SOMERS S102 AIRFOIL (BLUNT) (s102b-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: SOMERS S102 AIRFOIL (BLUNT) (s102b-il) Reynolds number: 1,000,000 Max Cl/Cd: 85.33 at α=8.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-s102b-il-1000000-n5.txt Download as CSV file: xf-s102b-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: SOMERS S102 AIRFOIL (BLUNT)
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-13.500 -0.7261 0.06882 0.06680 -0.0536 1.0000 0.0036
-13.250 -0.7674 0.05859 0.05631 -0.0593 1.0000 0.0036
-13.000 -0.7974 0.05141 0.04889 -0.0623 1.0000 0.0036
-12.750 -0.8175 0.04603 0.04329 -0.0639 1.0000 0.0036
-12.500 -0.8307 0.04172 0.03876 -0.0648 1.0000 0.0036
-12.250 -0.8392 0.03808 0.03492 -0.0651 1.0000 0.0036
-12.000 -0.8403 0.03488 0.03151 -0.0659 0.9886 0.0036
-11.750 -0.8328 0.03206 0.02846 -0.0674 0.9667 0.0036
-11.500 -0.8273 0.02983 0.02600 -0.0673 0.9412 0.0037
-11.250 -0.8209 0.02799 0.02394 -0.0665 0.9161 0.0037
-11.000 -0.8122 0.02636 0.02206 -0.0658 0.8911 0.0037
-10.750 -0.8002 0.02493 0.02041 -0.0654 0.8667 0.0037
-10.500 -0.7840 0.02363 0.01887 -0.0652 0.8457 0.0038
-10.000 -0.7465 0.02143 0.01630 -0.0647 0.8150 0.0038
-9.750 -0.7258 0.02047 0.01519 -0.0645 0.8030 0.0038
-9.500 -0.7042 0.01959 0.01415 -0.0644 0.7924 0.0039
-9.250 -0.6819 0.01877 0.01320 -0.0643 0.7823 0.0039
-9.000 -0.6588 0.01801 0.01233 -0.0642 0.7737 0.0039
-8.750 -0.6352 0.01731 0.01151 -0.0642 0.7653 0.0039
-8.500 -0.6107 0.01670 0.01082 -0.0643 0.7581 0.0040
-8.250 -0.5858 0.01615 0.01018 -0.0644 0.7507 0.0040
-8.000 -0.5614 0.01544 0.00938 -0.0644 0.7444 0.0041
-7.750 -0.5371 0.01467 0.00853 -0.0646 0.7377 0.0042
-7.500 -0.5116 0.01409 0.00787 -0.0648 0.7316 0.0043
-7.250 -0.4852 0.01358 0.00730 -0.0651 0.7262 0.0044
-7.000 -0.4585 0.01311 0.00678 -0.0654 0.7209 0.0045
-6.750 -0.4315 0.01269 0.00630 -0.0657 0.7162 0.0046
-6.500 -0.4039 0.01228 0.00585 -0.0661 0.7121 0.0047
-6.250 -0.3760 0.01191 0.00544 -0.0665 0.7078 0.0048
-6.000 -0.3479 0.01158 0.00507 -0.0669 0.7036 0.0049
-5.500 -0.2910 0.01098 0.00439 -0.0678 0.6966 0.0053
-5.250 -0.2622 0.01072 0.00409 -0.0683 0.6931 0.0056
-5.000 -0.2333 0.01048 0.00382 -0.0688 0.6895 0.0060
-4.750 -0.2043 0.01023 0.00355 -0.0693 0.6860 0.0069
-4.500 -0.1752 0.01003 0.00332 -0.0698 0.6829 0.0083
-4.250 -0.1459 0.00981 0.00311 -0.0703 0.6801 0.0113
-4.000 -0.1165 0.00960 0.00292 -0.0709 0.6773 0.0166
-3.750 -0.0870 0.00940 0.00275 -0.0715 0.6745 0.0253
-3.500 -0.0575 0.00920 0.00259 -0.0721 0.6719 0.0378
-3.250 -0.0279 0.00886 0.00238 -0.0729 0.6694 0.0780
-3.000 0.0025 0.00807 0.00205 -0.0743 0.6672 0.2075
-2.750 0.0349 0.00642 0.00155 -0.0771 0.6652 0.5429
-2.500 0.0649 0.00645 0.00158 -0.0776 0.6630 0.5597
-2.250 0.0948 0.00653 0.00165 -0.0780 0.6606 0.5739
-2.000 0.1248 0.00668 0.00175 -0.0783 0.6582 0.5846
-1.750 0.1546 0.00669 0.00171 -0.0788 0.6559 0.5855
-1.500 0.1842 0.00668 0.00167 -0.0792 0.6535 0.5864
-1.250 0.2140 0.00668 0.00164 -0.0797 0.6503 0.5873
-1.000 0.2437 0.00666 0.00161 -0.0801 0.6450 0.5880
-0.750 0.2732 0.00668 0.00158 -0.0805 0.6395 0.5887
-0.500 0.3027 0.00669 0.00157 -0.0809 0.6333 0.5893
-0.250 0.3322 0.00670 0.00155 -0.0813 0.6258 0.5900
0.000 0.3615 0.00674 0.00154 -0.0816 0.6196 0.5907
0.250 0.3912 0.00675 0.00154 -0.0820 0.6125 0.5914
0.500 0.4203 0.00680 0.00155 -0.0824 0.6037 0.5920
0.750 0.4496 0.00683 0.00155 -0.0827 0.5924 0.5928
1.000 0.4787 0.00688 0.00157 -0.0830 0.5793 0.5935
1.250 0.5075 0.00696 0.00159 -0.0833 0.5625 0.5942
1.500 0.5355 0.00711 0.00163 -0.0835 0.5327 0.5949
1.750 0.5591 0.00772 0.00184 -0.0830 0.4423 0.5958
2.000 0.5825 0.00839 0.00214 -0.0825 0.3603 0.5967
2.250 0.6070 0.00893 0.00239 -0.0822 0.2969 0.5975
2.500 0.6324 0.00935 0.00260 -0.0821 0.2503 0.5983
2.750 0.6587 0.00966 0.00278 -0.0820 0.2209 0.5990
3.000 0.6854 0.00993 0.00295 -0.0820 0.1993 0.5997
3.250 0.7123 0.01016 0.00310 -0.0820 0.1826 0.6003
3.500 0.7393 0.01039 0.00327 -0.0821 0.1695 0.6009
3.750 0.7663 0.01059 0.00342 -0.0821 0.1592 0.6016
4.000 0.7934 0.01077 0.00358 -0.0822 0.1509 0.6026
4.250 0.8201 0.01098 0.00376 -0.0822 0.1426 0.6036
4.500 0.8473 0.01114 0.00392 -0.0822 0.1380 0.6045
4.750 0.8743 0.01132 0.00410 -0.0823 0.1335 0.6055
5.000 0.9008 0.01152 0.00429 -0.0822 0.1288 0.6065
5.250 0.9276 0.01170 0.00448 -0.0822 0.1257 0.6074
5.500 0.9544 0.01188 0.00467 -0.0822 0.1231 0.6085
5.750 0.9806 0.01208 0.00488 -0.0821 0.1197 0.6095
6.000 1.0065 0.01231 0.00510 -0.0820 0.1159 0.6106
6.250 1.0323 0.01254 0.00534 -0.0818 0.1129 0.6117
6.500 1.0585 0.01273 0.00557 -0.0817 0.1115 0.6128
6.750 1.0843 0.01293 0.00580 -0.0816 0.1094 0.6139
7.000 1.1096 0.01317 0.00604 -0.0814 0.1068 0.6151
7.250 1.1344 0.01343 0.00631 -0.0811 0.1039 0.6163
7.500 1.1587 0.01372 0.00660 -0.0807 0.1007 0.6173
7.750 1.1834 0.01396 0.00688 -0.0804 0.0990 0.6186
8.000 1.2081 0.01418 0.00715 -0.0800 0.0973 0.6200
8.250 1.2321 0.01444 0.00745 -0.0796 0.0950 0.6214
8.500 1.2554 0.01474 0.00776 -0.0791 0.0920 0.6229
8.750 1.2779 0.01507 0.00810 -0.0785 0.0889 0.6244
9.000 1.3004 0.01538 0.00845 -0.0778 0.0867 0.6260
9.250 1.3229 0.01567 0.00879 -0.0772 0.0845 0.6276
9.500 1.3443 0.01601 0.00915 -0.0764 0.0813 0.6292
9.750 1.3626 0.01640 0.00954 -0.0750 0.0777 0.6308
10.000 1.3800 0.01678 0.00995 -0.0735 0.0749 0.6323
10.500 1.4153 0.01776 0.01094 -0.0708 0.0652 0.6359
10.750 1.4329 0.01827 0.01149 -0.0696 0.0611 0.6380
11.000 1.4481 0.01895 0.01215 -0.0681 0.0558 0.6402
11.250 1.4637 0.01961 0.01284 -0.0668 0.0509 0.6425
11.500 1.4775 0.02040 0.01364 -0.0652 0.0459 0.6449
11.750 1.4907 0.02126 0.01450 -0.0637 0.0411 0.6474
12.250 1.5145 0.02325 0.01650 -0.0606 0.0311 0.6528
12.500 1.5250 0.02438 0.01764 -0.0591 0.0266 0.6561
12.750 1.5351 0.02558 0.01886 -0.0576 0.0224 0.6594
13.000 1.5463 0.02672 0.02004 -0.0563 0.0194 0.6627
13.500 1.5664 0.02925 0.02265 -0.0538 0.0148 0.6696
13.750 1.5765 0.03056 0.02401 -0.0526 0.0131 0.6739
14.250 1.5940 0.03344 0.02701 -0.0504 0.0101 0.6827
14.500 1.6013 0.03505 0.02869 -0.0493 0.0089 0.6879
14.750 1.6094 0.03659 0.03032 -0.0483 0.0081 0.6938
15.000 1.6158 0.03832 0.03212 -0.0474 0.0073 0.6997
15.250 1.6218 0.04012 0.03401 -0.0465 0.0067 0.7069
15.750 1.6322 0.04394 0.03802 -0.0449 0.0057 0.7233
16.000 1.6352 0.04612 0.04030 -0.0442 0.0052 0.7330
16.250 1.6385 0.04836 0.04265 -0.0436 0.0049 0.7449
16.500 1.6412 0.05071 0.04514 -0.0431 0.0046 0.7595
16.750 1.6426 0.05324 0.04781 -0.0427 0.0043 0.7788
17.000 1.6426 0.05600 0.05073 -0.0425 0.0040 0.8067
17.250 1.6411 0.05878 0.05382 -0.0421 0.0038 0.8954
17.500 1.6355 0.06169 0.05691 -0.0413 0.0036 1.0000
17.750 1.6329 0.06500 0.06032 -0.0415 0.0035 1.0000
18.000 1.6284 0.06862 0.06404 -0.0418 0.0033 1.0000
18.250 1.6222 0.07259 0.06812 -0.0423 0.0031 1.0000
18.500 1.6138 0.07700 0.07265 -0.0432 0.0030 1.0000
18.750 1.6035 0.08182 0.07759 -0.0443 0.0029 1.0000
19.000 1.5899 0.08729 0.08318 -0.0459 0.0027 1.0000
19.250 1.5730 0.09351 0.08954 -0.0480 0.0026 1.0000
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