S8036 (16%) (s8036-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: S8036 (16%) (s8036-il) Reynolds number: 1,000,000 Max Cl/Cd: 99.6 at α=5.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-s8036-il-1000000.txt Download as CSV file: xf-s8036-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: S8036 (16%)
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.250 -0.7908 0.11841 0.11595 -0.0380 1.0000 0.0087
-18.000 -0.8336 0.10563 0.10294 -0.0449 1.0000 0.0085
-17.750 -0.8703 0.09475 0.09187 -0.0508 1.0000 0.0086
-17.500 -0.8891 0.08746 0.08444 -0.0548 1.0000 0.0085
-17.250 -0.8796 0.08501 0.08196 -0.0562 1.0000 0.0083
-17.000 -0.9160 0.07538 0.07212 -0.0613 1.0000 0.0084
-16.750 -0.9234 0.07062 0.06725 -0.0637 1.0000 0.0083
-16.500 -0.9306 0.06610 0.06264 -0.0660 1.0000 0.0083
-16.250 -0.9503 0.06019 0.05657 -0.0685 1.0000 0.0084
-16.000 -0.9525 0.05683 0.05313 -0.0698 1.0000 0.0083
-15.750 -0.9723 0.05161 0.04774 -0.0712 1.0000 0.0084
-15.500 -0.9809 0.04801 0.04402 -0.0718 1.0000 0.0084
-15.250 -0.9897 0.04457 0.04046 -0.0721 1.0000 0.0085
-15.000 -0.9965 0.04153 0.03734 -0.0720 1.0000 0.0086
-14.750 -0.9987 0.03906 0.03475 -0.0716 1.0000 0.0086
-14.500 -0.9989 0.03690 0.03252 -0.0710 1.0000 0.0086
-14.250 -1.0000 0.03477 0.03031 -0.0701 1.0000 0.0087
-14.000 -0.9964 0.03315 0.02863 -0.0691 1.0000 0.0088
-13.750 -0.9949 0.03145 0.02687 -0.0679 1.0000 0.0089
-13.500 -0.9908 0.03005 0.02540 -0.0665 1.0000 0.0090
-13.250 -0.9886 0.02857 0.02386 -0.0647 1.0000 0.0092
-13.000 -0.9867 0.02716 0.02237 -0.0626 1.0000 0.0092
-12.750 -0.9836 0.02595 0.02109 -0.0603 1.0000 0.0092
-12.500 -0.9773 0.02509 0.02017 -0.0581 1.0000 0.0096
-12.250 -0.9759 0.02400 0.01901 -0.0551 1.0000 0.0094
-12.000 -0.9731 0.02315 0.01810 -0.0519 1.0000 0.0096
-11.750 -0.9704 0.02243 0.01732 -0.0484 1.0000 0.0098
-11.500 -0.9630 0.02152 0.01634 -0.0459 0.9994 0.0098
-11.250 -0.9344 0.02060 0.01536 -0.0474 0.9972 0.0100
-11.000 -0.9037 0.01980 0.01450 -0.0491 0.9947 0.0102
-10.750 -0.8751 0.01903 0.01367 -0.0502 0.9915 0.0104
-10.500 -0.8470 0.01822 0.01280 -0.0512 0.9869 0.0105
-10.250 -0.8295 0.01712 0.01163 -0.0503 0.9776 0.0109
-9.750 -0.7804 0.01571 0.01014 -0.0502 0.9493 0.0114
-9.500 -0.7358 0.01494 0.00933 -0.0544 0.9410 0.0119
-9.250 -0.6798 0.01419 0.00853 -0.0610 0.9333 0.0126
-9.000 -0.6231 0.01343 0.00768 -0.0678 0.9176 0.0132
-8.750 -0.5878 0.01286 0.00698 -0.0699 0.8868 0.0141
-8.500 -0.5699 0.01263 0.00662 -0.0681 0.8588 0.0149
-8.250 -0.5534 0.01244 0.00632 -0.0659 0.8375 0.0155
-8.000 -0.5375 0.01214 0.00592 -0.0636 0.8207 0.0167
-7.750 -0.5194 0.01191 0.00563 -0.0618 0.8067 0.0181
-7.250 -0.4814 0.01142 0.00504 -0.0584 0.7837 0.0229
-7.000 -0.4618 0.01119 0.00477 -0.0568 0.7741 0.0266
-6.750 -0.4418 0.01093 0.00451 -0.0553 0.7648 0.0312
-6.500 -0.4212 0.01070 0.00427 -0.0539 0.7568 0.0364
-6.250 -0.4001 0.01046 0.00404 -0.0526 0.7489 0.0433
-6.000 -0.3793 0.01025 0.00382 -0.0513 0.7415 0.0523
-5.750 -0.3575 0.01000 0.00362 -0.0501 0.7348 0.0630
-5.500 -0.3358 0.00978 0.00343 -0.0489 0.7283 0.0757
-5.250 -0.3141 0.00956 0.00324 -0.0478 0.7224 0.0915
-5.000 -0.2926 0.00928 0.00306 -0.0466 0.7165 0.1138
-4.750 -0.2718 0.00900 0.00287 -0.0452 0.7105 0.1425
-4.500 -0.2520 0.00866 0.00268 -0.0437 0.7049 0.1836
-4.250 -0.2322 0.00828 0.00250 -0.0422 0.6996 0.2323
-4.000 -0.2143 0.00784 0.00230 -0.0404 0.6943 0.2996
-3.750 -0.1955 0.00746 0.00213 -0.0386 0.6890 0.3646
-3.500 -0.1755 0.00710 0.00199 -0.0371 0.6842 0.4268
-3.250 -0.1542 0.00684 0.00189 -0.0358 0.6788 0.4774
-3.000 -0.1325 0.00667 0.00182 -0.0345 0.6737 0.5209
-2.750 -0.1085 0.00655 0.00179 -0.0336 0.6691 0.5532
-2.500 -0.0832 0.00648 0.00176 -0.0330 0.6639 0.5752
-2.250 -0.0577 0.00646 0.00173 -0.0324 0.6586 0.5904
-2.000 -0.0319 0.00645 0.00171 -0.0319 0.6535 0.6035
-1.750 -0.0055 0.00641 0.00169 -0.0315 0.6486 0.6166
-1.500 0.0206 0.00641 0.00167 -0.0311 0.6434 0.6290
-1.250 0.0464 0.00642 0.00166 -0.0306 0.6381 0.6387
-0.750 0.0994 0.00638 0.00165 -0.0298 0.6284 0.6586
-0.500 0.1254 0.00640 0.00164 -0.0294 0.6233 0.6684
-0.250 0.1519 0.00640 0.00165 -0.0290 0.6183 0.6767
0.000 0.1789 0.00640 0.00164 -0.0288 0.6129 0.6837
0.250 0.2047 0.00641 0.00164 -0.0283 0.6072 0.6910
0.500 0.2315 0.00643 0.00165 -0.0280 0.6016 0.6976
0.750 0.2581 0.00642 0.00165 -0.0277 0.5956 0.7038
1.000 0.2839 0.00644 0.00167 -0.0272 0.5896 0.7104
1.250 0.3108 0.00646 0.00168 -0.0270 0.5839 0.7169
1.500 0.3369 0.00646 0.00170 -0.0266 0.5773 0.7235
1.750 0.3622 0.00650 0.00172 -0.0260 0.5703 0.7313
2.000 0.3885 0.00651 0.00174 -0.0257 0.5626 0.7385
2.250 0.4132 0.00655 0.00178 -0.0250 0.5546 0.7462
2.500 0.4397 0.00657 0.00180 -0.0247 0.5469 0.7539
2.750 0.4643 0.00660 0.00185 -0.0240 0.5394 0.7620
3.000 0.4903 0.00662 0.00189 -0.0236 0.5316 0.7706
3.250 0.5144 0.00666 0.00194 -0.0228 0.5227 0.7799
3.500 0.5397 0.00669 0.00199 -0.0222 0.5141 0.7899
3.750 0.5632 0.00674 0.00205 -0.0213 0.5047 0.8011
4.000 0.5869 0.00679 0.00212 -0.0205 0.4923 0.8130
4.250 0.6101 0.00685 0.00219 -0.0195 0.4794 0.8264
4.750 0.6539 0.00702 0.00238 -0.0170 0.4495 0.8594
5.000 0.6766 0.00711 0.00250 -0.0160 0.4343 0.8800
5.250 0.7035 0.00723 0.00266 -0.0159 0.4166 0.9048
5.500 0.7415 0.00751 0.00291 -0.0184 0.3926 0.9272
5.750 0.7888 0.00792 0.00321 -0.0231 0.3625 0.9389
6.000 0.8344 0.00838 0.00354 -0.0275 0.3309 0.9467
6.250 0.8716 0.00884 0.00388 -0.0299 0.3028 0.9553
6.500 0.8997 0.00931 0.00423 -0.0304 0.2767 0.9670
6.750 0.9243 0.00978 0.00458 -0.0301 0.2514 0.9788
7.000 0.9522 0.01024 0.00493 -0.0305 0.2300 0.9856
7.250 0.9845 0.01069 0.00528 -0.0320 0.2090 0.9899
7.500 1.0151 0.01116 0.00565 -0.0331 0.1904 0.9939
7.750 1.0493 0.01162 0.00601 -0.0351 0.1717 0.9965
8.000 1.0834 0.01204 0.00635 -0.0371 0.1577 0.9990
8.250 1.1063 0.01237 0.00664 -0.0366 0.1474 1.0000
8.500 1.1081 0.01263 0.00688 -0.0316 0.1397 1.0000
8.750 1.1130 0.01287 0.00710 -0.0272 0.1336 1.0000
9.000 1.1184 0.01320 0.00740 -0.0230 0.1261 1.0000
9.250 1.1277 0.01350 0.00769 -0.0197 0.1204 1.0000
9.500 1.1353 0.01391 0.00807 -0.0162 0.1139 1.0000
9.750 1.1471 0.01423 0.00841 -0.0135 0.1098 1.0000
10.000 1.1567 0.01467 0.00883 -0.0106 0.1045 1.0000
10.250 1.1669 0.01514 0.00929 -0.0079 0.0997 1.0000
10.500 1.1789 0.01558 0.00975 -0.0055 0.0962 1.0000
10.750 1.1892 0.01613 0.01029 -0.0031 0.0924 1.0000
11.000 1.1989 0.01675 0.01092 -0.0006 0.0885 1.0000
11.250 1.2123 0.01726 0.01147 0.0012 0.0864 1.0000
11.500 1.2237 0.01790 0.01211 0.0032 0.0835 1.0000
11.750 1.2334 0.01867 0.01288 0.0052 0.0803 1.0000
12.000 1.2432 0.01948 0.01372 0.0071 0.0775 1.0000
12.250 1.2565 0.02015 0.01444 0.0085 0.0758 1.0000
12.500 1.2683 0.02095 0.01526 0.0099 0.0739 1.0000
12.750 1.2785 0.02187 0.01620 0.0114 0.0716 1.0000
13.000 1.2869 0.02295 0.01730 0.0130 0.0692 1.0000
13.250 1.2976 0.02394 0.01833 0.0142 0.0670 1.0000
13.500 1.3099 0.02484 0.01927 0.0152 0.0653 1.0000
13.750 1.3202 0.02591 0.02037 0.0163 0.0636 1.0000
14.000 1.3287 0.02713 0.02161 0.0175 0.0615 1.0000
14.250 1.3344 0.02860 0.02311 0.0187 0.0594 1.0000
14.500 1.3453 0.02970 0.02426 0.0195 0.0577 1.0000
14.750 1.3558 0.03086 0.02547 0.0203 0.0561 1.0000
15.000 1.3636 0.03226 0.02689 0.0212 0.0542 1.0000
15.250 1.3693 0.03386 0.02851 0.0220 0.0523 1.0000
15.500 1.3749 0.03551 0.03020 0.0228 0.0503 1.0000
15.750 1.3841 0.03688 0.03163 0.0234 0.0488 1.0000
16.000 1.3902 0.03855 0.03336 0.0240 0.0477 1.0000
16.250 1.3952 0.04036 0.03518 0.0245 0.0457 1.0000
16.500 1.3966 0.04256 0.03741 0.0251 0.0440 1.0000
16.750 1.4024 0.04438 0.03929 0.0254 0.0429 1.0000
17.000 1.4080 0.04625 0.04123 0.0257 0.0419 1.0000
17.250 1.4122 0.04831 0.04334 0.0259 0.0405 1.0000
17.500 1.4127 0.05078 0.04583 0.0260 0.0387 1.0000
17.750 1.4122 0.05341 0.04851 0.0261 0.0378 1.0000
18.000 1.4144 0.05579 0.05097 0.0261 0.0370 1.0000
18.250 1.4182 0.05805 0.05329 0.0260 0.0359 1.0000
18.500 1.4187 0.06071 0.05602 0.0258 0.0349 1.0000
18.750 1.4178 0.06358 0.05894 0.0255 0.0342 1.0000
19.000 1.4150 0.06669 0.06211 0.0250 0.0333 1.0000
19.250 1.4074 0.07048 0.06595 0.0244 0.0321 1.0000
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Polar data table (+)
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