SD5060 (9.5%) (sd5060-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: SD5060 (9.5%) (sd5060-il) Reynolds number: 500,000 Max Cl/Cd: 79.78 at α=6.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-sd5060-il-500000-n5.txt Download as CSV file: xf-sd5060-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: SD5060 (9.5%)
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-12.000 -0.7289 0.07684 0.07440 -0.0204 1.0000 0.0084
-11.750 -0.7758 0.06336 0.06083 -0.0294 1.0000 0.0083
-11.500 -0.8154 0.05057 0.04791 -0.0397 1.0000 0.0081
-11.250 -0.8442 0.04058 0.03770 -0.0509 1.0000 0.0079
-11.000 -0.8558 0.03614 0.03297 -0.0530 1.0000 0.0080
-10.750 -0.8525 0.03299 0.02953 -0.0537 1.0000 0.0082
-10.500 -0.8433 0.03035 0.02661 -0.0540 1.0000 0.0084
-10.250 -0.8297 0.02814 0.02410 -0.0540 1.0000 0.0086
-10.000 -0.8124 0.02643 0.02216 -0.0539 1.0000 0.0088
-9.750 -0.7971 0.02415 0.01965 -0.0538 1.0000 0.0091
-9.500 -0.7761 0.02297 0.01836 -0.0536 1.0000 0.0094
-9.250 -0.7538 0.02204 0.01733 -0.0535 1.0000 0.0097
-9.000 -0.7314 0.02105 0.01623 -0.0532 1.0000 0.0100
-8.750 -0.7088 0.02010 0.01515 -0.0529 1.0000 0.0104
-8.500 -0.6811 0.01923 0.01414 -0.0536 0.9915 0.0109
-8.250 -0.6495 0.01837 0.01312 -0.0549 0.9802 0.0116
-8.000 -0.6182 0.01758 0.01219 -0.0560 0.9701 0.0120
-7.750 -0.5890 0.01688 0.01134 -0.0566 0.9589 0.0123
-7.500 -0.5635 0.01568 0.01000 -0.0566 0.9470 0.0128
-7.250 -0.5388 0.01485 0.00908 -0.0563 0.9355 0.0133
-7.000 -0.5141 0.01428 0.00841 -0.0558 0.9248 0.0139
-6.750 -0.4891 0.01382 0.00786 -0.0553 0.9143 0.0146
-6.500 -0.4639 0.01334 0.00730 -0.0548 0.9042 0.0153
-6.250 -0.4384 0.01287 0.00672 -0.0543 0.8948 0.0158
-6.000 -0.4127 0.01243 0.00617 -0.0538 0.8853 0.0163
-5.750 -0.3864 0.01203 0.00567 -0.0534 0.8761 0.0167
-5.500 -0.3602 0.01161 0.00516 -0.0530 0.8673 0.0171
-5.250 -0.3337 0.01114 0.00461 -0.0527 0.8581 0.0182
-5.000 -0.3068 0.01080 0.00420 -0.0525 0.8494 0.0195
-4.750 -0.2798 0.01052 0.00384 -0.0522 0.8406 0.0207
-4.500 -0.2524 0.01027 0.00351 -0.0520 0.8317 0.0219
-4.250 -0.2250 0.01002 0.00320 -0.0517 0.8231 0.0243
-4.000 -0.1975 0.00974 0.00292 -0.0516 0.8140 0.0306
-3.750 -0.1703 0.00941 0.00264 -0.0514 0.8053 0.0517
-3.500 -0.1429 0.00915 0.00242 -0.0513 0.7963 0.0739
-3.250 -0.1153 0.00889 0.00224 -0.0512 0.7870 0.1002
-3.000 -0.0877 0.00867 0.00208 -0.0511 0.7780 0.1260
-2.750 -0.0599 0.00853 0.00195 -0.0510 0.7683 0.1433
-2.500 -0.0320 0.00838 0.00184 -0.0509 0.7588 0.1638
-2.250 -0.0041 0.00825 0.00173 -0.0508 0.7492 0.1864
-2.000 0.0238 0.00812 0.00163 -0.0507 0.7388 0.2093
-1.750 0.0517 0.00797 0.00155 -0.0506 0.7283 0.2385
-1.500 0.0795 0.00784 0.00148 -0.0506 0.7176 0.2720
-1.250 0.1073 0.00773 0.00141 -0.0505 0.7062 0.3019
-1.000 0.1353 0.00763 0.00136 -0.0504 0.6940 0.3303
-0.750 0.1632 0.00754 0.00132 -0.0503 0.6811 0.3632
-0.500 0.1910 0.00745 0.00128 -0.0502 0.6674 0.3971
-0.250 0.2187 0.00736 0.00126 -0.0501 0.6525 0.4374
0.000 0.2462 0.00728 0.00125 -0.0500 0.6367 0.4804
0.250 0.2737 0.00720 0.00125 -0.0498 0.6201 0.5281
0.500 0.3010 0.00712 0.00127 -0.0496 0.6033 0.5781
0.750 0.3281 0.00704 0.00130 -0.0494 0.5860 0.6332
1.000 0.3548 0.00696 0.00135 -0.0490 0.5678 0.6912
1.250 0.3807 0.00689 0.00140 -0.0485 0.5484 0.7531
1.500 0.4054 0.00682 0.00147 -0.0475 0.5279 0.8195
1.750 0.4283 0.00677 0.00153 -0.0461 0.5056 0.8929
2.000 0.4640 0.00682 0.00157 -0.0475 0.4793 0.9742
2.250 0.4953 0.00700 0.00163 -0.0483 0.4539 1.0000
2.500 0.5222 0.00722 0.00172 -0.0481 0.4276 1.0000
2.750 0.5491 0.00745 0.00183 -0.0479 0.4004 1.0000
3.000 0.5759 0.00771 0.00195 -0.0477 0.3714 1.0000
3.250 0.6025 0.00798 0.00209 -0.0475 0.3428 1.0000
3.500 0.6293 0.00824 0.00225 -0.0474 0.3179 1.0000
3.750 0.6559 0.00852 0.00242 -0.0472 0.2919 1.0000
4.000 0.6823 0.00883 0.00261 -0.0470 0.2658 1.0000
4.250 0.7088 0.00913 0.00280 -0.0468 0.2442 1.0000
4.500 0.7353 0.00941 0.00302 -0.0466 0.2257 1.0000
4.750 0.7617 0.00971 0.00324 -0.0464 0.2066 1.0000
5.000 0.7881 0.01001 0.00347 -0.0462 0.1900 1.0000
5.250 0.8145 0.01029 0.00371 -0.0460 0.1765 1.0000
5.500 0.8406 0.01060 0.00397 -0.0458 0.1625 1.0000
5.750 0.8668 0.01090 0.00423 -0.0455 0.1508 1.0000
6.000 0.8928 0.01122 0.00451 -0.0453 0.1397 1.0000
6.500 0.9446 0.01184 0.00510 -0.0448 0.1209 1.0000
6.750 0.9701 0.01218 0.00542 -0.0445 0.1117 1.0000
7.000 0.9954 0.01256 0.00576 -0.0441 0.1029 1.0000
7.250 1.0210 0.01286 0.00609 -0.0438 0.0968 1.0000
7.750 1.0711 0.01360 0.00684 -0.0431 0.0830 1.0000
8.000 1.0955 0.01402 0.00725 -0.0427 0.0762 1.0000
8.250 1.1199 0.01442 0.00765 -0.0423 0.0686 1.0000
8.500 1.1438 0.01487 0.00811 -0.0418 0.0614 1.0000
8.750 1.1669 0.01540 0.00860 -0.0413 0.0524 1.0000
9.000 1.1897 0.01594 0.00912 -0.0407 0.0447 1.0000
9.250 1.2124 0.01647 0.00966 -0.0401 0.0389 1.0000
9.500 1.2341 0.01709 0.01026 -0.0394 0.0332 1.0000
9.750 1.2560 0.01766 0.01085 -0.0387 0.0288 1.0000
10.000 1.2768 0.01832 0.01154 -0.0379 0.0244 1.0000
10.250 1.2972 0.01897 0.01222 -0.0371 0.0209 1.0000
10.500 1.3170 0.01966 0.01294 -0.0362 0.0180 1.0000
10.750 1.3355 0.02041 0.01373 -0.0351 0.0150 1.0000
11.000 1.3534 0.02119 0.01455 -0.0340 0.0123 1.0000
11.250 1.3694 0.02207 0.01548 -0.0327 0.0101 1.0000
11.500 1.3846 0.02295 0.01643 -0.0313 0.0086 1.0000
11.750 1.3967 0.02394 0.01749 -0.0295 0.0075 1.0000
12.000 1.4066 0.02486 0.01850 -0.0273 0.0067 1.0000
12.250 1.4147 0.02589 0.01962 -0.0251 0.0062 1.0000
12.500 1.4214 0.02708 0.02090 -0.0231 0.0058 1.0000
12.750 1.4258 0.02851 0.02242 -0.0211 0.0054 1.0000
13.000 1.4308 0.02999 0.02401 -0.0194 0.0051 1.0000
13.250 1.4362 0.03152 0.02566 -0.0181 0.0048 1.0000
13.500 1.4399 0.03329 0.02755 -0.0169 0.0047 1.0000
13.750 1.4422 0.03530 0.02968 -0.0160 0.0045 1.0000
14.000 1.4430 0.03758 0.03209 -0.0153 0.0044 1.0000
14.250 1.4424 0.04016 0.03481 -0.0149 0.0043 1.0000
14.500 1.4400 0.04309 0.03787 -0.0149 0.0042 1.0000
14.750 1.4366 0.04632 0.04124 -0.0153 0.0041 1.0000
15.000 1.4300 0.05018 0.04525 -0.0162 0.0040 1.0000
15.250 1.4224 0.05440 0.04961 -0.0175 0.0040 1.0000
15.500 1.4114 0.05940 0.05476 -0.0194 0.0039 1.0000
15.750 1.3993 0.06486 0.06038 -0.0219 0.0039 1.0000
16.000 1.3835 0.07131 0.06699 -0.0250 0.0038 1.0000
16.250 1.3667 0.07831 0.07416 -0.0287 0.0038 1.0000
16.500 1.3484 0.08598 0.08198 -0.0329 0.0038 1.0000
16.750 1.3256 0.09483 0.09101 -0.0378 0.0038 1.0000
17.000 1.3027 0.10405 0.10040 -0.0429 0.0039 1.0000
17.250 1.2785 0.11375 0.11026 -0.0484 0.0039 1.0000
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