HOBIE (hobie-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: HOBIE (hobie-il) Reynolds number: 1,000,000 Max Cl/Cd: 102.74 at α=4.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-hobie-il-1000000-n5.txt Download as CSV file: xf-hobie-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: HOBIE
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
------ -------- --------- --------- -------- -------- --------
-12.250 -0.5532 0.09882 0.09699 -0.0309 1.0000 0.0059
-12.000 -0.5560 0.09441 0.09258 -0.0330 1.0000 0.0060
-11.500 -0.8225 0.02822 0.02558 -0.0867 0.9983 0.0048
-11.250 -0.7979 0.02483 0.02191 -0.0905 0.9959 0.0050
-11.000 -0.7716 0.02267 0.01953 -0.0928 0.9939 0.0052
-10.750 -0.7454 0.02098 0.01763 -0.0944 0.9914 0.0053
-10.500 -0.7172 0.01958 0.01606 -0.0959 0.9891 0.0055
-10.250 -0.6872 0.01840 0.01471 -0.0974 0.9871 0.0056
-10.000 -0.6589 0.01699 0.01313 -0.0988 0.9845 0.0059
-9.750 -0.6306 0.01598 0.01200 -0.0997 0.9811 0.0062
-9.500 -0.5996 0.01513 0.01103 -0.1010 0.9785 0.0065
-9.250 -0.5692 0.01437 0.01016 -0.1020 0.9753 0.0068
-9.000 -0.5402 0.01370 0.00936 -0.1027 0.9708 0.0071
-8.750 -0.5090 0.01309 0.00864 -0.1037 0.9675 0.0074
-8.500 -0.4804 0.01244 0.00789 -0.1042 0.9621 0.0078
-8.250 -0.4498 0.01184 0.00721 -0.1051 0.9568 0.0084
-8.000 -0.4208 0.01137 0.00667 -0.1055 0.9488 0.0090
-7.750 -0.3914 0.01096 0.00615 -0.1059 0.9391 0.0097
-7.500 -0.3631 0.01052 0.00561 -0.1060 0.9255 0.0104
-7.250 -0.3359 0.01014 0.00513 -0.1059 0.9083 0.0113
-7.000 -0.3093 0.00985 0.00472 -0.1056 0.8893 0.0123
-6.750 -0.2832 0.00956 0.00431 -0.1052 0.8706 0.0136
-6.500 -0.2570 0.00928 0.00394 -0.1048 0.8534 0.0155
-6.250 -0.2307 0.00901 0.00359 -0.1045 0.8384 0.0183
-6.000 -0.2043 0.00879 0.00329 -0.1042 0.8229 0.0218
-5.750 -0.1778 0.00865 0.00313 -0.1038 0.8056 0.0276
-5.500 -0.1509 0.00869 0.00317 -0.1035 0.7881 0.0342
-5.250 -0.1238 0.00871 0.00312 -0.1032 0.7728 0.0372
-5.000 -0.0966 0.00873 0.00305 -0.1029 0.7583 0.0388
-4.750 -0.0693 0.00878 0.00303 -0.1027 0.7447 0.0395
-4.500 -0.0419 0.00882 0.00301 -0.1025 0.7327 0.0399
-4.250 -0.0150 0.00856 0.00266 -0.1022 0.7211 0.0414
-4.000 0.0123 0.00843 0.00247 -0.1020 0.7101 0.0430
-3.750 0.0396 0.00838 0.00237 -0.1019 0.6992 0.0446
-3.500 0.0672 0.00830 0.00225 -0.1017 0.6891 0.0456
-3.250 0.0947 0.00817 0.00207 -0.1015 0.6806 0.0462
-3.000 0.1221 0.00807 0.00189 -0.1013 0.6708 0.0468
-2.750 0.1495 0.00799 0.00175 -0.1012 0.6580 0.0478
-2.500 0.1766 0.00792 0.00160 -0.1009 0.6407 0.0486
-2.250 0.2036 0.00789 0.00148 -0.1006 0.6208 0.0496
-2.000 0.2306 0.00789 0.00138 -0.1004 0.5991 0.0506
-1.750 0.2575 0.00791 0.00130 -0.1001 0.5782 0.0514
-1.500 0.2846 0.00794 0.00126 -0.0999 0.5589 0.0521
-1.250 0.3116 0.00798 0.00122 -0.0996 0.5398 0.0526
-1.000 0.3386 0.00803 0.00119 -0.0994 0.5205 0.0528
-0.750 0.3655 0.00807 0.00114 -0.0992 0.5008 0.0537
-0.500 0.3924 0.00811 0.00110 -0.0989 0.4806 0.0549
-0.250 0.4193 0.00817 0.00108 -0.0987 0.4592 0.0559
0.000 0.4463 0.00823 0.00107 -0.0984 0.4424 0.0570
0.250 0.4735 0.00827 0.00107 -0.0982 0.4314 0.0581
0.500 0.5007 0.00832 0.00108 -0.0980 0.4220 0.0592
0.750 0.5280 0.00836 0.00110 -0.0979 0.4132 0.0605
1.000 0.5550 0.00844 0.00114 -0.0976 0.4010 0.0622
1.250 0.5820 0.00850 0.00119 -0.0974 0.3900 0.0644
1.750 0.6359 0.00834 0.00130 -0.0972 0.3684 0.1965
2.000 0.6626 0.00840 0.00139 -0.0969 0.3503 0.2339
2.250 0.6882 0.00859 0.00150 -0.0966 0.3198 0.2530
2.500 0.7132 0.00886 0.00166 -0.0961 0.2822 0.2705
2.750 0.7363 0.00925 0.00195 -0.0954 0.2219 0.3395
3.000 0.7627 0.00935 0.00209 -0.0951 0.2145 0.3683
3.250 0.7890 0.00944 0.00224 -0.0949 0.2081 0.3991
3.500 0.8154 0.00938 0.00240 -0.0947 0.2048 0.4858
3.750 0.8400 0.00908 0.00262 -0.0942 0.2013 0.6978
4.000 0.8690 0.00864 0.00279 -0.0944 0.1973 1.0000
4.250 0.8953 0.00881 0.00296 -0.0941 0.1921 1.0000
4.500 0.9215 0.00900 0.00312 -0.0938 0.1822 1.0000
4.750 0.9473 0.00922 0.00329 -0.0934 0.1676 1.0000
5.000 0.9654 0.01028 0.00385 -0.0920 0.0723 1.0000
5.250 0.9901 0.01061 0.00414 -0.0914 0.0613 1.0000
5.500 1.0152 0.01089 0.00440 -0.0909 0.0547 1.0000
5.750 1.0406 0.01112 0.00464 -0.0905 0.0508 1.0000
6.000 1.0650 0.01145 0.00494 -0.0899 0.0422 1.0000
6.250 1.0896 0.01176 0.00522 -0.0894 0.0343 1.0000
6.500 1.1130 0.01218 0.00557 -0.0887 0.0241 1.0000
6.750 1.1368 0.01254 0.00591 -0.0880 0.0190 1.0000
7.000 1.1603 0.01293 0.00629 -0.0873 0.0158 1.0000
7.250 1.1839 0.01330 0.00665 -0.0866 0.0137 1.0000
7.500 1.2070 0.01369 0.00706 -0.0859 0.0119 1.0000
7.750 1.2300 0.01408 0.00747 -0.0852 0.0107 1.0000
8.000 1.2524 0.01452 0.00791 -0.0843 0.0096 1.0000
8.250 1.2750 0.01491 0.00835 -0.0835 0.0089 1.0000
8.500 1.2970 0.01535 0.00882 -0.0826 0.0082 1.0000
8.750 1.3180 0.01586 0.00934 -0.0816 0.0075 1.0000
9.000 1.3391 0.01632 0.00985 -0.0806 0.0070 1.0000
9.250 1.3599 0.01679 0.01036 -0.0795 0.0066 1.0000
9.500 1.3798 0.01731 0.01092 -0.0783 0.0062 1.0000
9.750 1.3988 0.01787 0.01153 -0.0770 0.0059 1.0000
10.000 1.4158 0.01856 0.01226 -0.0754 0.0055 1.0000
10.250 1.4334 0.01914 0.01290 -0.0739 0.0054 1.0000
10.500 1.4499 0.01974 0.01357 -0.0723 0.0051 1.0000
10.750 1.4635 0.02037 0.01425 -0.0701 0.0049 1.0000
11.000 1.4755 0.02103 0.01497 -0.0677 0.0048 1.0000
11.250 1.4874 0.02169 0.01569 -0.0654 0.0046 1.0000
11.500 1.4981 0.02245 0.01650 -0.0630 0.0044 1.0000
11.750 1.5071 0.02334 0.01747 -0.0606 0.0042 1.0000
12.000 1.5129 0.02448 0.01868 -0.0579 0.0040 1.0000
12.250 1.5211 0.02551 0.01980 -0.0557 0.0040 1.0000
12.500 1.5288 0.02662 0.02100 -0.0537 0.0039 1.0000
12.750 1.5351 0.02790 0.02236 -0.0516 0.0038 1.0000
13.000 1.5413 0.02926 0.02381 -0.0498 0.0037 1.0000
13.250 1.5460 0.03082 0.02546 -0.0481 0.0036 1.0000
13.500 1.5507 0.03247 0.02720 -0.0466 0.0035 1.0000
13.750 1.5542 0.03432 0.02915 -0.0453 0.0034 1.0000
14.000 1.5564 0.03639 0.03132 -0.0441 0.0034 1.0000
14.250 1.5593 0.03850 0.03352 -0.0432 0.0033 1.0000
14.500 1.5602 0.04092 0.03605 -0.0425 0.0032 1.0000
14.750 1.5599 0.04357 0.03880 -0.0420 0.0032 1.0000
15.000 1.5587 0.04646 0.04179 -0.0417 0.0032 1.0000
15.250 1.5572 0.04949 0.04493 -0.0417 0.0031 1.0000
15.500 1.5537 0.05292 0.04846 -0.0419 0.0030 1.0000
15.750 1.5501 0.05652 0.05219 -0.0424 0.0030 1.0000
16.000 1.5439 0.06065 0.05644 -0.0433 0.0030 1.0000
16.250 1.5365 0.06516 0.06107 -0.0445 0.0029 1.0000
16.500 1.5268 0.07024 0.06628 -0.0461 0.0029 1.0000
16.750 1.5159 0.07572 0.07188 -0.0481 0.0028 1.0000
17.000 1.5037 0.08164 0.07794 -0.0505 0.0028 1.0000
17.250 1.4896 0.08814 0.08457 -0.0533 0.0028 1.0000
17.500 1.4772 0.09446 0.09103 -0.0562 0.0028 1.0000
17.750 1.4642 0.10107 0.09777 -0.0593 0.0028 1.0000
18.000 1.4499 0.10815 0.10498 -0.0628 0.0028 1.0000
18.250 1.4348 0.11554 0.11251 -0.0666 0.0028 1.0000
18.500 1.4203 0.12302 0.12012 -0.0706 0.0028 1.0000
18.750 1.4062 0.13063 0.12786 -0.0749 0.0028 1.0000
19.000 1.3912 0.13862 0.13598 -0.0795 0.0027 1.0000
19.250 1.3765 0.14675 0.14424 -0.0843 0.0027 1.0000
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