WORTMANN FX 66-17A-175 AIRFOIL (fx66a175-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
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Airfoil: WORTMANN FX 66-17A-175 AIRFOIL (fx66a175-il) Reynolds number: 1,000,000 Max Cl/Cd: 124.1 at α=7.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx66a175-il-1000000-n5.txt Download as CSV file: xf-fx66a175-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 66-17A-175 AIRFOIL
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
------ -------- --------- --------- -------- -------- --------
-15.250 -0.6103 0.06439 0.06064 -0.0942 0.6533 0.0025
-15.000 -0.6241 0.05888 0.05500 -0.0974 0.6459 0.0026
-14.750 -0.6310 0.05471 0.05072 -0.0996 0.6383 0.0026
-14.500 -0.6166 0.05350 0.04949 -0.1003 0.6284 0.0028
-14.250 -0.6431 0.04766 0.04344 -0.1030 0.6227 0.0027
-14.000 -0.6406 0.04531 0.04103 -0.1039 0.6165 0.0028
-13.750 -0.6605 0.04086 0.03638 -0.1053 0.6109 0.0027
-13.500 -0.6550 0.03903 0.03448 -0.1058 0.6019 0.0028
-13.250 -0.6517 0.03703 0.03240 -0.1063 0.5952 0.0029
-13.000 -0.6525 0.03469 0.02995 -0.1067 0.5897 0.0029
-12.750 -0.6507 0.03263 0.02778 -0.1070 0.5828 0.0030
-12.500 -0.6511 0.03040 0.02544 -0.1071 0.5777 0.0031
-12.250 -0.6448 0.02878 0.02373 -0.1072 0.5723 0.0031
-12.000 -0.6450 0.02664 0.02145 -0.1072 0.5681 0.0032
-11.750 -0.6381 0.02511 0.01984 -0.1072 0.5639 0.0033
-11.500 -0.6384 0.02337 0.01799 -0.1067 0.5595 0.0033
-11.250 -0.6329 0.02254 0.01706 -0.1049 0.5552 0.0034
-11.000 -0.6233 0.02148 0.01587 -0.1036 0.5510 0.0034
-10.750 -0.6079 0.02071 0.01501 -0.1027 0.5467 0.0035
-10.500 -0.5927 0.01987 0.01405 -0.1018 0.5421 0.0036
-10.250 -0.5748 0.01916 0.01324 -0.1010 0.5385 0.0036
-10.000 -0.5551 0.01853 0.01253 -0.1004 0.5346 0.0037
-9.750 -0.5352 0.01789 0.01179 -0.0998 0.5307 0.0038
-9.500 -0.5163 0.01712 0.01091 -0.0991 0.5269 0.0039
-9.250 -0.4960 0.01642 0.01012 -0.0984 0.5240 0.0041
-9.000 -0.4734 0.01590 0.00955 -0.0980 0.5209 0.0043
-8.750 -0.4501 0.01545 0.00903 -0.0977 0.5177 0.0045
-8.500 -0.4257 0.01511 0.00863 -0.0974 0.5146 0.0047
-8.000 -0.3770 0.01432 0.00773 -0.0969 0.5092 0.0052
-7.750 -0.3520 0.01397 0.00732 -0.0966 0.5065 0.0054
-7.500 -0.3268 0.01363 0.00692 -0.0964 0.5035 0.0057
-7.250 -0.3010 0.01336 0.00659 -0.0963 0.5005 0.0059
-7.000 -0.2760 0.01299 0.00614 -0.0960 0.4976 0.0063
-6.750 -0.2509 0.01258 0.00569 -0.0958 0.4953 0.0068
-6.500 -0.2247 0.01227 0.00534 -0.0957 0.4930 0.0072
-6.250 -0.1983 0.01200 0.00503 -0.0956 0.4905 0.0075
-6.000 -0.1718 0.01175 0.00472 -0.0955 0.4879 0.0080
-5.750 -0.1450 0.01154 0.00446 -0.0955 0.4854 0.0086
-5.500 -0.1180 0.01136 0.00423 -0.0955 0.4828 0.0090
-5.250 -0.0914 0.01107 0.00389 -0.0954 0.4809 0.0102
-5.000 -0.0642 0.01086 0.00365 -0.0954 0.4788 0.0112
-4.750 -0.0367 0.01068 0.00344 -0.0954 0.4764 0.0125
-4.500 -0.0093 0.01051 0.00324 -0.0954 0.4740 0.0148
-4.250 0.0180 0.01033 0.00305 -0.0954 0.4717 0.0200
-4.000 0.0452 0.01014 0.00287 -0.0954 0.4694 0.0317
-3.750 0.0721 0.00988 0.00269 -0.0955 0.4674 0.0559
-3.500 0.0990 0.00958 0.00250 -0.0955 0.4656 0.0940
-3.250 0.1256 0.00922 0.00231 -0.0956 0.4637 0.1484
-3.000 0.1508 0.00864 0.00204 -0.0955 0.4617 0.2507
-2.750 0.1756 0.00800 0.00182 -0.0955 0.4597 0.3786
-2.500 0.2035 0.00794 0.00184 -0.0956 0.4578 0.4198
-2.250 0.2320 0.00797 0.00186 -0.0957 0.4557 0.4368
-2.000 0.2605 0.00803 0.00188 -0.0958 0.4538 0.4494
-1.750 0.2893 0.00806 0.00190 -0.0960 0.4524 0.4569
-1.500 0.3181 0.00810 0.00191 -0.0962 0.4509 0.4626
-1.250 0.3467 0.00812 0.00191 -0.0964 0.4492 0.4657
-1.000 0.3753 0.00815 0.00192 -0.0966 0.4475 0.4684
-0.750 0.4038 0.00819 0.00192 -0.0968 0.4455 0.4706
-0.500 0.4322 0.00823 0.00192 -0.0969 0.4434 0.4720
-0.250 0.4604 0.00828 0.00192 -0.0971 0.4409 0.4731
0.000 0.4888 0.00833 0.00194 -0.0973 0.4391 0.4741
0.250 0.5173 0.00834 0.00194 -0.0975 0.4376 0.4752
0.500 0.5458 0.00836 0.00196 -0.0977 0.4361 0.4764
0.750 0.5741 0.00838 0.00199 -0.0978 0.4344 0.4776
1.000 0.6024 0.00842 0.00202 -0.0980 0.4325 0.4789
1.250 0.6306 0.00846 0.00205 -0.0982 0.4306 0.4801
1.500 0.6586 0.00851 0.00209 -0.0983 0.4286 0.4813
1.750 0.6864 0.00858 0.00215 -0.0984 0.4267 0.4826
2.000 0.7143 0.00864 0.00220 -0.0986 0.4251 0.4839
2.250 0.7427 0.00868 0.00225 -0.0988 0.4239 0.4853
2.500 0.7709 0.00872 0.00231 -0.0990 0.4226 0.4867
2.750 0.7990 0.00877 0.00237 -0.0991 0.4211 0.4880
3.250 0.8548 0.00887 0.00251 -0.0994 0.4179 0.4905
3.500 0.8824 0.00893 0.00259 -0.0996 0.4164 0.4919
3.750 0.9100 0.00900 0.00267 -0.0997 0.4148 0.4934
4.000 0.9374 0.00907 0.00276 -0.0997 0.4133 0.4950
4.250 0.9646 0.00916 0.00287 -0.0998 0.4117 0.4969
4.500 0.9922 0.00922 0.00297 -0.0999 0.4106 0.4988
4.750 1.0198 0.00929 0.00307 -0.1000 0.4094 0.5008
5.000 1.0473 0.00936 0.00319 -0.1002 0.4081 0.5025
5.500 1.1018 0.00950 0.00342 -0.1003 0.4054 0.5062
5.750 1.1288 0.00958 0.00355 -0.1004 0.4041 0.5083
6.000 1.1555 0.00967 0.00368 -0.1004 0.4015 0.5103
6.250 1.1815 0.00978 0.00380 -0.1003 0.3957 0.5124
6.500 1.2081 0.00987 0.00392 -0.1002 0.3905 0.5145
6.750 1.2328 0.01004 0.00408 -0.0999 0.3832 0.5167
7.250 1.2832 0.01034 0.00443 -0.0994 0.3666 0.5213
7.500 1.3043 0.01070 0.00470 -0.0985 0.3375 0.5241
7.750 1.2973 0.01255 0.00597 -0.0931 0.2426 0.5263
8.000 1.2677 0.01490 0.00775 -0.0839 0.1424 0.5280
8.250 1.2442 0.01668 0.00923 -0.0758 0.0833 0.5299
8.500 1.2106 0.01909 0.01138 -0.0674 0.0240 0.5314
9.000 1.2044 0.02216 0.01449 -0.0613 0.0046 0.5369
9.250 1.2083 0.02368 0.01607 -0.0598 0.0038 0.5403
9.500 1.2121 0.02541 0.01787 -0.0586 0.0033 0.5440
9.750 1.2158 0.02733 0.01986 -0.0576 0.0030 0.5476
10.000 1.2194 0.02933 0.02196 -0.0568 0.0028 0.5519
10.250 1.2217 0.03151 0.02421 -0.0561 0.0027 0.5565
10.500 1.2239 0.03370 0.02647 -0.0554 0.0026 0.5616
10.750 1.2232 0.03619 0.02904 -0.0546 0.0023 0.5666
11.000 1.2238 0.03854 0.03147 -0.0539 0.0022 0.5739
11.250 1.2229 0.04108 0.03410 -0.0532 0.0021 0.5805
11.500 1.2204 0.04378 0.03689 -0.0526 0.0020 0.5885
11.750 1.2190 0.04642 0.03962 -0.0520 0.0020 0.5979
12.000 1.2194 0.04894 0.04222 -0.0516 0.0019 0.6104
12.250 1.2173 0.05180 0.04519 -0.0512 0.0019 0.6247
12.500 1.2188 0.05434 0.04785 -0.0510 0.0019 0.6471
12.750 1.2205 0.05687 0.05055 -0.0508 0.0018 0.6878
13.250 1.2412 0.06231 0.05676 -0.0546 0.0016 1.0000
13.500 1.2434 0.06502 0.05952 -0.0547 0.0015 1.0000
13.750 1.2445 0.06792 0.06249 -0.0547 0.0015 1.0000
14.000 1.2467 0.07069 0.06530 -0.0548 0.0015 1.0000
14.250 1.2475 0.07369 0.06837 -0.0550 0.0014 1.0000
14.500 1.2510 0.07637 0.07110 -0.0552 0.0015 1.0000
14.750 1.2522 0.07943 0.07421 -0.0555 0.0014 1.0000
15.000 1.2518 0.08266 0.07751 -0.0558 0.0015 1.0000
15.250 1.2549 0.08549 0.08039 -0.0562 0.0013 1.0000
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