Rhode St. Genese 30 (rhodesg30-il) Xfoil prediction polar at RE=100,000 Ncrit=5
| Details | Polar file |
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Airfoil: Rhode St. Genese 30 (rhodesg30-il) Reynolds number: 100,000 Max Cl/Cd: 51.49 at α=6.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-rhodesg30-il-100000-n5.txt Download as CSV file: xf-rhodesg30-il-100000-n5.csv |
XFOIL Version 6.96
Calculated polar for: Rhode St. Genese 30
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.100 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-11.250 -0.4320 0.09096 0.08601 -0.0343 1.0000 0.0206
-11.000 -0.4572 0.08235 0.07753 -0.0382 1.0000 0.0198
-10.750 -0.4989 0.07211 0.06737 -0.0434 1.0000 0.0191
-10.500 -0.5203 0.06713 0.06250 -0.0456 1.0000 0.0190
-10.250 -0.5411 0.06062 0.05602 -0.0495 1.0000 0.0188
-10.000 -0.5595 0.05383 0.04914 -0.0521 1.0000 0.0186
-9.750 -0.5736 0.04756 0.04264 -0.0528 1.0000 0.0184
-9.500 -0.5800 0.04269 0.03749 -0.0521 1.0000 0.0184
-9.250 -0.5796 0.03919 0.03368 -0.0508 1.0000 0.0184
-9.000 -0.5742 0.03644 0.03063 -0.0493 1.0000 0.0185
-8.750 -0.5654 0.03418 0.02808 -0.0478 1.0000 0.0186
-8.500 -0.5540 0.03226 0.02587 -0.0462 1.0000 0.0187
-8.250 -0.5273 0.03030 0.02356 -0.0474 0.9961 0.0190
-8.000 -0.4964 0.02877 0.02176 -0.0491 0.9909 0.0195
-7.750 -0.4638 0.02758 0.02035 -0.0508 0.9861 0.0201
-7.500 -0.4331 0.02657 0.01913 -0.0520 0.9804 0.0211
-7.250 -0.3939 0.03047 0.02397 -0.0540 0.9758 0.0254
-7.000 -0.3674 0.02571 0.01806 -0.0545 0.9698 0.0381
-6.750 -0.3337 0.02461 0.01651 -0.0557 0.9651 0.0411
-6.500 -0.3017 0.02415 0.01577 -0.0566 0.9595 0.0434
-6.250 -0.2684 0.02375 0.01502 -0.0576 0.9538 0.0462
-6.000 -0.2302 0.02386 0.01509 -0.0599 0.9493 0.0507
-5.750 -0.1994 0.02384 0.01491 -0.0606 0.9407 0.0549
-5.500 -0.1585 0.02359 0.01438 -0.0631 0.9353 0.0568
-5.250 -0.1271 0.02278 0.01356 -0.0641 0.9264 0.0606
-5.000 -0.0885 0.02235 0.01307 -0.0663 0.9200 0.0650
-4.750 -0.0581 0.02208 0.01260 -0.0667 0.9101 0.0696
-4.500 -0.0211 0.02131 0.01168 -0.0685 0.9038 0.0731
-4.250 0.0073 0.02064 0.01096 -0.0685 0.8931 0.0743
-4.000 0.0386 0.02001 0.01020 -0.0688 0.8836 0.0741
-3.750 0.0716 0.01936 0.00946 -0.0695 0.8746 0.0740
-3.500 0.0994 0.01880 0.00885 -0.0691 0.8619 0.0741
-3.250 0.1268 0.01828 0.00828 -0.0686 0.8493 0.0744
-3.000 0.1540 0.01783 0.00780 -0.0682 0.8377 0.0746
-2.750 0.1816 0.01739 0.00734 -0.0678 0.8271 0.0751
-2.500 0.2086 0.01700 0.00693 -0.0674 0.8156 0.0761
-2.250 0.2341 0.01668 0.00659 -0.0667 0.8022 0.0781
-2.000 0.2601 0.01639 0.00627 -0.0660 0.7882 0.0804
-1.750 0.2865 0.01613 0.00596 -0.0654 0.7737 0.0823
-1.500 0.3130 0.01590 0.00567 -0.0648 0.7584 0.0839
-1.250 0.3398 0.01570 0.00541 -0.0642 0.7423 0.0855
-1.000 0.3666 0.01550 0.00516 -0.0636 0.7252 0.0883
-0.750 0.3932 0.01535 0.00498 -0.0630 0.7061 0.0925
-0.500 0.4197 0.01522 0.00485 -0.0624 0.6845 0.1005
-0.250 0.4462 0.01490 0.00476 -0.0620 0.6613 0.1853
0.000 0.5082 0.01288 0.00482 -0.0686 0.6288 1.0000
0.250 0.5313 0.01306 0.00478 -0.0674 0.5995 1.0000
0.500 0.5541 0.01328 0.00479 -0.0662 0.5691 1.0000
0.750 0.5767 0.01353 0.00483 -0.0650 0.5389 1.0000
1.000 0.5993 0.01381 0.00492 -0.0639 0.5114 1.0000
1.250 0.6221 0.01411 0.00503 -0.0628 0.4889 1.0000
1.500 0.6453 0.01442 0.00519 -0.0619 0.4717 1.0000
1.750 0.6688 0.01475 0.00540 -0.0611 0.4579 1.0000
2.000 0.6927 0.01508 0.00562 -0.0604 0.4467 1.0000
2.250 0.7168 0.01542 0.00587 -0.0597 0.4371 1.0000
2.500 0.7413 0.01575 0.00618 -0.0591 0.4287 1.0000
2.750 0.7658 0.01611 0.00648 -0.0586 0.4213 1.0000
3.000 0.7905 0.01645 0.00682 -0.0581 0.4140 1.0000
3.250 0.8150 0.01682 0.00719 -0.0575 0.4069 1.0000
3.500 0.8397 0.01719 0.00757 -0.0570 0.3999 1.0000
3.750 0.8634 0.01757 0.00793 -0.0564 0.3904 1.0000
4.000 0.8865 0.01792 0.00833 -0.0557 0.3794 1.0000
4.250 0.9089 0.01828 0.00870 -0.0548 0.3672 1.0000
4.500 0.9310 0.01864 0.00907 -0.0539 0.3549 1.0000
4.750 0.9525 0.01899 0.00944 -0.0529 0.3415 1.0000
5.000 0.9742 0.01931 0.00987 -0.0520 0.3289 1.0000
5.250 0.9964 0.01964 0.01032 -0.0512 0.3180 1.0000
5.500 1.0182 0.02000 0.01077 -0.0503 0.3074 1.0000
5.750 1.0390 0.02033 0.01124 -0.0492 0.2931 1.0000
6.000 1.0598 0.02065 0.01172 -0.0482 0.2772 1.0000
6.250 1.0807 0.02099 0.01224 -0.0472 0.2575 1.0000
6.500 1.0981 0.02145 0.01269 -0.0457 0.2060 1.0000
6.750 1.1044 0.02288 0.01355 -0.0430 0.1423 1.0000
7.000 1.1147 0.02433 0.01485 -0.0409 0.1103 1.0000
7.250 1.1265 0.02556 0.01605 -0.0389 0.0852 1.0000
7.500 1.1365 0.02681 0.01726 -0.0368 0.0727 1.0000
7.750 1.1455 0.02801 0.01851 -0.0345 0.0677 1.0000
8.000 1.1513 0.02922 0.01981 -0.0317 0.0641 1.0000
8.250 1.1534 0.03062 0.02130 -0.0287 0.0608 1.0000
8.500 1.1534 0.03221 0.02295 -0.0258 0.0578 1.0000
8.750 1.1566 0.03369 0.02461 -0.0234 0.0548 1.0000
9.000 1.1580 0.03539 0.02645 -0.0212 0.0521 1.0000
9.250 1.1566 0.03741 0.02856 -0.0192 0.0491 1.0000
9.500 1.1524 0.03983 0.03099 -0.0172 0.0466 1.0000
9.750 1.1560 0.04179 0.03311 -0.0158 0.0441 1.0000
10.000 1.1599 0.04382 0.03532 -0.0146 0.0414 1.0000
10.250 1.1626 0.04606 0.03769 -0.0136 0.0388 1.0000
10.500 1.1643 0.04850 0.04017 -0.0127 0.0365 1.0000
10.750 1.1679 0.05112 0.04280 -0.0117 0.0339 1.0000
11.000 1.1723 0.05353 0.04546 -0.0111 0.0321 1.0000
11.250 1.1752 0.05618 0.04832 -0.0106 0.0301 1.0000
11.500 1.1767 0.05899 0.05128 -0.0103 0.0284 1.0000
11.750 1.1758 0.06198 0.05437 -0.0105 0.0269 1.0000
12.000 1.1764 0.06502 0.05746 -0.0106 0.0256 1.0000
12.250 1.1764 0.06852 0.06112 -0.0105 0.0246 1.0000
12.500 1.1715 0.07254 0.06544 -0.0112 0.0238 1.0000
12.750 1.1655 0.07686 0.07002 -0.0121 0.0232 1.0000
13.000 1.1559 0.08175 0.07518 -0.0137 0.0225 1.0000
13.250 1.1456 0.08698 0.08064 -0.0156 0.0221 1.0000
13.500 1.1337 0.09268 0.08657 -0.0181 0.0217 1.0000
13.750 1.1204 0.09888 0.09299 -0.0211 0.0214 1.0000
14.000 1.1048 0.10582 0.10014 -0.0247 0.0211 1.0000
14.250 1.0877 0.11343 0.10795 -0.0289 0.0211 1.0000
14.500 1.0676 0.12211 0.11683 -0.0339 0.0213 1.0000
14.750 1.0451 0.13187 0.12677 -0.0397 0.0216 1.0000
15.000 1.0200 0.14304 0.13808 -0.0464 0.0223 1.0000
15.250 0.9916 0.15638 0.15151 -0.0542 0.0229 1.0000
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Polar data table (+)
Polar graphs
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