0018,0.8665,0.6680 | ||
| -3.250,-0.3515,0.01714,0.00914,-0.0017,0.8575,0.6751 | ||
| -3.000,-0.3248,0.01698,0.00884,-0.0016,0.8491,0.6836 | ||
| -2.750,-0.2967,0.01694,0.00875,-0.0015,0.8402,0.6888 | ||
| -2.500,-0.2691,0.01682,0.00853,-0.0015,0.8324,0.6956 | ||
| -2.250,-0.2429,0.01672,0.00836,-0.0012,0.8234,0.7017 | ||
| -2.000,-0.2145,0.01665,0.00822,-0.0012,0.8161,0.7071 | ||
| -1.750,-0.1892,0.01655,0.00804,-0.0010,0.8077,0.7143 | ||
| -1.500,-0.1610,0.01649,0.00795,-0.0009,0.8004,0.7195 | ||
| -1.250,-0.1341,0.01645,0.00787,-0.0008,0.7927,0.7253 | ||
| -1.000,-0.1082,0.01637,0.00772,-0.0005,0.7851,0.7326 | ||
| -0.750,-0.0800,0.01636,0.00770,-0.0005,0.7786,0.7378 | ||
| -0.500,-0.0541,0.01633,0.00766,-0.0003,0.7709,0.7447 | ||
| -0.250,-0.0262,0.01629,0.00757,-0.0002,0.7652,0.7509 | ||
| 0.000,0.0000,0.01632,0.00764,0.0000,0.7572,0.7572 | ||
| 0.250,0.0263,0.01629,0.00757,0.0002,0.7509,0.7652 | ||
| 0.500,0.0541,0.01633,0.00766,0.0003,0.7447,0.7709 | ||
| 0.750,0.0801,0.01636,0.00770,0.0005,0.7378,0.7786 | ||
| 1.000,0.1082,0.01637,0.00772,0.0005,0.7326,0.7851 | ||
| 1.250,0.1341,0.01645,0.00787,0.0008,0.7253,0.7927 | ||
| 1.500,0.1610,0.01649,0.00795,0.0009,0.7195,0.8005 | ||
| 1.750,0.1892,0.01655,0.00804,0.0010,0.7143,0.8077 | ||
| 2.000,0.2145,0.01665,0.00822,0.0012,0.7071,0.8161 | ||
| 2.250,0.2429,0.01672,0.00836,0.0012,0.7017,0.8235 | ||
| 2.500,0.2691,0.01682,0.00853,0.0015,0.6956,0.8324 | ||
| 2.750,0.2967,0.01694,0.00875,0.0015,0.6888,0.8402 | ||
| 3.000,0.3248,0.01698,0.00884,0.0016,0.6836,0.8491 | ||
| 3.250,0.3515,0.01713,0.00914,0.0017,0.6751,0.8575 | ||
| 3.500,0.3802,0.01714,0.00920,0.0018,0.6680,0.8665 | ||
| 3.750,0.4070,0.01723,0.00942,0.0020,0.6573,0.8756 | ||
| 4.000,0.4353,0.01720,0.00947,0.0022,0.6456,0.8845 | ||
| 4.250,0.4622,0.01707,0.00941,0.0028,0.6293,0.8947 | ||
| 4.500,0.4915,0.01690,0.00927,0.0031,0.6069,0.9030 | ||
| 4.750,0.5182,0.01678,0.00920,0.0037,0.5842,0.9137 | ||
| 5.000,0.5490,0.01678,0.00928,0.0033,0.5593,0.9224 | ||
| 5.250,0.5777,0.01681,0.00936,0.0032,0.5300,0.9324 | ||
| 5.500,0.6063,0.01690,0.00944,0.0031,0.4872,0.9429 | ||
| 5.750,0.6342,0.01723,0.00949,0.0029,0.3973,0.9525 | ||
| 6.000,0.6518,0.01859,0.01000,0.0036,0.2619,0.9646 | ||
| 6.250,0.6738,0.02012,0.01099,0.0030,0.1690,0.9760 | ||
| 6.500,0.7005,0.02138,0.01194,0.0017,0.1202,0.9867 | ||
| 6.750,0.7295,0.02252,0.01291,0.0000,0.0951,0.9969 | ||
| 7.000,0.7404,0.02322,0.01359,0.0022,0.0840,1.0000 | ||
| 7.250,0.7432,0.02385,0.01420,0.0060,0.0772,1.0000 | ||
| 7.500,0.7476,0.02453,0.01484,0.0095,0.0713,1.0000 | ||
| 7.750,0.7533,0.02529,0.01560,0.0128,0.0665,1.0000 | ||
| 8.000,0.7617,0.02605,0.01637,0.0155,0.0619,1.0000 | ||
| 8.250,0.7690,0.02701,0.01725,0.0182,0.0583,1.0000 | ||
| 8.500,0.7802,0.02784,0.01818,0.0205,0.0549,1.0000 | ||
| 8.750,0.7911,0.02879,0.01915,0.0227,0.0522,1.0000 | ||
| 9.000,0.8025,0.02982,0.02015,0.0245,0.0499,1.0000 | ||
| 9.250,0.8168,0.03096,0.02132,0.0260,0.0475,1.0000 | ||
| 9.500,0.8327,0.03203,0.02250,0.0273,0.0451,1.0000 | ||
| 9.750,0.8482,0.03317,0.02370,0.0285,0.0431,1.0000 | ||
| 10.000,0.8647,0.03443,0.02496,0.0294,0.0417,1.0000 | ||
| 10.250,0.8841,0.03596,0.02645,0.0300,0.0405,1.0000 | ||
| 10.500,0.9029,0.03752,0.02824,0.0309,0.0394,1.0000 | ||
| 10.750,0.9192,0.03916,0.03009,0.0318,0.0381,1.0000 | ||
| 11.000,0.9323,0.04080,0.03192,0.0329,0.0368,1.0000 | ||
| 11.250,0.9431,0.04241,0.03367,0.0341,0.0357,1.0000 | ||
| 11.500,0.9530,0.04404,0.03541,0.0352,0.0348,1.0000 | ||
| 11.750,0.9629,0.04588,0.03733,0.0362,0.0341,1.0000 | ||
| 12.000,0.9729,0.04811,0.03965,0.0371,0.0336,1.0000 | ||
| 12.250,0.9729,0.05073,0.04258,0.0385,0.0332,1.0000 | ||
| 12.500,0.9688,0.05366,0.04582,0.0398,0.0329,1.0000 | ||
| 12.750,0.9614,0.05690,0.04936,0.0408,0.0327,1.0000 | ||
| 13.000,0.9507,0.06050,0.05327,0.0414,0.0325,1.0000 | ||
| 13.250,0.9367,0.06454,0.05758,0.0414,0.0324,1.0000 | ||
| 13.500,0.9196,0.06911,0.06241,0.0408,0.0323,1.0000 | ||
| 13.750,0.8995,0.07430,0.06785,0.0394,0.0323,1.0000 | ||
| 14.000,0.8764,0.08028,0.07406,0.0370,0.0324,1.0000 | ||
| 14.250,0.8501,0.08724,0.08122,0.0336,0.0325,1.0000 | ||
| 14.500,0.8206,0.09555,0.08973,0.0289,0.0327,1.0000 | ||
| 14.750,0.7872,0.10590,0.10025,0.0224,0.0330,1.0000 | ||
| 15.000,0.7514,0.11884,0.11330,0.0143,0.0333,1.0000 |