Rhode St. Genese 36 (rhodesg36-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: Rhode St. Genese 36 (rhodesg36-il) Reynolds number: 1,000,000 Max Cl/Cd: 90.99 at α=4.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-rhodesg36-il-1000000.txt Download as CSV file: xf-rhodesg36-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: Rhode St. Genese 36
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
------ -------- --------- --------- -------- -------- --------
-16.000 -0.5321 0.03954 0.03684 -0.1469 0.9658 0.0317
-15.750 -0.5933 0.03300 0.03000 -0.1492 0.9551 0.0316
-15.500 -0.6161 0.03111 0.02797 -0.1457 0.9473 0.0317
-15.250 -0.6399 0.02907 0.02576 -0.1413 0.9389 0.0318
-15.000 -0.6532 0.02791 0.02446 -0.1361 0.9323 0.0319
-14.750 -0.6569 0.02661 0.02302 -0.1324 0.9254 0.0320
-14.500 -0.6542 0.02554 0.02182 -0.1291 0.9209 0.0322
-14.250 -0.6418 0.02451 0.02067 -0.1273 0.9141 0.0325
-14.000 -0.6315 0.02347 0.01949 -0.1249 0.9085 0.0327
-13.750 -0.6159 0.02252 0.01843 -0.1233 0.9004 0.0329
-13.500 -0.6000 0.02164 0.01742 -0.1215 0.8914 0.0330
-13.250 -0.5852 0.02060 0.01622 -0.1196 0.8786 0.0332
-13.000 -0.5747 0.01903 0.01445 -0.1172 0.8622 0.0336
-12.750 -0.5563 0.01835 0.01363 -0.1155 0.8463 0.0339
-12.500 -0.5349 0.01786 0.01304 -0.1142 0.8335 0.0341
-12.250 -0.5120 0.01747 0.01257 -0.1132 0.8229 0.0344
-12.000 -0.4888 0.01711 0.01211 -0.1122 0.8132 0.0346
-11.750 -0.4647 0.01671 0.01164 -0.1114 0.8053 0.0349
-11.500 -0.4406 0.01633 0.01117 -0.1105 0.7975 0.0353
-11.250 -0.4162 0.01593 0.01068 -0.1097 0.7907 0.0357
-11.000 -0.3913 0.01549 0.01017 -0.1091 0.7839 0.0360
-10.750 -0.3665 0.01510 0.00968 -0.1083 0.7761 0.0364
-10.500 -0.3410 0.01472 0.00922 -0.1076 0.7695 0.0368
-10.250 -0.3150 0.01440 0.00882 -0.1070 0.7619 0.0371
-10.000 -0.2894 0.01408 0.00840 -0.1064 0.7542 0.0374
-9.750 -0.2653 0.01337 0.00766 -0.1057 0.7464 0.0381
-9.500 -0.2393 0.01310 0.00734 -0.1051 0.7371 0.0386
-9.250 -0.2125 0.01287 0.00709 -0.1046 0.7285 0.0390
-9.000 -0.1860 0.01266 0.00682 -0.1041 0.7183 0.0395
-8.750 -0.1593 0.01243 0.00654 -0.1036 0.7079 0.0401
-8.500 -0.1330 0.01222 0.00624 -0.1030 0.6961 0.0407
-8.250 -0.1063 0.01202 0.00597 -0.1025 0.6844 0.0412
-8.000 -0.0797 0.01186 0.00573 -0.1020 0.6742 0.0417
-7.750 -0.0542 0.01150 0.00530 -0.1014 0.6649 0.0423
-7.500 -0.0283 0.01125 0.00502 -0.1008 0.6566 0.0431
-7.250 -0.0013 0.01111 0.00486 -0.1004 0.6487 0.0437
-7.000 0.0253 0.01102 0.00471 -0.0999 0.6399 0.0445
-6.750 0.0526 0.01090 0.00456 -0.0995 0.6319 0.0454
-6.500 0.0794 0.01084 0.00444 -0.0991 0.6231 0.0463
-6.250 0.1067 0.01075 0.00430 -0.0987 0.6156 0.0469
-6.000 0.1318 0.01044 0.00397 -0.0980 0.6069 0.0481
-5.750 0.1585 0.01035 0.00386 -0.0976 0.5986 0.0490
-5.500 0.1855 0.01026 0.00375 -0.0972 0.5893 0.0500
-5.250 0.2119 0.01020 0.00364 -0.0967 0.5795 0.0511
-5.000 0.2386 0.01017 0.00355 -0.0963 0.5664 0.0520
-4.750 0.2634 0.01000 0.00333 -0.0956 0.5493 0.0535
-4.500 0.2870 0.01006 0.00327 -0.0946 0.5139 0.0547
-4.250 0.3036 0.01051 0.00336 -0.0925 0.4367 0.0559
-4.000 0.3254 0.01071 0.00339 -0.0913 0.4056 0.0572
-3.750 0.3492 0.01083 0.00341 -0.0904 0.3882 0.0581
-3.500 0.3721 0.01077 0.00330 -0.0894 0.3757 0.0599
-3.250 0.3965 0.01080 0.00329 -0.0886 0.3657 0.0616
-3.000 0.4209 0.01085 0.00329 -0.0879 0.3576 0.0633
-2.750 0.4459 0.01087 0.00328 -0.0872 0.3517 0.0648
-2.500 0.4694 0.01083 0.00322 -0.0863 0.3457 0.0672
-2.250 0.4932 0.01086 0.00322 -0.0855 0.3402 0.0695
-2.000 0.5183 0.01087 0.00322 -0.0849 0.3370 0.0717
-1.750 0.5422 0.01083 0.00319 -0.0841 0.3334 0.0756
-1.500 0.5656 0.01086 0.00320 -0.0832 0.3296 0.0794
-1.250 0.5876 0.01087 0.00323 -0.0820 0.3255 0.0913
-1.000 0.6094 0.01086 0.00336 -0.0809 0.3220 0.1444
-0.750 0.6329 0.01087 0.00342 -0.0800 0.3203 0.1569
-0.500 0.6550 0.01090 0.00346 -0.0789 0.3182 0.1639
-0.250 0.6758 0.01093 0.00351 -0.0775 0.3158 0.1707
0.000 0.6964 0.01101 0.00358 -0.0761 0.3132 0.1756
0.250 0.7164 0.01110 0.00368 -0.0747 0.3105 0.1840
0.500 0.7361 0.01123 0.00382 -0.0732 0.3075 0.1926
0.750 0.7545 0.01135 0.00402 -0.0716 0.3045 0.2251
1.000 0.7732 0.01108 0.00419 -0.0701 0.3037 0.3963
1.250 0.7794 0.01034 0.00445 -0.0661 0.3027 0.7505
1.500 0.9300 0.01041 0.00499 -0.0920 0.2992 1.0000
1.750 0.9417 0.01052 0.00509 -0.0890 0.2977 1.0000
2.000 0.9560 0.01066 0.00522 -0.0865 0.2962 1.0000
2.250 0.9718 0.01083 0.00536 -0.0843 0.2946 1.0000
2.500 0.9886 0.01102 0.00553 -0.0824 0.2928 1.0000
2.750 1.0051 0.01126 0.00573 -0.0805 0.2907 1.0000
3.000 1.0211 0.01155 0.00600 -0.0785 0.2881 1.0000
3.250 1.0409 0.01174 0.00619 -0.0772 0.2868 1.0000
3.500 1.0633 0.01184 0.00629 -0.0765 0.2853 1.0000
3.750 1.0842 0.01201 0.00646 -0.0755 0.2839 1.0000
4.000 1.1052 0.01218 0.00663 -0.0745 0.2821 1.0000
4.250 1.1259 0.01238 0.00683 -0.0735 0.2807 1.0000
4.500 1.1465 0.01260 0.00704 -0.0726 0.2792 1.0000
4.750 1.1666 0.01284 0.00728 -0.0716 0.2776 1.0000
5.000 1.1858 0.01313 0.00755 -0.0705 0.2756 1.0000
5.250 1.2044 0.01345 0.00786 -0.0693 0.2737 1.0000
5.500 1.2217 0.01386 0.00825 -0.0680 0.2708 1.0000
5.750 1.2436 0.01407 0.00847 -0.0674 0.2700 1.0000
6.000 1.2650 0.01429 0.00872 -0.0668 0.2690 1.0000
6.250 1.2859 0.01456 0.00901 -0.0661 0.2679 1.0000
6.500 1.3069 0.01483 0.00929 -0.0655 0.2667 1.0000
6.750 1.3276 0.01511 0.00960 -0.0649 0.2655 1.0000
7.000 1.3480 0.01541 0.00992 -0.0642 0.2639 1.0000
7.250 1.3679 0.01575 0.01026 -0.0636 0.2625 1.0000
7.500 1.3874 0.01611 0.01063 -0.0629 0.2606 1.0000
7.750 1.4055 0.01655 0.01107 -0.0621 0.2586 1.0000
8.000 1.4223 0.01707 0.01158 -0.0611 0.2560 1.0000
8.250 1.4412 0.01750 0.01203 -0.0604 0.2544 1.0000
8.500 1.4619 0.01784 0.01242 -0.0601 0.2533 1.0000
8.750 1.4822 0.01820 0.01282 -0.0597 0.2520 1.0000
9.000 1.5023 0.01859 0.01323 -0.0593 0.2503 1.0000
9.250 1.5217 0.01902 0.01369 -0.0589 0.2482 1.0000
9.500 1.5402 0.01951 0.01420 -0.0584 0.2460 1.0000
9.750 1.5574 0.02008 0.01478 -0.0578 0.2440 1.0000
10.000 1.5730 0.02075 0.01545 -0.0571 0.2414 1.0000
10.250 1.5895 0.02139 0.01612 -0.0565 0.2393 1.0000
10.500 1.6092 0.02185 0.01664 -0.0563 0.2376 1.0000
10.750 1.6284 0.02234 0.01717 -0.0561 0.2350 1.0000
11.000 1.6456 0.02297 0.01782 -0.0557 0.2316 1.0000
11.250 1.6603 0.02377 0.01862 -0.0552 0.2281 1.0000
11.500 1.6748 0.02459 0.01945 -0.0546 0.2247 1.0000
11.750 1.6925 0.02520 0.02012 -0.0543 0.2214 1.0000
12.000 1.7075 0.02601 0.02096 -0.0539 0.2168 1.0000
12.250 1.7186 0.02711 0.02203 -0.0532 0.2102 1.0000
12.500 1.7275 0.02838 0.02327 -0.0523 0.1990 1.0000
12.750 1.7309 0.03008 0.02490 -0.0511 0.1846 1.0000
13.000 1.7216 0.03281 0.02750 -0.0491 0.1606 1.0000
13.250 1.6928 0.03729 0.03178 -0.0461 0.1297 1.0000
13.500 1.6839 0.04034 0.03480 -0.0447 0.1185 1.0000
13.750 1.6746 0.04357 0.03802 -0.0436 0.1089 1.0000
14.000 1.6663 0.04681 0.04127 -0.0428 0.1010 1.0000
14.250 1.6563 0.05034 0.04482 -0.0421 0.0933 1.0000
14.500 1.6423 0.05441 0.04889 -0.0414 0.0819 1.0000
14.750 1.6132 0.06028 0.05474 -0.0408 0.0679 1.0000
15.000 1.5940 0.06529 0.05980 -0.0406 0.0631 1.0000
15.250 1.5780 0.07009 0.06468 -0.0408 0.0606 1.0000
15.500 1.5630 0.07495 0.06964 -0.0411 0.0595 1.0000
15.750 1.5438 0.08049 0.07528 -0.0417 0.0584 1.0000
16.000 1.5203 0.08673 0.08164 -0.0425 0.0573 1.0000
16.250 1.4976 0.09294 0.08796 -0.0435 0.0565 1.0000
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Polar data table (+)
Polar graphs
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