Rhode St. Genese 32 (rhodesg32-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: Rhode St. Genese 32 (rhodesg32-il) Reynolds number: 500,000 Max Cl/Cd: 92.12 at α=7.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-rhodesg32-il-500000.txt Download as CSV file: xf-rhodesg32-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: Rhode St. Genese 32
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-12.000 -0.3313 0.10072 0.09834 -0.0391 1.0000 0.0390
-11.750 -0.3312 0.09772 0.09537 -0.0397 1.0000 0.0404
-11.500 -0.3696 0.08916 0.08688 -0.0471 1.0000 0.0424
-11.250 -0.2441 0.07826 0.07609 -0.0518 0.9871 0.0438
-11.000 -0.3629 0.08201 0.07978 -0.0490 0.9972 0.0431
-10.750 -0.3421 0.07977 0.07753 -0.0511 0.9923 0.0436
-10.500 -0.2606 0.05441 0.05222 -0.0777 0.9700 0.0492
-10.250 -0.3018 0.03799 0.03553 -0.0932 0.9559 0.0498
-10.000 -0.2720 0.03846 0.03608 -0.0921 0.9488 0.0503
-9.750 -0.2523 0.03639 0.03397 -0.0935 0.9406 0.0508
-9.500 -0.3121 0.03626 0.03297 -0.1005 0.9408 0.0481
-9.250 -0.3076 0.03138 0.02770 -0.1001 0.9289 0.0476
-9.000 -0.2995 0.02737 0.02321 -0.0989 0.9187 0.0473
-8.750 -0.2844 0.02478 0.02022 -0.0976 0.9098 0.0477
-8.500 -0.2664 0.02345 0.01854 -0.0961 0.9008 0.0487
-8.250 -0.2451 0.02273 0.01747 -0.0948 0.8929 0.0494
-8.000 -0.2284 0.02015 0.01461 -0.0934 0.8846 0.0498
-7.750 -0.2061 0.01865 0.01296 -0.0926 0.8771 0.0505
-7.500 -0.1821 0.01803 0.01235 -0.0919 0.8685 0.0515
-7.250 -0.1573 0.01739 0.01162 -0.0912 0.8601 0.0524
-7.000 -0.1335 0.01664 0.01076 -0.0903 0.8508 0.0531
-6.750 -0.1085 0.01589 0.00985 -0.0895 0.8425 0.0537
-6.500 -0.0839 0.01523 0.00908 -0.0887 0.8321 0.0545
-6.250 -0.0585 0.01466 0.00837 -0.0879 0.8223 0.0553
-6.000 -0.0328 0.01427 0.00787 -0.0872 0.8117 0.0562
-5.750 -0.0071 0.01393 0.00741 -0.0865 0.8002 0.0569
-5.500 0.0188 0.01367 0.00704 -0.0857 0.7876 0.0574
-5.250 0.0433 0.01253 0.00581 -0.0850 0.7740 0.0584
-5.000 0.0680 0.01196 0.00519 -0.0842 0.7579 0.0594
-4.750 0.0930 0.01161 0.00478 -0.0834 0.7409 0.0605
-4.500 0.1181 0.01136 0.00448 -0.0826 0.7237 0.0620
-4.250 0.1430 0.01113 0.00417 -0.0818 0.7051 0.0633
-4.000 0.1676 0.01094 0.00388 -0.0809 0.6847 0.0643
-3.500 0.2159 0.01071 0.00343 -0.0790 0.6362 0.0664
-3.250 0.2389 0.01065 0.00321 -0.0778 0.6040 0.0673
-3.000 0.2594 0.01051 0.00288 -0.0763 0.5557 0.0696
-2.750 0.2758 0.01086 0.00280 -0.0740 0.4556 0.0717
-2.500 0.2960 0.01113 0.00280 -0.0725 0.4026 0.0736
-2.250 0.3196 0.01122 0.00276 -0.0716 0.3839 0.0757
-2.000 0.3445 0.01125 0.00271 -0.0710 0.3738 0.0778
-1.750 0.3690 0.01125 0.00266 -0.0702 0.3664 0.0822
-1.500 0.3944 0.01121 0.00263 -0.0697 0.3614 0.0891
-1.250 0.4189 0.01110 0.00270 -0.0690 0.3570 0.1454
-1.000 0.4431 0.01105 0.00276 -0.0683 0.3531 0.1906
-0.750 0.4650 0.01073 0.00285 -0.0673 0.3499 0.3372
-0.500 0.4816 0.00993 0.00295 -0.0653 0.3475 0.6282
-0.250 0.5391 0.00936 0.00326 -0.0712 0.3433 0.9585
0.000 0.6002 0.00961 0.00341 -0.0784 0.3389 0.9923
0.250 0.6436 0.00986 0.00355 -0.0819 0.3352 1.0000
0.500 0.6655 0.01002 0.00367 -0.0807 0.3331 1.0000
0.750 0.6884 0.01013 0.00376 -0.0797 0.3318 1.0000
1.000 0.7114 0.01024 0.00386 -0.0787 0.3299 1.0000
1.250 0.7344 0.01037 0.00396 -0.0777 0.3276 1.0000
1.500 0.7573 0.01051 0.00408 -0.0768 0.3256 1.0000
1.750 0.7804 0.01066 0.00421 -0.0758 0.3239 1.0000
2.000 0.8033 0.01083 0.00435 -0.0749 0.3220 1.0000
2.250 0.8263 0.01103 0.00452 -0.0740 0.3204 1.0000
2.500 0.8492 0.01127 0.00472 -0.0731 0.3184 1.0000
2.750 0.8726 0.01150 0.00493 -0.0723 0.3165 1.0000
3.000 0.8965 0.01163 0.00508 -0.0716 0.3153 1.0000
3.250 0.9202 0.01175 0.00523 -0.0708 0.3137 1.0000
3.500 0.9437 0.01186 0.00535 -0.0701 0.3110 1.0000
3.750 0.9670 0.01198 0.00549 -0.0693 0.3080 1.0000
4.000 0.9902 0.01213 0.00564 -0.0685 0.3053 1.0000
4.250 1.0132 0.01236 0.00584 -0.0677 0.3027 1.0000
4.500 1.0365 0.01265 0.00611 -0.0670 0.2999 1.0000
4.750 1.0599 0.01272 0.00625 -0.0663 0.2981 1.0000
5.000 1.0831 0.01281 0.00639 -0.0655 0.2952 1.0000
5.250 1.1061 0.01291 0.00653 -0.0647 0.2919 1.0000
5.500 1.1286 0.01304 0.00667 -0.0639 0.2884 1.0000
5.750 1.1502 0.01330 0.00690 -0.0630 0.2842 1.0000
6.000 1.1732 0.01333 0.00703 -0.0622 0.2807 1.0000
6.250 1.1959 0.01341 0.00717 -0.0614 0.2765 1.0000
6.500 1.2173 0.01354 0.00731 -0.0604 0.2714 1.0000
6.750 1.2387 0.01367 0.00748 -0.0594 0.2657 1.0000
7.000 1.2605 0.01376 0.00763 -0.0585 0.2577 1.0000
7.250 1.2804 0.01390 0.00778 -0.0573 0.2467 1.0000
7.500 1.2955 0.01418 0.00793 -0.0552 0.2123 1.0000
7.750 1.2942 0.01542 0.00877 -0.0508 0.1584 1.0000
8.000 1.3035 0.01624 0.00952 -0.0481 0.1442 1.0000
8.250 1.3167 0.01686 0.01013 -0.0461 0.1346 1.0000
8.500 1.3299 0.01750 0.01077 -0.0442 0.1244 1.0000
8.750 1.3422 0.01820 0.01144 -0.0423 0.1130 1.0000
9.000 1.3524 0.01905 0.01221 -0.0401 0.0933 1.0000
9.250 1.3540 0.02042 0.01334 -0.0371 0.0648 1.0000
9.500 1.3602 0.02153 0.01444 -0.0348 0.0581 1.0000
9.750 1.3653 0.02275 0.01568 -0.0325 0.0543 1.0000
10.000 1.3719 0.02393 0.01692 -0.0305 0.0515 1.0000
10.250 1.3798 0.02506 0.01813 -0.0288 0.0495 1.0000
10.500 1.3845 0.02646 0.01960 -0.0270 0.0475 1.0000
10.750 1.3841 0.02830 0.02149 -0.0250 0.0455 1.0000
11.000 1.3861 0.03007 0.02335 -0.0234 0.0439 1.0000
11.250 1.3934 0.03151 0.02488 -0.0224 0.0424 1.0000
11.500 1.3974 0.03329 0.02673 -0.0213 0.0408 1.0000
11.750 1.3975 0.03549 0.02901 -0.0203 0.0395 1.0000
12.000 1.3919 0.03836 0.03196 -0.0194 0.0384 1.0000
12.250 1.3861 0.04143 0.03513 -0.0188 0.0372 1.0000
12.500 1.3911 0.04354 0.03734 -0.0186 0.0361 1.0000
12.750 1.3917 0.04618 0.04007 -0.0185 0.0349 1.0000
13.000 1.3893 0.04926 0.04324 -0.0186 0.0340 1.0000
13.250 1.3847 0.05274 0.04678 -0.0189 0.0329 1.0000
13.500 1.3736 0.05712 0.05124 -0.0194 0.0321 1.0000
13.750 1.3659 0.06123 0.05545 -0.0201 0.0313 1.0000
14.000 1.3646 0.06466 0.05899 -0.0209 0.0304 1.0000
14.250 1.3608 0.06847 0.06291 -0.0218 0.0295 1.0000
14.500 1.3552 0.07258 0.06710 -0.0228 0.0288 1.0000
14.750 1.3501 0.07670 0.07129 -0.0239 0.0282 1.0000
15.000 1.3434 0.08105 0.07571 -0.0251 0.0276 1.0000
15.250 1.3331 0.08579 0.08049 -0.0263 0.0269 1.0000
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Polar data table (+)
Polar graphs
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