S1016 (s1016-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: S1016 (s1016-il) Reynolds number: 500,000 Max Cl/Cd: 40.14 at α=10.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-s1016-il-500000.txt Download as CSV file: xf-s1016-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: S1016
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.1075 0.08686 0.08242 -0.0544 1.0000 0.0306
-19.500 -1.1158 0.08213 0.07764 -0.0568 1.0000 0.0313
-19.250 -1.1227 0.07784 0.07330 -0.0587 0.9690 0.0319
-19.000 -1.1193 0.07331 0.06864 -0.0629 0.9533 0.0326
-18.750 -1.1158 0.06907 0.06426 -0.0665 0.9433 0.0334
-18.500 -1.1126 0.06537 0.06040 -0.0691 0.9347 0.0344
-18.250 -1.1101 0.06221 0.05708 -0.0707 0.9275 0.0351
-18.000 -1.1152 0.05861 0.05339 -0.0718 0.9222 0.0360
-17.750 -1.1175 0.05544 0.05014 -0.0726 0.9180 0.0369
-17.500 -1.1163 0.05277 0.04738 -0.0731 0.9142 0.0378
-17.250 -1.1130 0.05045 0.04496 -0.0734 0.9110 0.0389
-17.000 -1.1081 0.04833 0.04272 -0.0736 0.9082 0.0401
-16.750 -1.1029 0.04627 0.04055 -0.0736 0.9058 0.0411
-16.500 -1.1043 0.04372 0.03796 -0.0734 0.9034 0.0423
-16.250 -1.1002 0.04177 0.03596 -0.0731 0.9010 0.0436
-16.000 -1.0930 0.04015 0.03427 -0.0727 0.8989 0.0450
-15.750 -1.0839 0.03872 0.03274 -0.0723 0.8971 0.0464
-15.500 -1.0770 0.03717 0.03111 -0.0717 0.8953 0.0480
-15.250 -1.0725 0.03551 0.02942 -0.0709 0.8936 0.0497
-15.000 -1.0629 0.03427 0.02813 -0.0702 0.8920 0.0514
-14.750 -1.0510 0.03319 0.02698 -0.0696 0.8909 0.0532
-14.500 -1.0392 0.03212 0.02583 -0.0689 0.8897 0.0549
-14.250 -1.0327 0.03073 0.02444 -0.0678 0.8884 0.0570
-14.000 -1.0207 0.02977 0.02345 -0.0670 0.8871 0.0591
-13.750 -1.0067 0.02894 0.02257 -0.0663 0.8859 0.0613
-13.500 -0.9936 0.02807 0.02164 -0.0654 0.8847 0.0635
-13.250 -0.9839 0.02703 0.02060 -0.0642 0.8835 0.0661
-13.000 -0.9693 0.02630 0.01985 -0.0634 0.8825 0.0688
-12.750 -0.9528 0.02570 0.01918 -0.0626 0.8814 0.0711
-12.500 -0.9414 0.02482 0.01829 -0.0613 0.8804 0.0742
-12.250 -0.9272 0.02413 0.01759 -0.0603 0.8794 0.0773
-12.000 -0.9099 0.02362 0.01704 -0.0595 0.8784 0.0805
-11.750 -0.8958 0.02297 0.01636 -0.0583 0.8772 0.0841
-11.500 -0.8813 0.02237 0.01577 -0.0572 0.8761 0.0880
-11.250 -0.8626 0.02194 0.01530 -0.0565 0.8754 0.0919
-11.000 -0.8468 0.02133 0.01470 -0.0555 0.8747 0.0963
-10.750 -0.8300 0.02079 0.01419 -0.0546 0.8740 0.1009
-10.500 -0.8100 0.02043 0.01378 -0.0540 0.8733 0.1052
-10.250 -0.7949 0.01982 0.01321 -0.0529 0.8725 0.1107
-10.000 -0.7759 0.01941 0.01281 -0.0521 0.8717 0.1161
-9.750 -0.7575 0.01899 0.01238 -0.0513 0.8709 0.1216
-9.500 -0.7399 0.01854 0.01197 -0.0503 0.8701 0.1282
-9.250 -0.7200 0.01821 0.01162 -0.0496 0.8693 0.1342
-9.000 -0.7028 0.01776 0.01122 -0.0485 0.8683 0.1416
-8.750 -0.6827 0.01745 0.01090 -0.0478 0.8672 0.1488
-8.500 -0.6654 0.01703 0.01054 -0.0467 0.8663 0.1574
-8.250 -0.6459 0.01672 0.01024 -0.0458 0.8655 0.1659
-8.000 -0.6273 0.01637 0.00994 -0.0448 0.8647 0.1756
-7.750 -0.6090 0.01603 0.00965 -0.0438 0.8639 0.1865
-7.500 -0.5901 0.01573 0.00938 -0.0428 0.8631 0.1983
-7.250 -0.5717 0.01544 0.00913 -0.0417 0.8621 0.2112
-7.000 -0.5549 0.01513 0.00888 -0.0402 0.8610 0.2263
-6.750 -0.5380 0.01485 0.00868 -0.0388 0.8601 0.2429
-6.500 -0.5213 0.01460 0.00852 -0.0374 0.8591 0.2617
-6.250 -0.5045 0.01424 0.00826 -0.0361 0.8582 0.2824
-6.000 -0.4890 0.01387 0.00801 -0.0346 0.8567 0.3060
-5.500 -0.4629 0.01317 0.00758 -0.0306 0.8537 0.3608
-5.250 -0.4546 0.01286 0.00740 -0.0275 0.8515 0.3904
-5.000 -0.4502 0.01264 0.00731 -0.0236 0.8495 0.4216
-4.750 -0.4494 0.01242 0.00723 -0.0187 0.8472 0.4553
-4.500 -0.4445 0.01215 0.00713 -0.0145 0.8454 0.4945
-4.250 -0.4380 0.01189 0.00706 -0.0105 0.8436 0.5397
-4.000 -0.4300 0.01169 0.00711 -0.0071 0.8413 0.5907
-3.750 -0.4178 0.01156 0.00727 -0.0044 0.8378 0.6433
-3.500 -0.3974 0.01170 0.00766 -0.0028 0.8352 0.6890
-3.250 -0.3717 0.01197 0.00799 -0.0022 0.8332 0.7162
-3.000 -0.3458 0.01215 0.00816 -0.0017 0.8314 0.7323
-2.750 -0.3199 0.01228 0.00823 -0.0011 0.8298 0.7446
-2.500 -0.2907 0.01248 0.00841 -0.0010 0.8284 0.7527
-2.250 -0.2638 0.01263 0.00851 -0.0006 0.8269 0.7603
-2.000 -0.2354 0.01300 0.00890 -0.0005 0.8243 0.7650
-1.750 -0.2135 0.01328 0.00918 0.0004 0.8190 0.7715
-1.500 -0.1854 0.01339 0.00927 0.0006 0.8161 0.7766
-1.250 -0.1519 0.01352 0.00941 0.0001 0.8141 0.7797
-1.000 -0.1185 0.01359 0.00946 -0.0003 0.8121 0.7835
-0.750 -0.0887 0.01352 0.00935 -0.0002 0.8101 0.7886
-0.500 -0.0633 0.01359 0.00941 0.0004 0.8061 0.7929
-0.250 -0.0334 0.01372 0.00958 0.0004 0.8011 0.7952
0.000 0.0000 0.01372 0.00959 0.0000 0.7978 0.7978
0.250 0.0335 0.01371 0.00957 -0.0004 0.7952 0.8011
0.500 0.0634 0.01358 0.00940 -0.0004 0.7929 0.8061
0.750 0.0888 0.01352 0.00935 0.0002 0.7887 0.8101
1.000 0.1185 0.01357 0.00945 0.0003 0.7834 0.8121
1.250 0.1518 0.01353 0.00942 -0.0001 0.7798 0.8141
1.500 0.1853 0.01339 0.00927 -0.0006 0.7767 0.8161
1.750 0.2135 0.01328 0.00918 -0.0004 0.7716 0.8191
2.000 0.2354 0.01300 0.00890 0.0005 0.7649 0.8244
2.250 0.2638 0.01262 0.00850 0.0006 0.7602 0.8269
2.500 0.2907 0.01248 0.00841 0.0011 0.7527 0.8284
2.750 0.3199 0.01228 0.00823 0.0011 0.7447 0.8298
3.000 0.3458 0.01216 0.00816 0.0017 0.7325 0.8314
3.250 0.3717 0.01197 0.00799 0.0022 0.7159 0.8332
3.500 0.3974 0.01170 0.00766 0.0028 0.6891 0.8352
3.750 0.4178 0.01156 0.00727 0.0044 0.6433 0.8378
4.000 0.4300 0.01169 0.00711 0.0071 0.5909 0.8413
4.250 0.4381 0.01189 0.00706 0.0105 0.5399 0.8436
4.500 0.4446 0.01215 0.00713 0.0145 0.4946 0.8454
5.000 0.4505 0.01263 0.00731 0.0235 0.4217 0.8495
5.250 0.4545 0.01286 0.00740 0.0276 0.3900 0.8515
5.500 0.4631 0.01317 0.00758 0.0305 0.3609 0.8537
5.750 0.4742 0.01354 0.00780 0.0329 0.3322 0.8554
6.000 0.4892 0.01386 0.00801 0.0346 0.3061 0.8567
6.250 0.5046 0.01424 0.00826 0.0361 0.2821 0.8582
6.500 0.5215 0.01460 0.00851 0.0374 0.2610 0.8591
6.750 0.5382 0.01484 0.00868 0.0388 0.2430 0.8601
7.000 0.5551 0.01512 0.00888 0.0402 0.2262 0.8610
7.250 0.5720 0.01544 0.00913 0.0416 0.2114 0.8621
7.500 0.5903 0.01573 0.00938 0.0428 0.1982 0.8631
7.750 0.6093 0.01603 0.00964 0.0437 0.1865 0.8639
8.000 0.6277 0.01637 0.00993 0.0448 0.1759 0.8647
8.250 0.6462 0.01672 0.01023 0.0458 0.1657 0.8655
8.500 0.6658 0.01703 0.01053 0.0466 0.1574 0.8663
8.750 0.6830 0.01745 0.01090 0.0477 0.1486 0.8672
9.000 0.7031 0.01775 0.01121 0.0485 0.1416 0.8683
9.250 0.7203 0.01821 0.01161 0.0496 0.1341 0.8693
9.500 0.7404 0.01853 0.01196 0.0502 0.1282 0.8701
9.750 0.7580 0.01898 0.01237 0.0512 0.1215 0.8709
10.000 0.7765 0.01940 0.01279 0.0520 0.1159 0.8717
10.250 0.7952 0.01981 0.01321 0.0528 0.1106 0.8725
10.500 0.8107 0.02041 0.01376 0.0539 0.1051 0.8733
10.750 0.8307 0.02077 0.01417 0.0545 0.1009 0.8740
11.000 0.8472 0.02132 0.01469 0.0555 0.0961 0.8747
11.250 0.8633 0.02192 0.01529 0.0564 0.0918 0.8754
11.500 0.8819 0.02236 0.01576 0.0571 0.0878 0.8761
11.750 0.8961 0.02298 0.01636 0.0583 0.0838 0.8772
12.000 0.9107 0.02360 0.01701 0.0594 0.0805 0.8785
12.250 0.9278 0.02412 0.01758 0.0602 0.0773 0.8795
12.500 0.9421 0.02481 0.01827 0.0612 0.0741 0.8804
12.750 0.9536 0.02568 0.01916 0.0625 0.0711 0.8815
13.000 0.9702 0.02628 0.01982 0.0632 0.0686 0.8825
13.250 0.9847 0.02701 0.02058 0.0641 0.0661 0.8836
13.500 0.9946 0.02803 0.02160 0.0653 0.0635 0.8848
13.750 1.0070 0.02895 0.02257 0.0662 0.0614 0.8860
14.000 1.0218 0.02972 0.02340 0.0669 0.0590 0.8872
14.250 1.0336 0.03071 0.02442 0.0677 0.0571 0.8884
14.500 1.0398 0.03211 0.02582 0.0689 0.0547 0.8897
14.750 1.0519 0.03316 0.02695 0.0695 0.0531 0.8909
15.000 1.0643 0.03421 0.02806 0.0701 0.0512 0.8921
15.250 1.0737 0.03544 0.02935 0.0707 0.0496 0.8937
15.500 1.0785 0.03708 0.03101 0.0716 0.0480 0.8954
15.750 1.0849 0.03867 0.03268 0.0722 0.0465 0.8972
16.000 1.0946 0.04004 0.03416 0.0726 0.0450 0.8991
16.250 1.1016 0.04168 0.03587 0.0730 0.0436 0.9012
16.500 1.1061 0.04360 0.03784 0.0733 0.0424 0.9036
16.750 1.1043 0.04617 0.04044 0.0735 0.0410 0.9061
17.000 1.1103 0.04817 0.04255 0.0735 0.0400 0.9084
17.250 1.1146 0.05033 0.04484 0.0733 0.0389 0.9113
17.500 1.1182 0.05262 0.04723 0.0730 0.0377 0.9146
17.750 1.1193 0.05530 0.05000 0.0725 0.0370 0.9185
18.000 1.1170 0.05847 0.05324 0.0717 0.0359 0.9229
18.250 1.1125 0.06204 0.05691 0.0706 0.0350 0.9285
18.500 1.1152 0.06525 0.06028 0.0689 0.0344 0.9359
18.750 1.1195 0.06892 0.06411 0.0661 0.0335 0.9449
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