Rhode St. Genese 32 (rhodesg32-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: Rhode St. Genese 32 (rhodesg32-il) Reynolds number: 200,000 Max Cl/Cd: 64.93 at α=7.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-rhodesg32-il-200000-n5.txt Download as CSV file: xf-rhodesg32-il-200000-n5.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 = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-12.250 -0.3477 0.10052 0.09669 -0.0420 1.0000 0.0362
-12.000 -0.3621 0.09448 0.09070 -0.0449 1.0000 0.0370
-11.750 -0.3735 0.08951 0.08578 -0.0467 1.0000 0.0376
-11.500 -0.3729 0.08744 0.08376 -0.0462 1.0000 0.0378
-11.250 -0.3692 0.08644 0.08281 -0.0448 1.0000 0.0384
-11.000 -0.3647 0.08393 0.08034 -0.0459 0.9979 0.0392
-10.750 -0.3543 0.07932 0.07573 -0.0511 0.9877 0.0402
-10.500 -0.3515 0.07310 0.06951 -0.0583 0.9761 0.0409
-10.250 -0.3561 0.06325 0.05960 -0.0719 0.9610 0.0414
-10.000 -0.4098 0.03791 0.03296 -0.0916 0.9404 0.0438
-9.750 -0.3884 0.03573 0.03061 -0.0926 0.9329 0.0444
-9.500 -0.3619 0.03411 0.02886 -0.0938 0.9267 0.0450
-9.250 -0.3403 0.03260 0.02720 -0.0939 0.9184 0.0458
-9.000 -0.3153 0.03078 0.02513 -0.0947 0.9125 0.0469
-8.750 -0.2980 0.02877 0.02279 -0.0939 0.9030 0.0478
-8.250 -0.2561 0.02513 0.01843 -0.0927 0.8862 0.0493
-8.000 -0.2321 0.02381 0.01675 -0.0922 0.8787 0.0503
-7.750 -0.2102 0.02296 0.01557 -0.0911 0.8692 0.0511
-7.500 -0.1865 0.02161 0.01405 -0.0905 0.8607 0.0519
-7.250 -0.1627 0.02065 0.01299 -0.0898 0.8514 0.0526
-7.000 -0.1379 0.01986 0.01209 -0.0892 0.8431 0.0532
-6.750 -0.1128 0.01915 0.01125 -0.0885 0.8340 0.0539
-6.500 -0.0881 0.01849 0.01048 -0.0878 0.8238 0.0547
-6.250 -0.0621 0.01792 0.00978 -0.0872 0.8142 0.0558
-6.000 -0.0371 0.01740 0.00916 -0.0865 0.8033 0.0571
-5.750 -0.0115 0.01689 0.00853 -0.0858 0.7916 0.0582
-5.500 0.0143 0.01639 0.00791 -0.0851 0.7785 0.0590
-5.250 0.0403 0.01595 0.00735 -0.0844 0.7649 0.0598
-5.000 0.0660 0.01558 0.00686 -0.0837 0.7497 0.0605
-4.750 0.0908 0.01499 0.00623 -0.0829 0.7328 0.0615
-4.500 0.1153 0.01456 0.00575 -0.0821 0.7135 0.0630
-4.250 0.1400 0.01426 0.00539 -0.0812 0.6936 0.0648
-4.000 0.1647 0.01402 0.00506 -0.0804 0.6747 0.0664
-3.750 0.1892 0.01381 0.00475 -0.0795 0.6552 0.0678
-3.500 0.2135 0.01365 0.00447 -0.0786 0.6341 0.0692
-3.250 0.2376 0.01354 0.00424 -0.0777 0.6100 0.0705
-3.000 0.2608 0.01345 0.00401 -0.0766 0.5818 0.0723
-2.750 0.2831 0.01337 0.00380 -0.0754 0.5437 0.0753
-2.500 0.3034 0.01350 0.00365 -0.0738 0.4875 0.0784
-2.250 0.3232 0.01373 0.00358 -0.0722 0.4376 0.0814
-2.000 0.3450 0.01386 0.00355 -0.0710 0.4103 0.0855
-1.750 0.3678 0.01390 0.00355 -0.0700 0.3945 0.0938
-1.500 0.3908 0.01387 0.00364 -0.0692 0.3840 0.1419
-1.250 0.4142 0.01388 0.00368 -0.0683 0.3759 0.1782
-1.000 0.4373 0.01380 0.00374 -0.0675 0.3700 0.2300
-0.750 0.4591 0.01349 0.00382 -0.0665 0.3654 0.3599
-0.500 0.4720 0.01256 0.00399 -0.0636 0.3616 0.6930
0.000 0.5977 0.01272 0.00446 -0.0779 0.3527 1.0000
0.250 0.6203 0.01289 0.00456 -0.0769 0.3502 1.0000
0.500 0.6430 0.01306 0.00468 -0.0759 0.3479 1.0000
0.750 0.6657 0.01326 0.00481 -0.0749 0.3455 1.0000
1.000 0.6883 0.01347 0.00495 -0.0739 0.3429 1.0000
1.250 0.7108 0.01371 0.00511 -0.0729 0.3402 1.0000
1.500 0.7335 0.01396 0.00529 -0.0720 0.3374 1.0000
1.750 0.7570 0.01413 0.00545 -0.0712 0.3344 1.0000
2.000 0.7805 0.01433 0.00563 -0.0704 0.3318 1.0000
2.250 0.8040 0.01453 0.00582 -0.0696 0.3296 1.0000
2.500 0.8276 0.01476 0.00602 -0.0689 0.3273 1.0000
2.750 0.8511 0.01500 0.00624 -0.0682 0.3252 1.0000
3.000 0.8749 0.01527 0.00647 -0.0675 0.3234 1.0000
3.250 0.8990 0.01556 0.00673 -0.0670 0.3217 1.0000
3.500 0.9233 0.01581 0.00699 -0.0664 0.3201 1.0000
3.750 0.9472 0.01602 0.00725 -0.0658 0.3182 1.0000
4.000 0.9708 0.01623 0.00751 -0.0652 0.3156 1.0000
4.250 0.9942 0.01645 0.00777 -0.0645 0.3127 1.0000
4.500 1.0171 0.01668 0.00803 -0.0638 0.3095 1.0000
4.750 1.0397 0.01696 0.00828 -0.0630 0.3060 1.0000
5.000 1.0625 0.01724 0.00857 -0.0623 0.3026 1.0000
5.250 1.0849 0.01743 0.00887 -0.0615 0.2993 1.0000
5.500 1.1073 0.01765 0.00917 -0.0607 0.2960 1.0000
5.750 1.1291 0.01788 0.00946 -0.0599 0.2925 1.0000
6.000 1.1500 0.01815 0.00973 -0.0589 0.2885 1.0000
6.250 1.1707 0.01837 0.01004 -0.0578 0.2838 1.0000
6.500 1.1912 0.01856 0.01035 -0.0568 0.2786 1.0000
6.750 1.2105 0.01879 0.01064 -0.0555 0.2736 1.0000
7.000 1.2299 0.01903 0.01097 -0.0543 0.2682 1.0000
7.250 1.2488 0.01925 0.01130 -0.0530 0.2613 1.0000
7.500 1.2652 0.01950 0.01162 -0.0513 0.2547 1.0000
7.750 1.2823 0.01975 0.01197 -0.0497 0.2443 1.0000
8.000 1.2978 0.02004 0.01234 -0.0479 0.2258 1.0000
8.250 1.2944 0.02093 0.01285 -0.0435 0.1738 1.0000
8.500 1.2985 0.02205 0.01385 -0.0406 0.1567 1.0000
8.750 1.3055 0.02309 0.01487 -0.0383 0.1460 1.0000
9.000 1.3139 0.02407 0.01589 -0.0362 0.1381 1.0000
9.250 1.3227 0.02505 0.01693 -0.0343 0.1308 1.0000
9.500 1.3293 0.02619 0.01812 -0.0323 0.1219 1.0000
9.750 1.3374 0.02730 0.01928 -0.0306 0.1127 1.0000
10.000 1.3427 0.02862 0.02063 -0.0287 0.1022 1.0000
10.250 1.3470 0.03006 0.02207 -0.0270 0.0841 1.0000
10.500 1.3429 0.03219 0.02408 -0.0250 0.0685 1.0000
10.750 1.3394 0.03441 0.02626 -0.0233 0.0625 1.0000
11.000 1.3381 0.03660 0.02852 -0.0219 0.0592 1.0000
11.250 1.3348 0.03910 0.03108 -0.0208 0.0564 1.0000
11.500 1.3301 0.04187 0.03394 -0.0199 0.0544 1.0000
11.750 1.3250 0.04486 0.03703 -0.0193 0.0525 1.0000
12.000 1.3231 0.04766 0.03996 -0.0190 0.0509 1.0000
12.250 1.3193 0.05081 0.04324 -0.0190 0.0495 1.0000
12.500 1.3136 0.05433 0.04688 -0.0192 0.0481 1.0000
12.750 1.3058 0.05826 0.05092 -0.0196 0.0468 1.0000
13.000 1.2960 0.06265 0.05540 -0.0204 0.0457 1.0000
13.250 1.2849 0.06733 0.06018 -0.0214 0.0447 1.0000
13.500 1.2795 0.07139 0.06437 -0.0224 0.0436 1.0000
13.750 1.2762 0.07527 0.06838 -0.0234 0.0424 1.0000
14.000 1.2716 0.07936 0.07258 -0.0246 0.0412 1.0000
14.250 1.2670 0.08349 0.07682 -0.0258 0.0400 1.0000
14.500 1.2621 0.08771 0.08112 -0.0271 0.0389 1.0000
14.750 1.2565 0.09204 0.08551 -0.0285 0.0378 1.0000
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Polar data table (+)
Polar graphs
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