S1046 17% (Danny Howell) (s1046-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: S1046 17% (Danny Howell) (s1046-il) Reynolds number: 1,000,000 Max Cl/Cd: 90.87 at α=9° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-s1046-il-1000000.txt Download as CSV file: xf-s1046-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: S1046 17% (Danny Howell)
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.500 -1.1274 0.10837 0.10454 -0.0092 1.0000 0.0101
-19.250 -1.1390 0.10283 0.09891 -0.0119 1.0000 0.0103
-19.000 -1.1516 0.09725 0.09325 -0.0145 1.0000 0.0105
-18.750 -1.1636 0.09187 0.08779 -0.0169 1.0000 0.0107
-18.500 -1.1747 0.08673 0.08256 -0.0191 1.0000 0.0109
-18.250 -1.1850 0.08179 0.07753 -0.0212 1.0000 0.0111
-18.000 -1.1924 0.07738 0.07304 -0.0230 1.0000 0.0115
-17.750 -1.2018 0.07277 0.06833 -0.0248 1.0000 0.0117
-17.500 -1.2091 0.06852 0.06399 -0.0263 1.0000 0.0119
-17.250 -1.2143 0.06464 0.06003 -0.0277 1.0000 0.0122
-17.000 -1.2270 0.05987 0.05517 -0.0293 1.0000 0.0126
-16.750 -1.2383 0.05541 0.05063 -0.0308 1.0000 0.0131
-16.500 -1.2432 0.05186 0.04700 -0.0318 1.0000 0.0134
-16.250 -1.2478 0.04844 0.04351 -0.0326 1.0000 0.0138
-16.000 -1.2506 0.04532 0.04031 -0.0333 1.0000 0.0144
-15.750 -1.2498 0.04271 0.03762 -0.0337 1.0000 0.0149
-15.500 -1.2537 0.03968 0.03451 -0.0341 1.0000 0.0155
-15.250 -1.2573 0.03679 0.03156 -0.0343 1.0000 0.0163
-15.000 -1.2574 0.03433 0.02905 -0.0343 1.0000 0.0171
-14.750 -1.2549 0.03219 0.02684 -0.0341 1.0000 0.0179
-14.500 -1.2524 0.03012 0.02472 -0.0338 1.0000 0.0191
-14.250 -1.2506 0.02808 0.02264 -0.0333 1.0000 0.0204
-14.000 -1.2461 0.02635 0.02087 -0.0326 1.0000 0.0218
-13.750 -1.2420 0.02468 0.01916 -0.0318 1.0000 0.0238
-13.500 -1.2376 0.02313 0.01759 -0.0307 1.0000 0.0262
-13.250 -1.2332 0.02170 0.01614 -0.0294 1.0000 0.0294
-12.750 -1.2221 0.01930 0.01374 -0.0261 1.0000 0.0377
-12.500 -1.2154 0.01833 0.01277 -0.0241 1.0000 0.0423
-12.250 -1.2075 0.01751 0.01194 -0.0220 1.0000 0.0471
-12.000 -1.2011 0.01670 0.01116 -0.0194 1.0000 0.0527
-11.750 -1.1923 0.01608 0.01054 -0.0169 1.0000 0.0581
-11.500 -1.1846 0.01549 0.00998 -0.0139 1.0000 0.0638
-11.250 -1.1765 0.01494 0.00946 -0.0109 1.0000 0.0710
-11.000 -1.1624 0.01445 0.00899 -0.0088 1.0000 0.0782
-10.750 -1.1483 0.01394 0.00852 -0.0067 1.0000 0.0863
-10.500 -1.1335 0.01346 0.00809 -0.0047 1.0000 0.0949
-10.250 -1.1174 0.01305 0.00771 -0.0029 1.0000 0.1031
-10.000 -1.1018 0.01263 0.00733 -0.0009 1.0000 0.1126
-9.750 -1.0864 0.01221 0.00697 0.0012 1.0000 0.1226
-9.250 -1.0169 0.01122 0.00614 -0.0027 0.9837 0.1519
-9.000 -0.9794 0.01078 0.00576 -0.0052 0.9670 0.1662
-8.750 -0.9426 0.01040 0.00540 -0.0073 0.9408 0.1791
-8.500 -0.9181 0.01015 0.00511 -0.0067 0.9061 0.1910
-8.250 -0.8958 0.00996 0.00486 -0.0057 0.8782 0.2023
-8.000 -0.8726 0.00980 0.00464 -0.0048 0.8558 0.2126
-7.750 -0.8489 0.00959 0.00441 -0.0040 0.8367 0.2235
-7.500 -0.8240 0.00943 0.00421 -0.0035 0.8197 0.2328
-7.250 -0.7987 0.00929 0.00403 -0.0030 0.8047 0.2413
-7.000 -0.7733 0.00913 0.00384 -0.0026 0.7907 0.2500
-6.750 -0.7468 0.00902 0.00369 -0.0023 0.7778 0.2587
-6.500 -0.7211 0.00884 0.00351 -0.0019 0.7661 0.2688
-6.250 -0.6944 0.00873 0.00336 -0.0017 0.7551 0.2768
-6.000 -0.6679 0.00859 0.00321 -0.0014 0.7444 0.2857
-5.750 -0.6408 0.00848 0.00308 -0.0013 0.7345 0.2933
-5.500 -0.6140 0.00837 0.00294 -0.0010 0.7248 0.3021
-5.250 -0.5867 0.00825 0.00282 -0.0009 0.7151 0.3099
-5.000 -0.5594 0.00815 0.00270 -0.0008 0.7063 0.3186
-4.750 -0.5321 0.00804 0.00258 -0.0006 0.6967 0.3272
-4.500 -0.5043 0.00796 0.00248 -0.0006 0.6880 0.3360
-4.250 -0.4770 0.00785 0.00238 -0.0004 0.6787 0.3450
-3.750 -0.4216 0.00769 0.00219 -0.0003 0.6606 0.3629
-3.500 -0.3935 0.00761 0.00211 -0.0003 0.6515 0.3714
-3.250 -0.3658 0.00755 0.00203 -0.0002 0.6422 0.3811
-3.000 -0.3377 0.00746 0.00196 -0.0002 0.6325 0.3899
-2.750 -0.3096 0.00742 0.00189 -0.0001 0.6230 0.3992
-2.500 -0.2818 0.00734 0.00183 -0.0001 0.6128 0.4090
-2.250 -0.2534 0.00730 0.00178 -0.0001 0.6027 0.4181
-2.000 -0.2256 0.00725 0.00172 0.0000 0.5924 0.4283
-1.750 -0.1974 0.00721 0.00168 0.0000 0.5818 0.4379
-1.500 -0.1690 0.00718 0.00164 -0.0001 0.5713 0.4479
-1.250 -0.1412 0.00715 0.00161 0.0000 0.5605 0.4579
-1.000 -0.1128 0.00713 0.00158 0.0000 0.5498 0.4675
-0.750 -0.0846 0.00711 0.00156 0.0000 0.5395 0.4780
-0.500 -0.0566 0.00710 0.00154 0.0000 0.5286 0.4878
0.000 0.0000 0.00708 0.00153 0.0000 0.5085 0.5084
0.500 0.0566 0.00710 0.00154 0.0000 0.4878 0.5286
0.750 0.0846 0.00711 0.00156 0.0000 0.4779 0.5395
1.000 0.1128 0.00713 0.00158 0.0000 0.4674 0.5499
1.250 0.1412 0.00715 0.00161 0.0000 0.4579 0.5606
1.500 0.1690 0.00718 0.00164 0.0001 0.4478 0.5714
1.750 0.1974 0.00721 0.00168 0.0000 0.4379 0.5818
2.000 0.2256 0.00725 0.00172 0.0000 0.4283 0.5924
2.250 0.2534 0.00730 0.00178 0.0001 0.4181 0.6028
2.500 0.2818 0.00734 0.00183 0.0001 0.4090 0.6129
2.750 0.3096 0.00742 0.00189 0.0001 0.3993 0.6230
3.000 0.3377 0.00746 0.00196 0.0002 0.3899 0.6325
3.250 0.3658 0.00755 0.00203 0.0002 0.3811 0.6422
3.500 0.3935 0.00761 0.00211 0.0003 0.3713 0.6515
3.750 0.4216 0.00769 0.00219 0.0003 0.3629 0.6606
4.250 0.4770 0.00785 0.00238 0.0004 0.3449 0.6787
4.500 0.5043 0.00796 0.00248 0.0006 0.3360 0.6881
4.750 0.5321 0.00804 0.00258 0.0006 0.3272 0.6967
5.000 0.5594 0.00815 0.00270 0.0008 0.3186 0.7061
5.250 0.5867 0.00825 0.00282 0.0009 0.3099 0.7152
5.500 0.6140 0.00837 0.00294 0.0010 0.3021 0.7248
5.750 0.6408 0.00848 0.00308 0.0013 0.2934 0.7344
6.000 0.6679 0.00859 0.00321 0.0014 0.2857 0.7443
6.250 0.6944 0.00873 0.00336 0.0017 0.2768 0.7551
6.500 0.7211 0.00884 0.00351 0.0019 0.2689 0.7660
6.750 0.7468 0.00902 0.00369 0.0023 0.2588 0.7777
7.000 0.7733 0.00913 0.00384 0.0026 0.2499 0.7907
7.250 0.7987 0.00929 0.00403 0.0030 0.2411 0.8047
7.500 0.8241 0.00943 0.00421 0.0035 0.2327 0.8196
7.750 0.8489 0.00959 0.00441 0.0040 0.2236 0.8365
8.000 0.8726 0.00980 0.00464 0.0048 0.2125 0.8557
8.250 0.8959 0.00996 0.00486 0.0056 0.2024 0.8781
8.500 0.9182 0.01015 0.00510 0.0067 0.1911 0.9061
8.750 0.9427 0.01040 0.00540 0.0073 0.1790 0.9411
9.000 0.9796 0.01078 0.00576 0.0051 0.1660 0.9672
9.250 1.0171 0.01121 0.00614 0.0027 0.1527 0.9837
9.750 1.0866 0.01220 0.00697 -0.0012 0.1233 1.0000
10.000 1.1018 0.01263 0.00733 0.0009 0.1124 1.0000
10.250 1.1172 0.01306 0.00771 0.0029 0.1027 1.0000
10.500 1.1335 0.01346 0.00809 0.0047 0.0947 1.0000
10.750 1.1485 0.01394 0.00852 0.0067 0.0864 1.0000
11.000 1.1624 0.01446 0.00899 0.0088 0.0780 1.0000
11.250 1.1762 0.01496 0.00947 0.0109 0.0704 1.0000
11.500 1.1852 0.01549 0.00997 0.0138 0.0640 1.0000
11.750 1.1925 0.01608 0.01055 0.0168 0.0580 1.0000
12.000 1.2013 0.01671 0.01117 0.0194 0.0524 1.0000
12.250 1.2079 0.01750 0.01194 0.0219 0.0470 1.0000
12.500 1.2158 0.01833 0.01277 0.0241 0.0421 1.0000
12.750 1.2228 0.01929 0.01372 0.0260 0.0378 1.0000
13.000 1.2272 0.02050 0.01492 0.0279 0.0329 1.0000
13.250 1.2333 0.02172 0.01615 0.0294 0.0292 1.0000
13.500 1.2386 0.02310 0.01756 0.0306 0.0263 1.0000
13.750 1.2427 0.02467 0.01915 0.0317 0.0237 1.0000
14.000 1.2472 0.02632 0.02084 0.0325 0.0218 1.0000
14.250 1.2516 0.02806 0.02262 0.0331 0.0203 1.0000
14.500 1.2528 0.03016 0.02476 0.0336 0.0189 1.0000
14.750 1.2565 0.03212 0.02678 0.0339 0.0180 1.0000
15.000 1.2588 0.03429 0.02901 0.0341 0.0170 1.0000
15.250 1.2582 0.03680 0.03157 0.0341 0.0162 1.0000
15.500 1.2541 0.03975 0.03457 0.0339 0.0153 1.0000
15.750 1.2531 0.04248 0.03739 0.0335 0.0147 1.0000
16.000 1.2523 0.04528 0.04026 0.0331 0.0143 1.0000
16.250 1.2501 0.04833 0.04339 0.0324 0.0137 1.0000
16.500 1.2453 0.05180 0.04694 0.0315 0.0134 1.0000
16.750 1.2390 0.05553 0.05073 0.0304 0.0129 1.0000
17.000 1.2281 0.05996 0.05525 0.0290 0.0125 1.0000
17.250 1.2150 0.06478 0.06017 0.0273 0.0121 1.0000
17.500 1.2120 0.06836 0.06383 0.0261 0.0118 1.0000
17.750 1.2028 0.07289 0.06845 0.0244 0.0116 1.0000
18.000 1.1950 0.07727 0.07292 0.0227 0.0112 1.0000
18.250 1.1863 0.08188 0.07761 0.0208 0.0111 1.0000
18.500 1.1777 0.08656 0.08238 0.0189 0.0110 1.0000
18.750 1.1672 0.09161 0.08752 0.0167 0.0108 1.0000
19.000 1.1537 0.09720 0.09321 0.0142 0.0106 1.0000
19.250 1.1438 0.10236 0.09844 0.0118 0.0104 1.0000
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