S6063 7.05% (s6063-il) Xfoil prediction polar at RE=50,000 Ncrit=9
| Details | Polar file |
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Airfoil: S6063 7.05% (s6063-il) Reynolds number: 50,000 Max Cl/Cd: 34.71 at α=5.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-s6063-il-50000.txt Download as CSV file: xf-s6063-il-50000.csv |
XFOIL Version 6.96
Calculated polar for: S6063 7.05%
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.050 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-7.750 -0.5196 0.09618 0.08961 0.0068 1.0000 0.2578
-7.500 -0.5206 0.09322 0.08674 0.0062 1.0000 0.2700
-7.250 -0.5206 0.09025 0.08386 0.0060 1.0000 0.2833
-6.750 -0.5062 0.08328 0.07699 0.0073 1.0000 0.3139
-6.500 -0.5001 0.08003 0.07380 0.0080 1.0000 0.3313
-6.250 -0.5044 0.07748 0.07137 0.0073 1.0000 0.3528
-6.000 -0.4894 0.07361 0.06751 0.0092 1.0000 0.3708
-5.750 -0.4845 0.07064 0.06462 0.0105 1.0000 0.3969
-5.500 -0.4653 0.05045 0.04278 -0.0351 1.0000 0.1283
-5.250 -0.4443 0.04502 0.03706 -0.0356 1.0000 0.1128
-5.000 -0.4217 0.04037 0.03145 -0.0362 1.0000 0.1009
-4.750 -0.4003 0.03656 0.02750 -0.0357 1.0000 0.0982
-4.500 -0.3773 0.03338 0.02382 -0.0352 1.0000 0.0975
-4.250 -0.3530 0.03070 0.02057 -0.0344 1.0000 0.0996
-4.000 -0.3288 0.02808 0.01760 -0.0335 1.0000 0.1031
-3.750 -0.3039 0.02585 0.01514 -0.0324 1.0000 0.1079
-3.500 -0.2781 0.02380 0.01279 -0.0310 1.0000 0.1159
-3.250 -0.2540 0.02199 0.01104 -0.0296 1.0000 0.1398
-3.000 -0.2308 0.01950 0.00921 -0.0284 1.0000 0.2400
-2.750 -0.1430 0.01527 0.00759 -0.0313 1.0000 1.0000
-2.500 -0.1349 0.01496 0.00691 -0.0292 1.0000 1.0000
-2.250 -0.1229 0.01480 0.00640 -0.0272 1.0000 1.0000
-2.000 -0.1081 0.01472 0.00597 -0.0255 1.0000 1.0000
-1.750 -0.0914 0.01469 0.00563 -0.0240 1.0000 1.0000
-1.500 -0.0736 0.01469 0.00535 -0.0227 1.0000 1.0000
-1.250 -0.0550 0.01473 0.00510 -0.0215 1.0000 1.0000
-1.000 -0.0358 0.01480 0.00494 -0.0204 1.0000 1.0000
-0.750 -0.0164 0.01490 0.00485 -0.0194 1.0000 1.0000
-0.500 0.0034 0.01503 0.00481 -0.0185 1.0000 1.0000
-0.250 0.0232 0.01520 0.00483 -0.0177 1.0000 1.0000
0.000 0.0430 0.01539 0.00488 -0.0169 1.0000 1.0000
0.250 0.0628 0.01562 0.00500 -0.0162 1.0000 1.0000
0.500 0.0825 0.01589 0.00519 -0.0155 1.0000 1.0000
0.750 0.1019 0.01621 0.00544 -0.0149 1.0000 1.0000
1.000 0.1211 0.01656 0.00576 -0.0144 1.0000 1.0000
1.250 0.1399 0.01698 0.00614 -0.0140 1.0000 1.0000
1.500 0.1583 0.01745 0.00661 -0.0136 1.0000 1.0000
1.750 0.1763 0.01798 0.00716 -0.0134 1.0000 1.0000
2.000 0.1937 0.01860 0.00780 -0.0132 1.0000 1.0000
2.250 0.2105 0.01929 0.00853 -0.0132 1.0000 1.0000
2.500 0.2383 0.02024 0.00959 -0.0154 0.9947 1.0000
2.750 0.3091 0.02159 0.01118 -0.0253 0.9657 1.0000
3.000 0.3779 0.02260 0.01250 -0.0340 0.9344 1.0000
3.250 0.4536 0.02316 0.01354 -0.0428 0.9015 1.0000
3.500 0.5146 0.02326 0.01407 -0.0477 0.8649 1.0000
3.750 0.5700 0.02293 0.01423 -0.0502 0.8275 1.0000
4.000 0.6124 0.02235 0.01401 -0.0493 0.7884 1.0000
4.250 0.6417 0.02185 0.01377 -0.0460 0.7452 1.0000
4.500 0.6657 0.02138 0.01349 -0.0417 0.6969 1.0000
4.750 0.6870 0.02100 0.01325 -0.0370 0.6413 1.0000
5.000 0.7044 0.02068 0.01283 -0.0316 0.5688 1.0000
5.250 0.7126 0.02053 0.01216 -0.0254 0.4516 1.0000
5.500 0.7124 0.02296 0.01291 -0.0203 0.2250 1.0000
5.750 0.7280 0.02651 0.01548 -0.0182 0.1303 1.0000
6.000 0.7535 0.02912 0.01782 -0.0169 0.1101 1.0000
6.250 0.7823 0.03160 0.02060 -0.0158 0.1009 1.0000
6.500 0.8094 0.03468 0.02384 -0.0150 0.0958 1.0000
6.750 0.8334 0.03759 0.02733 -0.0139 0.0914 1.0000
7.000 0.8553 0.04062 0.03068 -0.0130 0.0874 1.0000
7.250 0.8749 0.04434 0.03487 -0.0120 0.0866 1.0000
7.500 0.8885 0.04888 0.04021 -0.0108 0.0889 1.0000
7.750 0.8979 0.05391 0.04584 -0.0100 0.0919 1.0000
8.000 0.9060 0.05897 0.05129 -0.0094 0.0949 1.0000
8.250 0.9120 0.06411 0.05683 -0.0091 0.0988 1.0000
8.500 0.8932 0.07099 0.06429 -0.0104 0.1053 1.0000
8.750 0.8983 0.07665 0.07007 -0.0108 0.1117 1.0000
9.000 0.8564 0.08391 0.07755 -0.0155 0.1167 1.0000
9.250 0.8450 0.09074 0.08440 -0.0189 0.1260 1.0000
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Polar data table (+)
Polar graphs
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