WORTMANN FX 05-188 AIRFOIL (fx05188-il) Xfoil prediction polar at RE=100,000 Ncrit=9
| Details | Polar file |
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Airfoil: WORTMANN FX 05-188 AIRFOIL (fx05188-il) Reynolds number: 100,000 Max Cl/Cd: 27.8 at α=11.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx05188-il-100000.txt Download as CSV file: xf-fx05188-il-100000.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 05-188 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.100 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-11.500 -0.3603 0.12098 0.11638 -0.0638 0.9812 0.1721
-11.250 -0.3331 0.11807 0.11342 -0.0646 0.9780 0.1764
-11.000 -0.3515 0.11244 0.10785 -0.0707 0.9744 0.1881
-10.750 -0.3201 0.10930 0.10464 -0.0717 0.9721 0.1916
-10.500 -0.3156 0.10586 0.10121 -0.0733 0.9670 0.1972
-10.250 -0.3190 0.10106 0.09644 -0.0769 0.9632 0.2069
-10.000 -0.5987 0.06780 0.06250 -0.0934 0.9467 0.1027
-9.750 -0.6574 0.06479 0.05902 -0.0861 0.9373 0.0910
-9.500 -0.6998 0.06062 0.05389 -0.0814 0.9309 0.0813
-9.250 -0.6912 0.05802 0.05124 -0.0794 0.9269 0.0794
-9.000 -0.6926 0.05551 0.04861 -0.0765 0.9224 0.0780
-8.750 -0.6847 0.05254 0.04537 -0.0753 0.9185 0.0757
-8.500 -0.6703 0.04911 0.04140 -0.0749 0.9152 0.0725
-8.250 -0.6663 0.04716 0.03884 -0.0722 0.9112 0.0703
-8.000 -0.6640 0.04620 0.03760 -0.0687 0.9068 0.0696
-7.750 -0.6457 0.04484 0.03596 -0.0677 0.9028 0.0692
-7.500 -0.6161 0.04295 0.03384 -0.0685 0.8996 0.0693
-7.250 -0.5778 0.04090 0.03172 -0.0705 0.8973 0.0705
-7.000 -0.5688 0.04022 0.03102 -0.0679 0.8933 0.0716
-6.750 -0.5589 0.03962 0.03039 -0.0654 0.8889 0.0733
-6.500 -0.5337 0.03878 0.02951 -0.0651 0.8850 0.0752
-6.250 -0.4987 0.03792 0.02859 -0.0660 0.8818 0.0770
-6.000 -0.4572 0.03716 0.02778 -0.0679 0.8794 0.0797
-5.750 -0.4691 0.03724 0.02782 -0.0620 0.8741 0.0804
-5.500 -0.4581 0.03662 0.02735 -0.0595 0.8696 0.0829
-5.250 -0.4360 0.03603 0.02686 -0.0592 0.8656 0.0878
-5.000 -0.4047 0.03528 0.02613 -0.0605 0.8624 0.0972
-4.750 -0.4109 0.03517 0.02604 -0.0562 0.8576 0.1025
-4.500 -0.4031 0.03463 0.02557 -0.0542 0.8532 0.1154
-4.250 -0.3953 0.03118 0.02488 -0.0539 0.8495 0.5217
-4.000 -0.3712 0.03398 0.02786 -0.0490 0.8455 0.6136
-3.750 -0.3656 0.03528 0.02903 -0.0452 0.8408 0.6375
-3.500 -0.3622 0.03696 0.03067 -0.0400 0.8367 0.6542
-3.250 -0.3524 0.03946 0.03318 -0.0334 0.8321 0.6725
-3.000 -0.3320 0.04317 0.03689 -0.0257 0.8284 0.6964
-2.750 -0.3354 0.04507 0.03879 -0.0180 0.8244 0.7123
-2.500 -0.3365 0.04648 0.04020 -0.0115 0.8208 0.7275
-2.250 -0.3221 0.04758 0.04123 -0.0076 0.8165 0.7427
-2.000 -0.2927 0.04795 0.04145 -0.0077 0.8125 0.7551
-1.750 -0.2767 0.04817 0.04156 -0.0064 0.8087 0.7627
-1.500 -0.2854 0.04796 0.04131 -0.0025 0.8049 0.7713
-1.250 -0.2739 0.04802 0.04130 -0.0007 0.8008 0.7783
-1.000 -0.2484 0.04790 0.04105 -0.0017 0.7967 0.7862
-0.750 -0.3217 0.05036 0.04374 0.0078 0.8616 0.7939
-0.500 -0.3255 0.04914 0.04247 0.0110 0.8528 0.8017
-0.250 -0.2773 0.05051 0.04368 0.0076 0.8441 0.8073
0.000 -0.2782 0.04953 0.04264 0.0097 0.8357 0.8155
0.250 -0.2373 0.05049 0.04348 0.0079 0.8264 0.8204
0.500 -0.2390 0.04998 0.04295 0.0108 0.8208 0.8276
0.750 -0.1300 0.04821 0.04084 0.0032 0.7589 0.8332
1.000 -0.1263 0.04841 0.04102 0.0059 0.7542 0.8399
1.250 -0.0911 0.04851 0.04102 0.0036 0.7485 0.8469
1.500 -0.0830 0.04860 0.04110 0.0060 0.7414 0.8523
1.750 -0.0673 0.04885 0.04131 0.0063 0.7360 0.8582
2.000 -0.0242 0.04896 0.04134 0.0035 0.7310 0.8634
2.250 -0.0283 0.04923 0.04163 0.0068 0.7231 0.8687
2.500 0.0018 0.04939 0.04174 0.0055 0.7169 0.8736
2.750 0.0293 0.04972 0.04202 0.0043 0.7104 0.8785
3.000 0.0321 0.05011 0.04243 0.0066 0.7039 0.8836
3.250 0.0695 0.05024 0.04252 0.0048 0.6985 0.8884
3.500 0.0824 0.05087 0.04314 0.0047 0.6898 0.8929
3.750 0.1008 0.05112 0.04339 0.0054 0.6840 0.8974
4.000 0.1422 0.05122 0.04347 0.0035 0.6802 0.9021
4.250 0.1404 0.05214 0.04442 0.0049 0.6701 0.9070
4.500 0.1736 0.05225 0.04453 0.0038 0.6651 0.9108
4.750 0.1836 0.05303 0.04533 0.0046 0.6578 0.9153
5.000 0.2044 0.05360 0.04591 0.0042 0.6511 0.9201
5.250 0.2464 0.05356 0.04589 0.0023 0.6474 0.9241
5.500 0.2410 0.05482 0.04719 0.0041 0.6374 0.9286
5.750 0.2794 0.05491 0.04731 0.0024 0.6327 0.9327
6.000 0.2837 0.05614 0.04858 0.0031 0.6237 0.9371
6.250 0.3146 0.05636 0.04884 0.0022 0.6184 0.9416
6.500 0.3288 0.05738 0.04991 0.0021 0.6105 0.9461
6.750 0.3529 0.05801 0.05060 0.0013 0.6040 0.9505
7.000 0.3999 0.05771 0.05036 -0.0009 0.6005 0.9550
7.250 0.3973 0.05956 0.05228 -0.0003 0.5890 0.9601
7.500 0.4448 0.05928 0.05209 -0.0027 0.5852 0.9647
7.750 0.4473 0.06126 0.05415 -0.0029 0.5736 0.9700
8.000 0.4967 0.06089 0.05389 -0.0056 0.5694 0.9752
8.250 0.5043 0.06286 0.05595 -0.0065 0.5574 0.9812
8.500 0.5585 0.06189 0.05510 -0.0094 0.5530 0.9898
8.750 0.5631 0.06362 0.05691 -0.0095 0.5401 1.0000
9.000 0.6206 0.06189 0.05530 -0.0117 0.5361 1.0000
9.250 0.6300 0.06340 0.05690 -0.0121 0.5226 1.0000
9.500 0.6761 0.06200 0.05563 -0.0135 0.5153 1.0000
9.750 0.7164 0.06063 0.05438 -0.0145 0.5053 1.0000
10.000 0.7927 0.05574 0.04968 -0.0163 0.5029 1.0000
10.250 0.8108 0.05620 0.05027 -0.0166 0.4891 1.0000
10.500 0.8830 0.05115 0.04543 -0.0180 0.4874 1.0000
10.750 1.0166 0.03858 0.03309 -0.0205 0.4855 1.0000
11.000 1.0143 0.04040 0.03502 -0.0195 0.4634 1.0000
11.250 1.0565 0.03800 0.03268 -0.0199 0.4388 1.0000
11.500 1.0716 0.03856 0.03328 -0.0197 0.4091 1.0000
11.750 1.0860 0.03918 0.03378 -0.0192 0.3678 1.0000
12.000 1.0838 0.04140 0.03572 -0.0181 0.3103 1.0000
12.250 1.0713 0.04472 0.03850 -0.0168 0.2454 1.0000
12.500 1.0557 0.04878 0.04207 -0.0158 0.1969 1.0000
12.750 1.0463 0.05256 0.04549 -0.0154 0.1621 1.0000
13.000 1.0427 0.05591 0.04852 -0.0151 0.1366 1.0000
13.250 1.0472 0.05857 0.05100 -0.0149 0.1163 1.0000
13.500 1.0609 0.06028 0.05255 -0.0147 0.1031 1.0000
13.750 1.0853 0.06104 0.05309 -0.0145 0.0936 1.0000
14.000 1.1084 0.06222 0.05426 -0.0147 0.0865 1.0000
14.250 1.1448 0.06260 0.05455 -0.0149 0.0807 1.0000
14.500 1.1737 0.06384 0.05594 -0.0153 0.0770 1.0000
14.750 1.2091 0.06491 0.05697 -0.0160 0.0735 1.0000
15.000 1.2504 0.06658 0.05868 -0.0170 0.0701 1.0000
15.250 1.2597 0.06933 0.06175 -0.0173 0.0685 1.0000
15.500 1.2709 0.07228 0.06497 -0.0177 0.0671 1.0000
15.750 1.2797 0.07551 0.06848 -0.0180 0.0661 1.0000
16.000 1.2835 0.07911 0.07235 -0.0184 0.0653 1.0000
16.250 1.2832 0.08298 0.07648 -0.0188 0.0647 1.0000
16.500 1.2798 0.08708 0.08083 -0.0194 0.0641 1.0000
16.750 1.2755 0.09129 0.08526 -0.0202 0.0634 1.0000
17.000 1.2730 0.09547 0.08962 -0.0212 0.0627 1.0000
17.250 1.2597 0.10063 0.09503 -0.0225 0.0624 1.0000
17.500 1.2101 0.10964 0.10454 -0.0257 0.0635 1.0000
17.750 1.1548 0.12110 0.11646 -0.0311 0.0652 1.0000
18.000 1.0998 0.13449 0.13020 -0.0387 0.0671 1.0000
18.250 1.0492 0.14927 0.14517 -0.0480 0.0692 1.0000
18.500 1.0215 0.16126 0.15724 -0.0553 0.0706 1.0000
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