Rhode St. Genese 36 (rhodesg36-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: Rhode St. Genese 36 (rhodesg36-il) Reynolds number: 500,000 Max Cl/Cd: 70.54 at α=5.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-rhodesg36-il-500000.txt Download as CSV file: xf-rhodesg36-il-500000.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 = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-13.500 -0.0379 0.09291 0.09027 -0.1076 0.9717 0.0469
-13.250 -0.0183 0.09050 0.08785 -0.1088 0.9682 0.0471
-13.000 -0.0033 0.08854 0.08589 -0.1092 0.9625 0.0474
-12.750 0.0104 0.08664 0.08398 -0.1095 0.9570 0.0477
-12.500 0.0151 0.08484 0.08219 -0.1086 0.9490 0.0481
-12.250 0.0172 0.08289 0.08023 -0.1077 0.9405 0.0485
-12.000 0.0178 0.08063 0.07798 -0.1071 0.9324 0.0490
-11.750 -0.0504 0.06881 0.06618 -0.1152 0.9142 0.0523
-11.500 -0.0425 0.06728 0.06466 -0.1136 0.9035 0.0525
-11.250 -0.2297 0.04114 0.03788 -0.1234 0.8604 0.0472
-11.000 -0.2204 0.03972 0.03639 -0.1218 0.8484 0.0474
-10.750 -0.2087 0.03855 0.03512 -0.1204 0.8366 0.0477
-10.500 -0.2352 0.03195 0.02795 -0.1178 0.8245 0.0447
-10.250 -0.2434 0.02747 0.02286 -0.1151 0.8140 0.0444
-10.000 -0.2331 0.02514 0.02017 -0.1133 0.8054 0.0446
-9.750 -0.2181 0.02339 0.01809 -0.1118 0.7968 0.0450
-9.500 -0.2002 0.02198 0.01638 -0.1104 0.7886 0.0456
-9.250 -0.1806 0.02082 0.01491 -0.1091 0.7796 0.0464
-9.000 -0.1593 0.02003 0.01380 -0.1078 0.7717 0.0469
-8.750 -0.1365 0.01867 0.01237 -0.1072 0.7635 0.0474
-8.500 -0.1117 0.01806 0.01169 -0.1065 0.7559 0.0480
-8.250 -0.0862 0.01756 0.01116 -0.1060 0.7483 0.0486
-8.000 -0.0608 0.01705 0.01057 -0.1054 0.7397 0.0492
-7.750 -0.0354 0.01653 0.00993 -0.1047 0.7314 0.0500
-7.500 -0.0098 0.01601 0.00929 -0.1041 0.7223 0.0509
-7.250 0.0159 0.01560 0.00872 -0.1034 0.7142 0.0517
-7.000 0.0417 0.01499 0.00803 -0.1029 0.7055 0.0527
-6.500 0.0938 0.01426 0.00725 -0.1019 0.6873 0.0548
-6.250 0.1198 0.01396 0.00686 -0.1013 0.6787 0.0558
-6.000 0.1461 0.01367 0.00651 -0.1008 0.6698 0.0570
-5.750 0.1722 0.01352 0.00623 -0.1002 0.6602 0.0580
-5.500 0.1973 0.01297 0.00569 -0.0996 0.6511 0.0593
-5.250 0.2227 0.01276 0.00544 -0.0989 0.6413 0.0607
-5.000 0.2486 0.01257 0.00524 -0.0984 0.6317 0.0624
-4.500 0.2990 0.01217 0.00473 -0.0970 0.6111 0.0653
-4.250 0.3228 0.01194 0.00448 -0.0961 0.5996 0.0671
-4.000 0.3471 0.01180 0.00431 -0.0953 0.5851 0.0690
-3.750 0.3709 0.01174 0.00418 -0.0943 0.5666 0.0710
-3.500 0.3920 0.01160 0.00396 -0.0929 0.5371 0.0731
-3.250 0.4050 0.01182 0.00387 -0.0901 0.4691 0.0751
-3.000 0.4192 0.01214 0.00393 -0.0876 0.4263 0.0772
-2.750 0.4383 0.01231 0.00397 -0.0859 0.4065 0.0795
-2.500 0.4580 0.01233 0.00394 -0.0843 0.3939 0.0832
-2.250 0.4789 0.01239 0.00394 -0.0830 0.3841 0.0874
-2.000 0.4997 0.01242 0.00396 -0.0816 0.3765 0.0948
-1.750 0.5213 0.01238 0.00409 -0.0804 0.3704 0.1371
-1.500 0.5426 0.01251 0.00420 -0.0792 0.3647 0.1598
-1.250 0.5619 0.01263 0.00431 -0.0775 0.3594 0.1734
-1.000 0.5835 0.01264 0.00436 -0.0763 0.3559 0.1858
-0.750 0.6039 0.01268 0.00443 -0.0749 0.3522 0.1992
-0.500 0.6234 0.01275 0.00453 -0.0734 0.3485 0.2155
-0.250 0.6420 0.01280 0.00467 -0.0718 0.3451 0.2546
0.000 0.6577 0.01267 0.00491 -0.0698 0.3412 0.4010
0.250 0.6674 0.01204 0.00515 -0.0664 0.3394 0.6818
0.500 0.8175 0.01216 0.00588 -0.0916 0.3332 1.0000
0.750 0.8300 0.01230 0.00598 -0.0888 0.3308 1.0000
1.000 0.8424 0.01248 0.00610 -0.0859 0.3284 1.0000
1.250 0.8563 0.01270 0.00627 -0.0833 0.3260 1.0000
1.500 0.8725 0.01300 0.00649 -0.0813 0.3232 1.0000
1.750 0.8907 0.01319 0.00666 -0.0796 0.3216 1.0000
2.000 0.9095 0.01335 0.00682 -0.0780 0.3202 1.0000
2.250 0.9286 0.01354 0.00700 -0.0766 0.3186 1.0000
2.500 0.9480 0.01374 0.00718 -0.0752 0.3168 1.0000
2.750 0.9676 0.01395 0.00738 -0.0739 0.3150 1.0000
3.000 0.9876 0.01418 0.00759 -0.0727 0.3133 1.0000
3.250 1.0077 0.01442 0.00781 -0.0715 0.3116 1.0000
3.500 1.0281 0.01469 0.00805 -0.0704 0.3100 1.0000
3.750 1.0489 0.01499 0.00831 -0.0695 0.3081 1.0000
4.000 1.0719 0.01536 0.00863 -0.0690 0.3057 1.0000
4.250 1.0946 0.01567 0.00892 -0.0684 0.3041 1.0000
4.500 1.1147 0.01589 0.00917 -0.0674 0.3030 1.0000
4.750 1.1353 0.01614 0.00944 -0.0665 0.3017 1.0000
5.000 1.1543 0.01637 0.00969 -0.0654 0.2996 1.0000
5.250 1.1736 0.01664 0.00997 -0.0643 0.2975 1.0000
5.500 1.1929 0.01691 0.01024 -0.0633 0.2954 1.0000
5.750 1.2132 0.01721 0.01054 -0.0625 0.2938 1.0000
6.000 1.2332 0.01753 0.01085 -0.0617 0.2919 1.0000
6.250 1.2547 0.01789 0.01118 -0.0612 0.2902 1.0000
6.500 1.2794 0.01834 0.01158 -0.0612 0.2872 1.0000
6.750 1.2969 0.01863 0.01193 -0.0601 0.2861 1.0000
7.000 1.3156 0.01896 0.01231 -0.0591 0.2849 1.0000
7.250 1.3344 0.01929 0.01269 -0.0583 0.2834 1.0000
7.500 1.3534 0.01965 0.01308 -0.0575 0.2819 1.0000
7.750 1.3722 0.02003 0.01349 -0.0568 0.2803 1.0000
8.000 1.3907 0.02041 0.01390 -0.0560 0.2786 1.0000
8.250 1.4094 0.02081 0.01432 -0.0553 0.2771 1.0000
8.500 1.4280 0.02123 0.01476 -0.0546 0.2757 1.0000
8.750 1.4463 0.02169 0.01521 -0.0539 0.2737 1.0000
9.000 1.4681 0.02214 0.01565 -0.0538 0.2715 1.0000
9.250 1.4866 0.02262 0.01617 -0.0532 0.2700 1.0000
9.500 1.5011 0.02314 0.01678 -0.0521 0.2686 1.0000
9.750 1.5161 0.02369 0.01740 -0.0512 0.2669 1.0000
10.000 1.5313 0.02425 0.01803 -0.0504 0.2650 1.0000
10.250 1.5471 0.02482 0.01865 -0.0497 0.2632 1.0000
10.500 1.5625 0.02543 0.01930 -0.0490 0.2615 1.0000
10.750 1.5771 0.02607 0.01998 -0.0482 0.2595 1.0000
11.000 1.5914 0.02678 0.02069 -0.0475 0.2572 1.0000
11.250 1.6078 0.02743 0.02135 -0.0470 0.2545 1.0000
11.500 1.6197 0.02828 0.02231 -0.0462 0.2529 1.0000
11.750 1.6325 0.02912 0.02325 -0.0456 0.2508 1.0000
12.000 1.6456 0.02998 0.02418 -0.0450 0.2487 1.0000
12.250 1.6577 0.03091 0.02519 -0.0444 0.2461 1.0000
12.500 1.6687 0.03196 0.02626 -0.0438 0.2433 1.0000
12.750 1.6790 0.03306 0.02735 -0.0432 0.2401 1.0000
13.000 1.6893 0.03425 0.02867 -0.0427 0.2371 1.0000
13.250 1.7007 0.03539 0.02991 -0.0423 0.2338 1.0000
13.500 1.7101 0.03671 0.03130 -0.0420 0.2302 1.0000
13.750 1.7168 0.03828 0.03288 -0.0415 0.2264 1.0000
14.000 1.7261 0.03971 0.03441 -0.0412 0.2218 1.0000
14.250 1.7327 0.04141 0.03618 -0.0409 0.2159 1.0000
14.500 1.7352 0.04350 0.03830 -0.0405 0.2095 1.0000
14.750 1.7352 0.04594 0.04077 -0.0402 0.1993 1.0000
15.000 1.7308 0.04884 0.04368 -0.0397 0.1869 1.0000
15.250 1.7138 0.05309 0.04788 -0.0391 0.1708 1.0000
15.500 1.6890 0.05829 0.05305 -0.0384 0.1535 1.0000
15.750 1.6558 0.06468 0.05943 -0.0380 0.1390 1.0000
16.000 1.6223 0.07141 0.06619 -0.0380 0.1290 1.0000
16.250 1.5886 0.07858 0.07343 -0.0385 0.1219 1.0000
16.500 1.5555 0.08595 0.08090 -0.0394 0.1165 1.0000
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Polar data table (+)
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