Rhode St. Genese 34 (rhodesg34-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: Rhode St. Genese 34 (rhodesg34-il) Reynolds number: 500,000 Max Cl/Cd: 81.62 at α=6.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-rhodesg34-il-500000.txt Download as CSV file: xf-rhodesg34-il-500000.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 = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-12.750 -0.1982 0.10382 0.10140 -0.0596 0.9603 0.0397
-12.500 -0.1785 0.09949 0.09703 -0.0652 0.9514 0.0409
-12.250 -0.1821 0.08917 0.08667 -0.0790 0.9433 0.0430
-12.000 -0.1501 0.08581 0.08327 -0.0841 0.9353 0.0433
-11.750 -0.1187 0.08291 0.08032 -0.0889 0.9268 0.0438
-11.500 -0.0905 0.07927 0.07662 -0.0951 0.9162 0.0444
-11.250 -0.0673 0.07553 0.07279 -0.1010 0.9033 0.0456
-11.000 -0.1072 0.06260 0.05975 -0.1157 0.8833 0.0486
-10.750 -0.0992 0.06060 0.05770 -0.1160 0.8739 0.0489
-10.500 -0.0952 0.05855 0.05563 -0.1164 0.8659 0.0491
-10.250 -0.1064 0.05532 0.05235 -0.1174 0.8569 0.0494
-10.000 -0.2413 0.03300 0.02885 -0.1180 0.8459 0.0424
-9.750 -0.2316 0.03060 0.02632 -0.1166 0.8403 0.0419
-9.500 -0.2252 0.02767 0.02306 -0.1146 0.8347 0.0413
-9.250 -0.2165 0.02505 0.02010 -0.1125 0.8296 0.0413
-9.000 -0.2028 0.02306 0.01778 -0.1106 0.8243 0.0416
-8.750 -0.1857 0.02133 0.01574 -0.1090 0.8192 0.0417
-8.500 -0.1658 0.01997 0.01411 -0.1077 0.8143 0.0418
-8.250 -0.1450 0.01883 0.01276 -0.1064 0.8090 0.0421
-8.000 -0.1223 0.01798 0.01170 -0.1052 0.8033 0.0425
-7.750 -0.0985 0.01711 0.01062 -0.1043 0.7977 0.0429
-7.500 -0.0754 0.01604 0.00952 -0.1034 0.7919 0.0435
-7.250 -0.0506 0.01547 0.00891 -0.1027 0.7854 0.0441
-7.000 -0.0247 0.01509 0.00845 -0.1021 0.7797 0.0449
-6.750 0.0002 0.01464 0.00800 -0.1013 0.7732 0.0458
-6.500 0.0256 0.01419 0.00748 -0.1005 0.7663 0.0466
-6.250 0.0512 0.01374 0.00693 -0.0998 0.7594 0.0474
-6.000 0.0765 0.01336 0.00649 -0.0989 0.7504 0.0481
-5.750 0.1012 0.01268 0.00578 -0.0981 0.7422 0.0492
-5.500 0.1262 0.01230 0.00542 -0.0974 0.7319 0.0502
-5.250 0.1515 0.01200 0.00511 -0.0966 0.7214 0.0515
-5.000 0.1765 0.01174 0.00479 -0.0957 0.7084 0.0530
-4.750 0.2017 0.01160 0.00456 -0.0949 0.6921 0.0545
-4.500 0.2243 0.01117 0.00409 -0.0937 0.6732 0.0564
-4.250 0.2477 0.01103 0.00387 -0.0925 0.6523 0.0584
-4.000 0.2711 0.01096 0.00368 -0.0914 0.6319 0.0605
-3.750 0.2933 0.01080 0.00343 -0.0901 0.6113 0.0630
-3.500 0.3155 0.01075 0.00329 -0.0888 0.5883 0.0660
-3.250 0.3378 0.01078 0.00320 -0.0875 0.5564 0.0693
-3.000 0.3548 0.01085 0.00305 -0.0853 0.4954 0.0736
-2.500 0.3898 0.01133 0.00305 -0.0812 0.4056 0.0847
-2.250 0.4113 0.01133 0.00307 -0.0799 0.3911 0.1031
-2.000 0.4337 0.01137 0.00319 -0.0788 0.3808 0.1563
-1.750 0.4573 0.01140 0.00325 -0.0779 0.3736 0.1778
-1.500 0.4810 0.01144 0.00330 -0.0771 0.3677 0.1948
-1.250 0.5037 0.01149 0.00338 -0.0761 0.3623 0.2194
-1.000 0.5260 0.01139 0.00346 -0.0751 0.3579 0.2837
-0.750 0.5445 0.01088 0.00355 -0.0735 0.3542 0.4837
-0.500 0.5542 0.01020 0.00369 -0.0697 0.3507 0.7479
-0.250 0.6516 0.01032 0.00417 -0.0842 0.3440 0.9749
0.000 0.7005 0.01060 0.00437 -0.0887 0.3404 0.9938
0.250 0.7457 0.01076 0.00448 -0.0925 0.3376 1.0000
0.500 0.7660 0.01087 0.00456 -0.0910 0.3351 1.0000
0.750 0.7859 0.01101 0.00465 -0.0895 0.3321 1.0000
1.000 0.8058 0.01118 0.00477 -0.0880 0.3298 1.0000
1.250 0.8254 0.01138 0.00492 -0.0864 0.3275 1.0000
1.500 0.8451 0.01163 0.00510 -0.0849 0.3252 1.0000
1.750 0.8660 0.01182 0.00527 -0.0836 0.3236 1.0000
2.000 0.8875 0.01195 0.00540 -0.0824 0.3223 1.0000
2.250 0.9090 0.01208 0.00553 -0.0812 0.3206 1.0000
2.500 0.9302 0.01222 0.00567 -0.0800 0.3184 1.0000
2.750 0.9511 0.01236 0.00579 -0.0788 0.3157 1.0000
3.000 0.9718 0.01252 0.00594 -0.0775 0.3133 1.0000
3.250 0.9922 0.01273 0.00611 -0.0762 0.3111 1.0000
3.500 1.0126 0.01299 0.00634 -0.0749 0.3087 1.0000
3.750 1.0339 0.01327 0.00659 -0.0739 0.3064 1.0000
4.000 1.0548 0.01340 0.00675 -0.0727 0.3052 1.0000
4.250 1.0748 0.01355 0.00693 -0.0713 0.3037 1.0000
4.500 1.0941 0.01371 0.00711 -0.0698 0.3021 1.0000
4.750 1.1132 0.01387 0.00729 -0.0683 0.3002 1.0000
5.000 1.1316 0.01403 0.00746 -0.0668 0.2977 1.0000
5.250 1.1503 0.01422 0.00765 -0.0653 0.2954 1.0000
5.500 1.1690 0.01446 0.00787 -0.0639 0.2928 1.0000
5.750 1.1893 0.01481 0.00819 -0.0629 0.2898 1.0000
6.000 1.2085 0.01495 0.00839 -0.0616 0.2883 1.0000
6.250 1.2278 0.01512 0.00861 -0.0603 0.2861 1.0000
6.500 1.2473 0.01531 0.00885 -0.0592 0.2837 1.0000
6.750 1.2660 0.01551 0.00908 -0.0580 0.2806 1.0000
7.000 1.2843 0.01577 0.00935 -0.0567 0.2777 1.0000
7.250 1.3020 0.01612 0.00968 -0.0555 0.2746 1.0000
7.500 1.3213 0.01637 0.01000 -0.0545 0.2719 1.0000
7.750 1.3409 0.01660 0.01030 -0.0536 0.2685 1.0000
8.000 1.3594 0.01687 0.01061 -0.0526 0.2641 1.0000
8.250 1.3763 0.01725 0.01100 -0.0514 0.2601 1.0000
8.500 1.3948 0.01759 0.01139 -0.0505 0.2550 1.0000
8.750 1.4129 0.01795 0.01178 -0.0496 0.2479 1.0000
9.000 1.4294 0.01842 0.01226 -0.0486 0.2412 1.0000
9.500 1.4537 0.01992 0.01362 -0.0459 0.1979 1.0000
9.750 1.4448 0.02209 0.01548 -0.0425 0.1566 1.0000
10.000 1.4490 0.02352 0.01685 -0.0405 0.1437 1.0000
10.250 1.4548 0.02490 0.01821 -0.0389 0.1346 1.0000
10.500 1.4624 0.02617 0.01949 -0.0375 0.1278 1.0000
10.750 1.4702 0.02746 0.02081 -0.0363 0.1223 1.0000
11.000 1.4783 0.02876 0.02213 -0.0351 0.1166 1.0000
11.250 1.4832 0.03034 0.02371 -0.0339 0.1097 1.0000
11.500 1.4877 0.03199 0.02537 -0.0327 0.1024 1.0000
11.750 1.4917 0.03375 0.02714 -0.0316 0.0915 1.0000
12.000 1.4850 0.03649 0.02978 -0.0302 0.0705 1.0000
12.250 1.4766 0.03956 0.03280 -0.0290 0.0635 1.0000
12.500 1.4744 0.04223 0.03554 -0.0284 0.0615 1.0000
12.750 1.4688 0.04537 0.03875 -0.0278 0.0597 1.0000
13.000 1.4623 0.04877 0.04222 -0.0275 0.0582 1.0000
13.250 1.4552 0.05237 0.04592 -0.0274 0.0570 1.0000
13.500 1.4503 0.05581 0.04947 -0.0275 0.0564 1.0000
13.750 1.4420 0.05977 0.05355 -0.0277 0.0557 1.0000
14.000 1.4327 0.06397 0.05787 -0.0282 0.0551 1.0000
14.250 1.4195 0.06880 0.06282 -0.0289 0.0544 1.0000
14.500 1.4056 0.07386 0.06800 -0.0297 0.0539 1.0000
14.750 1.3913 0.07909 0.07334 -0.0307 0.0534 1.0000
15.000 1.3761 0.08447 0.07883 -0.0318 0.0528 1.0000
15.250 1.3613 0.08981 0.08425 -0.0330 0.0522 1.0000
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