Rhode St. Genese 34 (rhodesg34-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
|---|---|
|
Airfoil: Rhode St. Genese 34 (rhodesg34-il) Reynolds number: 1,000,000 Max Cl/Cd: 107.64 at α=6.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-rhodesg34-il-1000000.txt Download as CSV file: xf-rhodesg34-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: Rhode St. Genese 34
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
------ -------- --------- --------- -------- -------- --------
-13.750 -0.4910 0.03433 0.03144 -0.1375 0.8824 0.0285
-13.500 -0.5308 0.03125 0.02802 -0.1320 0.8625 0.0286
-13.250 -0.5502 0.02845 0.02486 -0.1280 0.8518 0.0287
-13.000 -0.5521 0.02643 0.02259 -0.1251 0.8451 0.0288
-12.750 -0.5467 0.02478 0.02071 -0.1227 0.8401 0.0289
-12.500 -0.5341 0.02368 0.01940 -0.1208 0.8359 0.0291
-12.250 -0.5190 0.02269 0.01825 -0.1192 0.8321 0.0292
-12.000 -0.5146 0.02011 0.01538 -0.1166 0.8284 0.0295
-11.750 -0.4966 0.01910 0.01427 -0.1152 0.8249 0.0298
-11.500 -0.4760 0.01842 0.01351 -0.1140 0.8212 0.0300
-11.250 -0.4543 0.01782 0.01282 -0.1130 0.8172 0.0302
-11.000 -0.4318 0.01732 0.01227 -0.1120 0.8134 0.0305
-10.750 -0.4090 0.01679 0.01168 -0.1110 0.8100 0.0308
-10.500 -0.3858 0.01629 0.01110 -0.1100 0.8065 0.0311
-10.250 -0.3621 0.01586 0.01060 -0.1091 0.8027 0.0314
-10.000 -0.3381 0.01542 0.01006 -0.1083 0.7985 0.0318
-9.750 -0.3143 0.01488 0.00946 -0.1074 0.7952 0.0321
-9.500 -0.2901 0.01437 0.00887 -0.1065 0.7916 0.0324
-9.250 -0.2656 0.01391 0.00834 -0.1057 0.7872 0.0327
-9.000 -0.2406 0.01354 0.00789 -0.1049 0.7826 0.0330
-8.750 -0.2151 0.01323 0.00751 -0.1042 0.7781 0.0332
-8.500 -0.1920 0.01242 0.00664 -0.1032 0.7736 0.0337
-8.250 -0.1676 0.01192 0.00612 -0.1024 0.7684 0.0342
-8.000 -0.1421 0.01163 0.00579 -0.1017 0.7632 0.0346
-7.750 -0.1161 0.01136 0.00551 -0.1011 0.7579 0.0351
-7.500 -0.0901 0.01109 0.00523 -0.1005 0.7512 0.0356
-7.250 -0.0645 0.01085 0.00493 -0.0997 0.7445 0.0361
-7.000 -0.0382 0.01060 0.00466 -0.0992 0.7371 0.0367
-6.750 -0.0125 0.01040 0.00440 -0.0984 0.7270 0.0373
-6.500 0.0138 0.01025 0.00420 -0.0978 0.7137 0.0377
-6.250 0.0370 0.00985 0.00373 -0.0967 0.6960 0.0387
-6.000 0.0609 0.00972 0.00351 -0.0957 0.6729 0.0395
-5.750 0.0852 0.00965 0.00335 -0.0947 0.6513 0.0403
-5.500 0.1097 0.00960 0.00321 -0.0938 0.6321 0.0412
-5.250 0.1347 0.00955 0.00308 -0.0930 0.6160 0.0421
-5.000 0.1597 0.00950 0.00295 -0.0922 0.6006 0.0429
-4.750 0.1840 0.00936 0.00276 -0.0913 0.5840 0.0445
-4.500 0.2089 0.00935 0.00268 -0.0905 0.5632 0.0459
-4.250 0.2325 0.00943 0.00263 -0.0895 0.5290 0.0475
-4.000 0.2506 0.00974 0.00261 -0.0875 0.4527 0.0491
-3.750 0.2707 0.00998 0.00264 -0.0859 0.4044 0.0513
-3.500 0.2942 0.01010 0.00265 -0.0849 0.3814 0.0534
-3.250 0.3186 0.01011 0.00260 -0.0841 0.3676 0.0560
-3.000 0.3434 0.01013 0.00258 -0.0833 0.3575 0.0590
-2.750 0.3690 0.01015 0.00257 -0.0827 0.3507 0.0617
-2.500 0.3935 0.01013 0.00253 -0.0820 0.3440 0.0665
-2.250 0.4192 0.01013 0.00251 -0.0814 0.3395 0.0709
-2.000 0.4445 0.01008 0.00247 -0.0808 0.3350 0.0775
-1.750 0.4684 0.00997 0.00248 -0.0800 0.3305 0.1178
-1.500 0.4929 0.01000 0.00257 -0.0793 0.3260 0.1498
-1.250 0.5185 0.01002 0.00261 -0.0788 0.3231 0.1622
-1.000 0.5446 0.01004 0.00264 -0.0783 0.3207 0.1696
-0.750 0.5701 0.01004 0.00267 -0.0778 0.3183 0.1807
-0.500 0.5952 0.01006 0.00272 -0.0772 0.3158 0.1942
-0.250 0.6194 0.01004 0.00278 -0.0765 0.3136 0.2271
0.000 0.6404 0.00979 0.00288 -0.0753 0.3111 0.3645
0.250 0.6571 0.00937 0.00302 -0.0733 0.3083 0.5789
0.500 0.6684 0.00888 0.00316 -0.0699 0.3064 0.7936
0.750 0.7625 0.00883 0.00349 -0.0841 0.3043 0.9782
1.000 0.8134 0.00902 0.00365 -0.0891 0.3025 0.9948
1.250 0.8671 0.00917 0.00375 -0.0948 0.2997 1.0000
1.500 0.8875 0.00928 0.00383 -0.0934 0.2975 1.0000
1.750 0.9077 0.00940 0.00392 -0.0919 0.2952 1.0000
2.000 0.9274 0.00955 0.00404 -0.0903 0.2930 1.0000
2.250 0.9461 0.00974 0.00420 -0.0886 0.2898 1.0000
2.500 0.9683 0.00981 0.00427 -0.0875 0.2888 1.0000
2.750 0.9901 0.00990 0.00436 -0.0864 0.2876 1.0000
3.000 1.0117 0.00999 0.00447 -0.0853 0.2862 1.0000
3.250 1.0333 0.01010 0.00457 -0.0841 0.2848 1.0000
3.500 1.0546 0.01021 0.00468 -0.0829 0.2831 1.0000
3.750 1.0757 0.01034 0.00481 -0.0817 0.2813 1.0000
4.000 1.0964 0.01049 0.00494 -0.0805 0.2791 1.0000
4.250 1.1162 0.01067 0.00510 -0.0790 0.2766 1.0000
4.500 1.1341 0.01086 0.00527 -0.0773 0.2733 1.0000
4.750 1.1548 0.01093 0.00537 -0.0760 0.2717 1.0000
5.000 1.1748 0.01104 0.00549 -0.0746 0.2697 1.0000
5.250 1.1946 0.01116 0.00563 -0.0733 0.2676 1.0000
5.500 1.2140 0.01131 0.00578 -0.0719 0.2648 1.0000
5.750 1.2330 0.01150 0.00595 -0.0704 0.2614 1.0000
6.000 1.2512 0.01173 0.00617 -0.0689 0.2580 1.0000
6.250 1.2731 0.01185 0.00633 -0.0681 0.2553 1.0000
6.500 1.2938 0.01202 0.00650 -0.0671 0.2498 1.0000
6.750 1.3120 0.01230 0.00673 -0.0657 0.2432 1.0000
7.000 1.3324 0.01251 0.00695 -0.0648 0.2358 1.0000
7.250 1.3494 0.01288 0.00726 -0.0633 0.2222 1.0000
7.500 1.3427 0.01443 0.00838 -0.0585 0.1600 1.0000
7.750 1.3487 0.01546 0.00928 -0.0557 0.1381 1.0000
8.000 1.3623 0.01612 0.00991 -0.0541 0.1292 1.0000
8.250 1.3769 0.01676 0.01053 -0.0527 0.1224 1.0000
8.500 1.3911 0.01744 0.01118 -0.0514 0.1161 1.0000
8.750 1.4060 0.01810 0.01183 -0.0502 0.1105 1.0000
9.000 1.4210 0.01876 0.01249 -0.0491 0.1054 1.0000
9.250 1.4347 0.01953 0.01324 -0.0479 0.0990 1.0000
9.500 1.4464 0.02044 0.01410 -0.0466 0.0882 1.0000
9.750 1.4447 0.02225 0.01573 -0.0440 0.0610 1.0000
10.000 1.4538 0.02340 0.01689 -0.0427 0.0567 1.0000
10.250 1.4638 0.02451 0.01804 -0.0415 0.0549 1.0000
10.500 1.4710 0.02585 0.01941 -0.0401 0.0529 1.0000
10.750 1.4778 0.02724 0.02083 -0.0388 0.0511 1.0000
11.000 1.4872 0.02848 0.02212 -0.0378 0.0500 1.0000
11.250 1.4969 0.02972 0.02342 -0.0369 0.0494 1.0000
11.500 1.5053 0.03108 0.02484 -0.0361 0.0488 1.0000
11.750 1.5122 0.03261 0.02643 -0.0352 0.0481 1.0000
12.000 1.5175 0.03433 0.02821 -0.0343 0.0472 1.0000
12.250 1.5207 0.03629 0.03024 -0.0335 0.0465 1.0000
12.500 1.5224 0.03847 0.03248 -0.0328 0.0458 1.0000
12.750 1.5208 0.04110 0.03519 -0.0321 0.0450 1.0000
13.000 1.5165 0.04413 0.03832 -0.0316 0.0443 1.0000
13.250 1.5195 0.04647 0.04074 -0.0314 0.0439 1.0000
13.500 1.5228 0.04884 0.04317 -0.0313 0.0435 1.0000
13.750 1.5232 0.05160 0.04602 -0.0313 0.0430 1.0000
14.000 1.5224 0.05455 0.04905 -0.0314 0.0426 1.0000
14.250 1.5186 0.05790 0.05249 -0.0316 0.0420 1.0000
14.500 1.5134 0.06150 0.05619 -0.0319 0.0416 1.0000
14.750 1.5058 0.06552 0.06029 -0.0324 0.0412 1.0000
15.000 1.4977 0.06967 0.06453 -0.0330 0.0408 1.0000
15.250 1.4861 0.07439 0.06934 -0.0338 0.0402 1.0000
15.500 1.4724 0.07950 0.07455 -0.0348 0.0398 1.0000
15.750 1.4568 0.08492 0.08008 -0.0359 0.0394 1.0000
16.000 1.4419 0.09025 0.08550 -0.0370 0.0392 1.0000
|
Polar data table (+)
Polar graphs
<< Back to Rhode St. Genese 34 (rhodesg34-il)