S3016-095-87 (s3016-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: S3016-095-87 (s3016-il) Reynolds number: 1,000,000 Max Cl/Cd: 93.28 at α=6.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-s3016-il-1000000-n5.txt Download as CSV file: xf-s3016-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: S3016-095-87
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
------ -------- --------- --------- -------- -------- --------
-12.250 -0.9406 0.03962 0.03756 -0.0484 1.0000 0.0028
-12.000 -0.9651 0.03537 0.03306 -0.0469 1.0000 0.0028
-11.750 -0.9706 0.03181 0.02922 -0.0459 1.0000 0.0028
-11.500 -0.9656 0.02915 0.02633 -0.0451 1.0000 0.0029
-11.250 -0.9550 0.02699 0.02396 -0.0442 1.0000 0.0029
-11.000 -0.9411 0.02513 0.02189 -0.0435 1.0000 0.0030
-10.750 -0.9236 0.02372 0.02031 -0.0428 1.0000 0.0031
-10.500 -0.9057 0.02227 0.01868 -0.0422 1.0000 0.0031
-10.250 -0.8794 0.02105 0.01730 -0.0430 0.9777 0.0032
-10.000 -0.8542 0.01992 0.01601 -0.0433 0.9597 0.0034
-9.750 -0.8332 0.01907 0.01500 -0.0425 0.9437 0.0035
-9.500 -0.8133 0.01814 0.01389 -0.0414 0.9306 0.0036
-9.250 -0.7918 0.01736 0.01296 -0.0406 0.9199 0.0038
-9.000 -0.7698 0.01658 0.01203 -0.0398 0.9106 0.0039
-8.750 -0.7470 0.01588 0.01117 -0.0390 0.9018 0.0040
-8.500 -0.7237 0.01513 0.01027 -0.0384 0.8940 0.0041
-8.000 -0.6750 0.01398 0.00888 -0.0373 0.8795 0.0044
-7.500 -0.6261 0.01264 0.00729 -0.0363 0.8659 0.0049
-7.250 -0.6005 0.01222 0.00679 -0.0359 0.8593 0.0053
-7.000 -0.5743 0.01187 0.00638 -0.0356 0.8532 0.0057
-6.750 -0.5480 0.01153 0.00597 -0.0353 0.8468 0.0061
-6.500 -0.5215 0.01123 0.00562 -0.0351 0.8411 0.0066
-6.250 -0.4946 0.01097 0.00531 -0.0349 0.8348 0.0071
-6.000 -0.4684 0.01059 0.00486 -0.0345 0.8291 0.0078
-5.750 -0.4413 0.01034 0.00460 -0.0344 0.8230 0.0086
-5.500 -0.4142 0.01013 0.00434 -0.0342 0.8168 0.0095
-5.250 -0.3869 0.00991 0.00407 -0.0340 0.8108 0.0104
-5.000 -0.3596 0.00973 0.00384 -0.0339 0.8042 0.0110
-4.750 -0.3324 0.00948 0.00353 -0.0337 0.7980 0.0117
-4.500 -0.3054 0.00918 0.00320 -0.0335 0.7912 0.0130
-4.250 -0.2780 0.00900 0.00298 -0.0333 0.7848 0.0142
-4.000 -0.2504 0.00881 0.00275 -0.0332 0.7777 0.0151
-3.750 -0.2229 0.00865 0.00253 -0.0331 0.7708 0.0159
-3.500 -0.1951 0.00850 0.00235 -0.0330 0.7629 0.0165
-3.250 -0.1675 0.00833 0.00213 -0.0328 0.7552 0.0171
-3.000 -0.1399 0.00815 0.00188 -0.0326 0.7462 0.0191
-2.750 -0.1122 0.00799 0.00170 -0.0325 0.7370 0.0214
-2.500 -0.0845 0.00788 0.00155 -0.0324 0.7271 0.0246
-2.000 -0.0300 0.00746 0.00126 -0.0321 0.7031 0.0766
-1.750 -0.0031 0.00726 0.00114 -0.0319 0.6867 0.1177
-1.500 0.0241 0.00712 0.00105 -0.0318 0.6690 0.1504
-1.250 0.0514 0.00700 0.00097 -0.0317 0.6530 0.1845
-1.000 0.0785 0.00684 0.00091 -0.0316 0.6368 0.2318
-0.750 0.1051 0.00665 0.00086 -0.0314 0.6201 0.2962
-0.500 0.1314 0.00641 0.00083 -0.0312 0.6030 0.3809
-0.250 0.1577 0.00620 0.00081 -0.0310 0.5852 0.4592
0.000 0.1847 0.00614 0.00080 -0.0308 0.5661 0.5040
0.250 0.2115 0.00607 0.00081 -0.0306 0.5475 0.5540
0.500 0.2380 0.00599 0.00083 -0.0304 0.5290 0.6106
0.750 0.2643 0.00593 0.00085 -0.0300 0.5092 0.6634
1.000 0.2903 0.00589 0.00089 -0.0296 0.4888 0.7144
1.250 0.3160 0.00584 0.00094 -0.0291 0.4681 0.7673
1.500 0.3408 0.00580 0.00100 -0.0284 0.4470 0.8254
1.750 0.3651 0.00575 0.00107 -0.0275 0.4243 0.8897
2.000 0.4016 0.00584 0.00118 -0.0293 0.3986 0.9494
2.250 0.4442 0.00605 0.00128 -0.0326 0.3686 0.9741
2.500 0.4790 0.00625 0.00137 -0.0342 0.3437 0.9855
2.750 0.5121 0.00647 0.00146 -0.0355 0.3198 0.9934
3.250 0.5797 0.00687 0.00167 -0.0383 0.2758 1.0000
3.500 0.6049 0.00706 0.00179 -0.0379 0.2588 1.0000
3.750 0.6302 0.00724 0.00192 -0.0374 0.2445 1.0000
4.000 0.6554 0.00744 0.00205 -0.0369 0.2286 1.0000
4.250 0.6806 0.00763 0.00218 -0.0364 0.2153 1.0000
4.500 0.7057 0.00784 0.00233 -0.0359 0.2004 1.0000
4.750 0.7310 0.00805 0.00250 -0.0355 0.1882 1.0000
5.000 0.7560 0.00827 0.00267 -0.0350 0.1744 1.0000
5.250 0.7810 0.00849 0.00284 -0.0345 0.1636 1.0000
5.500 0.8060 0.00872 0.00302 -0.0340 0.1525 1.0000
5.750 0.8307 0.00897 0.00323 -0.0335 0.1399 1.0000
6.000 0.8557 0.00920 0.00345 -0.0330 0.1298 1.0000
6.250 0.8806 0.00944 0.00366 -0.0325 0.1210 1.0000
6.500 0.9051 0.00973 0.00390 -0.0320 0.1101 1.0000
6.750 0.9294 0.01005 0.00417 -0.0315 0.0977 1.0000
7.000 0.9531 0.01042 0.00447 -0.0309 0.0824 1.0000
7.250 0.9764 0.01085 0.00482 -0.0303 0.0670 1.0000
7.500 1.0004 0.01119 0.00513 -0.0297 0.0585 1.0000
7.750 1.0239 0.01157 0.00548 -0.0291 0.0501 1.0000
8.000 1.0471 0.01199 0.00586 -0.0285 0.0411 1.0000
8.250 1.0697 0.01247 0.00627 -0.0278 0.0314 1.0000
8.500 1.0923 0.01294 0.00671 -0.0271 0.0238 1.0000
8.750 1.1142 0.01347 0.00722 -0.0263 0.0168 1.0000
9.000 1.1353 0.01406 0.00777 -0.0255 0.0104 1.0000
9.250 1.1563 0.01464 0.00835 -0.0246 0.0062 1.0000
9.500 1.1775 0.01520 0.00893 -0.0237 0.0043 1.0000
9.750 1.1989 0.01569 0.00946 -0.0229 0.0038 1.0000
10.000 1.2194 0.01625 0.01007 -0.0219 0.0033 1.0000
10.250 1.2392 0.01685 0.01073 -0.0209 0.0029 1.0000
10.500 1.2586 0.01745 0.01141 -0.0198 0.0027 1.0000
10.750 1.2777 0.01804 0.01206 -0.0187 0.0026 1.0000
11.000 1.2962 0.01864 0.01273 -0.0176 0.0025 1.0000
11.250 1.3135 0.01929 0.01344 -0.0163 0.0023 1.0000
11.500 1.3294 0.01998 0.01421 -0.0148 0.0022 1.0000
11.750 1.3435 0.02070 0.01500 -0.0131 0.0021 1.0000
12.000 1.3538 0.02144 0.01582 -0.0107 0.0020 1.0000
12.250 1.3623 0.02228 0.01673 -0.0083 0.0019 1.0000
12.500 1.3706 0.02319 0.01773 -0.0061 0.0017 1.0000
12.750 1.3789 0.02418 0.01879 -0.0041 0.0017 1.0000
13.000 1.3846 0.02541 0.02012 -0.0021 0.0017 1.0000
13.250 1.3857 0.02706 0.02190 0.0000 0.0016 1.0000
13.500 1.3902 0.02855 0.02349 0.0015 0.0015 1.0000
13.750 1.3864 0.03084 0.02592 0.0032 0.0014 1.0000
14.000 1.3854 0.03303 0.02823 0.0043 0.0014 1.0000
14.250 1.3842 0.03540 0.03072 0.0051 0.0014 1.0000
14.500 1.3813 0.03811 0.03355 0.0055 0.0014 1.0000
14.750 1.3807 0.04075 0.03630 0.0055 0.0014 1.0000
15.000 1.3774 0.04387 0.03953 0.0052 0.0014 1.0000
15.250 1.3724 0.04741 0.04319 0.0045 0.0014 1.0000
15.500 1.3642 0.05158 0.04749 0.0032 0.0014 1.0000
15.750 1.3540 0.05633 0.05238 0.0014 0.0014 1.0000
16.000 1.3381 0.06225 0.05845 -0.0012 0.0014 1.0000
16.250 1.3245 0.06817 0.06450 -0.0040 0.0014 1.0000
16.500 1.3077 0.07492 0.07139 -0.0074 0.0013 1.0000
16.750 1.2807 0.08381 0.08046 -0.0120 0.0014 1.0000
17.000 1.2645 0.09095 0.08771 -0.0157 0.0014 1.0000
17.250 1.2340 0.10109 0.09801 -0.0210 0.0014 1.0000
17.500 1.2137 0.10945 0.10649 -0.0254 0.0014 1.0000
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