SOMERS S102 AIRFOIL (BLUNT) (s102b-il) Xfoil prediction polar at RE=100,000 Ncrit=5
| Details | Polar file |
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Airfoil: SOMERS S102 AIRFOIL (BLUNT) (s102b-il) Reynolds number: 100,000 Max Cl/Cd: 43.8 at α=5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-s102b-il-100000-n5.txt Download as CSV file: xf-s102b-il-100000-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 = 0.100 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-13.750 -0.3046 0.13908 0.13415 -0.0373 1.0000 0.0504
-13.500 -0.3056 0.13662 0.13169 -0.0383 1.0000 0.0504
-12.500 -0.4515 0.12542 0.12012 -0.0362 1.0000 0.0256
-12.250 -0.4447 0.12258 0.11730 -0.0365 1.0000 0.0252
-12.000 -0.4418 0.11864 0.11340 -0.0379 1.0000 0.0246
-11.750 -0.4415 0.11394 0.10873 -0.0399 1.0000 0.0239
-11.250 -0.4662 0.09432 0.08917 -0.0512 1.0000 0.0208
-11.000 -0.4730 0.08837 0.08323 -0.0547 1.0000 0.0206
-10.750 -0.4852 0.08219 0.07703 -0.0584 1.0000 0.0203
-10.500 -0.5012 0.07643 0.07122 -0.0617 1.0000 0.0201
-10.250 -0.5190 0.07135 0.06608 -0.0640 1.0000 0.0199
-10.000 -0.5376 0.06705 0.06170 -0.0652 1.0000 0.0197
-9.750 -0.5576 0.06362 0.05821 -0.0648 1.0000 0.0195
-9.500 -0.5815 0.06133 0.05589 -0.0621 1.0000 0.0194
-9.250 -0.6087 0.05994 0.05450 -0.0576 1.0000 0.0193
-9.000 -0.6055 0.05509 0.04931 -0.0610 0.9883 0.0191
-8.750 -0.5949 0.05032 0.04411 -0.0640 0.9771 0.0188
-8.500 -0.5782 0.04587 0.03918 -0.0665 0.9681 0.0186
-8.250 -0.5590 0.04213 0.03498 -0.0681 0.9582 0.0185
-8.000 -0.5369 0.03890 0.03131 -0.0692 0.9490 0.0186
-7.750 -0.5105 0.03602 0.02800 -0.0704 0.9415 0.0188
-7.500 -0.4851 0.03364 0.02528 -0.0708 0.9327 0.0191
-7.250 -0.4559 0.03151 0.02282 -0.0714 0.9261 0.0198
-7.000 -0.4286 0.02979 0.02079 -0.0715 0.9180 0.0212
-6.750 -0.4008 0.02853 0.01951 -0.0721 0.9108 0.0227
-6.500 -0.3738 0.02727 0.01811 -0.0720 0.9031 0.0243
-6.250 -0.3469 0.02602 0.01670 -0.0716 0.8957 0.0255
-6.000 -0.3227 0.02488 0.01558 -0.0712 0.8883 0.0269
-5.750 -0.2994 0.02397 0.01463 -0.0707 0.8803 0.0292
-5.500 -0.2754 0.02311 0.01373 -0.0705 0.8738 0.0331
-5.250 -0.2526 0.02238 0.01292 -0.0701 0.8661 0.0381
-5.000 -0.2277 0.02158 0.01208 -0.0700 0.8608 0.0464
-4.750 -0.2062 0.02077 0.01135 -0.0696 0.8534 0.0607
-4.500 -0.1834 0.01958 0.01046 -0.0699 0.8474 0.1120
-4.250 -0.1697 0.01796 0.01101 -0.0693 0.8411 0.5542
-4.000 -0.1436 0.01918 0.01207 -0.0675 0.8351 0.6057
-3.750 -0.1210 0.02077 0.01362 -0.0636 0.8307 0.6382
-3.500 -0.0994 0.02207 0.01484 -0.0601 0.8263 0.6654
-3.250 -0.0775 0.02262 0.01534 -0.0573 0.8211 0.6732
-3.000 -0.0489 0.02234 0.01485 -0.0581 0.8169 0.6766
-2.750 -0.0180 0.02195 0.01423 -0.0597 0.8134 0.6803
-2.500 0.0099 0.02172 0.01384 -0.0604 0.8086 0.6826
-2.250 0.0368 0.02159 0.01360 -0.0606 0.8039 0.6842
-2.000 0.0651 0.02145 0.01334 -0.0610 0.8003 0.6859
-1.750 0.0946 0.02127 0.01304 -0.0617 0.7974 0.6874
-1.500 0.1225 0.02118 0.01285 -0.0623 0.7938 0.6894
-1.250 0.1501 0.02110 0.01270 -0.0630 0.7894 0.6914
-1.000 0.1794 0.02097 0.01247 -0.0640 0.7857 0.6930
-0.750 0.2099 0.02083 0.01223 -0.0651 0.7826 0.6951
-0.500 0.2414 0.02069 0.01199 -0.0665 0.7803 0.6972
-0.250 0.2677 0.02075 0.01204 -0.0669 0.7762 0.6984
0.000 0.2948 0.02079 0.01207 -0.0673 0.7722 0.6995
0.250 0.3231 0.02079 0.01205 -0.0678 0.7689 0.7006
0.500 0.3522 0.02079 0.01203 -0.0683 0.7662 0.7020
0.750 0.3820 0.02079 0.01201 -0.0690 0.7640 0.7037
1.000 0.4067 0.02101 0.01227 -0.0692 0.7591 0.7054
1.250 0.4343 0.02112 0.01240 -0.0698 0.7552 0.7068
1.500 0.4639 0.02113 0.01242 -0.0705 0.7517 0.7083
1.750 0.4937 0.02100 0.01227 -0.0709 0.7454 0.7099
2.000 0.5229 0.02070 0.01194 -0.0710 0.7345 0.7115
2.250 0.5514 0.02035 0.01156 -0.0708 0.7206 0.7134
2.500 0.5782 0.02000 0.01121 -0.0701 0.7061 0.7148
2.750 0.6049 0.01973 0.01094 -0.0695 0.6924 0.7163
3.000 0.6323 0.01951 0.01074 -0.0691 0.6800 0.7179
3.250 0.6599 0.01937 0.01063 -0.0690 0.6693 0.7195
3.500 0.6855 0.01934 0.01068 -0.0687 0.6574 0.7211
3.750 0.7119 0.01926 0.01068 -0.0685 0.6448 0.7229
4.000 0.7382 0.01918 0.01066 -0.0683 0.6307 0.7249
4.250 0.7639 0.01913 0.01068 -0.0680 0.6128 0.7269
4.500 0.7894 0.01905 0.01064 -0.0676 0.5897 0.7290
4.750 0.8109 0.01907 0.01075 -0.0665 0.5536 0.7309
5.000 0.8322 0.01900 0.01036 -0.0648 0.4693 0.7329
5.250 0.8427 0.01986 0.01051 -0.0618 0.3696 0.7351
5.500 0.8538 0.02093 0.01121 -0.0596 0.3079 0.7376
5.750 0.8683 0.02183 0.01188 -0.0580 0.2696 0.7401
6.000 0.8848 0.02262 0.01252 -0.0568 0.2448 0.7426
6.250 0.9029 0.02333 0.01316 -0.0558 0.2272 0.7452
6.500 0.9201 0.02398 0.01378 -0.0545 0.2148 0.7473
6.750 0.9383 0.02461 0.01441 -0.0534 0.2050 0.7498
7.000 0.9572 0.02524 0.01505 -0.0524 0.1970 0.7525
7.250 0.9756 0.02589 0.01571 -0.0513 0.1897 0.7556
7.500 0.9945 0.02656 0.01638 -0.0504 0.1834 0.7591
7.750 1.0138 0.02718 0.01707 -0.0494 0.1773 0.7624
8.000 1.0321 0.02790 0.01780 -0.0484 0.1727 0.7659
8.250 1.0531 0.02859 0.01857 -0.0477 0.1682 0.7699
8.500 1.0745 0.02928 0.01936 -0.0472 0.1633 0.7744
8.750 1.0946 0.03002 0.02015 -0.0465 0.1589 0.7785
9.000 1.1158 0.03082 0.02099 -0.0459 0.1551 0.7828
9.250 1.1373 0.03156 0.02191 -0.0454 0.1510 0.7878
9.500 1.1580 0.03234 0.02281 -0.0448 0.1469 0.7933
9.750 1.1777 0.03316 0.02368 -0.0441 0.1432 0.7988
10.000 1.1987 0.03405 0.02471 -0.0436 0.1396 0.8056
10.250 1.2168 0.03490 0.02580 -0.0427 0.1357 0.8129
10.500 1.2344 0.03577 0.02682 -0.0418 0.1319 0.8221
10.750 1.2513 0.03663 0.02776 -0.0407 0.1285 0.8327
11.000 1.2676 0.03762 0.02896 -0.0396 0.1252 0.8462
11.250 1.2790 0.03855 0.03022 -0.0378 0.1214 0.8655
11.500 1.2875 0.03933 0.03123 -0.0355 0.1180 0.9048
11.750 1.2989 0.04022 0.03219 -0.0342 0.1149 1.0000
12.000 1.3129 0.04157 0.03366 -0.0336 0.1114 1.0000
12.250 1.3222 0.04306 0.03542 -0.0325 0.1074 1.0000
12.500 1.3316 0.04444 0.03695 -0.0316 0.1038 1.0000
12.750 1.3414 0.04573 0.03825 -0.0308 0.1007 1.0000
13.000 1.3472 0.04754 0.04031 -0.0297 0.0973 1.0000
13.250 1.3507 0.04946 0.04249 -0.0287 0.0935 1.0000
13.500 1.3547 0.05118 0.04433 -0.0278 0.0902 1.0000
13.750 1.3598 0.05281 0.04596 -0.0272 0.0875 1.0000
14.000 1.3579 0.05551 0.04902 -0.0264 0.0840 1.0000
14.250 1.3568 0.05800 0.05172 -0.0258 0.0805 1.0000
14.500 1.3568 0.06027 0.05411 -0.0255 0.0778 1.0000
14.750 1.3552 0.06289 0.05683 -0.0253 0.0752 1.0000
15.000 1.3476 0.06656 0.06082 -0.0252 0.0720 1.0000
15.250 1.3414 0.06999 0.06445 -0.0254 0.0692 1.0000
15.500 1.3366 0.07325 0.06779 -0.0259 0.0669 1.0000
15.750 1.3287 0.07720 0.07186 -0.0267 0.0647 1.0000
16.000 1.3131 0.08268 0.07765 -0.0281 0.0625 1.0000
16.250 1.2974 0.08838 0.08358 -0.0300 0.0605 1.0000
16.500 1.2822 0.09429 0.08966 -0.0325 0.0589 1.0000
16.750 1.2683 0.10026 0.09574 -0.0353 0.0574 1.0000
17.000 1.2567 0.10602 0.10155 -0.0382 0.0560 1.0000
17.250 1.2246 0.11644 0.11223 -0.0440 0.0556 1.0000
17.500 1.1827 0.12984 0.12585 -0.0520 0.0557 1.0000
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