Rhode St. Genese 32 (rhodesg32-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: Rhode St. Genese 32 (rhodesg32-il) Reynolds number: 1,000,000 Max Cl/Cd: 107.96 at α=4.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-rhodesg32-il-1000000-n5.txt Download as CSV file: xf-rhodesg32-il-1000000-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 = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-17.750 -1.1643 0.03198 0.02894 -0.1074 1.0000 0.0157
-17.500 -1.1782 0.03005 0.02688 -0.1039 1.0000 0.0160
-17.250 -1.1819 0.02847 0.02518 -0.1009 1.0000 0.0164
-17.000 -1.1794 0.02707 0.02367 -0.0983 1.0000 0.0168
-16.750 -1.1751 0.02575 0.02227 -0.0956 1.0000 0.0175
-16.500 -1.1677 0.02466 0.02110 -0.0931 1.0000 0.0181
-16.250 -1.1457 0.02352 0.01986 -0.0932 0.9986 0.0192
-16.000 -1.1201 0.02247 0.01870 -0.0938 0.9954 0.0200
-15.750 -1.0952 0.02164 0.01782 -0.0940 0.9910 0.0209
-15.500 -1.0688 0.02091 0.01704 -0.0942 0.9866 0.0218
-15.250 -1.0408 0.02019 0.01625 -0.0948 0.9831 0.0227
-15.000 -1.0151 0.01948 0.01543 -0.0948 0.9771 0.0233
-14.750 -0.9848 0.01881 0.01468 -0.0956 0.9731 0.0239
-14.500 -0.9520 0.01831 0.01415 -0.0968 0.9682 0.0246
-14.250 -0.9162 0.01785 0.01366 -0.0985 0.9615 0.0253
-14.000 -0.8782 0.01740 0.01313 -0.1007 0.9520 0.0262
-13.750 -0.8429 0.01687 0.01249 -0.1023 0.9397 0.0269
-13.250 -0.7889 0.01598 0.01136 -0.1021 0.9172 0.0278
-13.000 -0.7646 0.01562 0.01093 -0.1014 0.9069 0.0283
-12.750 -0.7394 0.01542 0.01070 -0.1007 0.8987 0.0288
-12.500 -0.7142 0.01524 0.01047 -0.1000 0.8923 0.0293
-12.250 -0.6894 0.01499 0.01016 -0.0993 0.8860 0.0298
-11.750 -0.6394 0.01449 0.00953 -0.0979 0.8741 0.0308
-11.500 -0.6144 0.01425 0.00922 -0.0971 0.8669 0.0314
-11.250 -0.5894 0.01399 0.00888 -0.0964 0.8593 0.0318
-11.000 -0.5640 0.01378 0.00858 -0.0957 0.8519 0.0321
-10.750 -0.5401 0.01334 0.00808 -0.0948 0.8455 0.0327
-10.500 -0.5150 0.01304 0.00774 -0.0941 0.8385 0.0331
-10.250 -0.4898 0.01280 0.00743 -0.0934 0.8312 0.0335
-10.000 -0.4640 0.01256 0.00715 -0.0928 0.8233 0.0338
-9.750 -0.4383 0.01239 0.00693 -0.0921 0.8136 0.0343
-9.500 -0.4126 0.01218 0.00666 -0.0915 0.8032 0.0347
-9.250 -0.3871 0.01195 0.00636 -0.0908 0.7923 0.0351
-9.000 -0.3620 0.01172 0.00603 -0.0900 0.7781 0.0355
-8.750 -0.3370 0.01150 0.00572 -0.0892 0.7623 0.0359
-8.500 -0.3120 0.01129 0.00541 -0.0885 0.7454 0.0363
-8.250 -0.2869 0.01112 0.00513 -0.0877 0.7265 0.0366
-8.000 -0.2616 0.01095 0.00486 -0.0869 0.7096 0.0369
-7.750 -0.2361 0.01083 0.00464 -0.0863 0.6922 0.0372
-7.500 -0.2111 0.01065 0.00437 -0.0855 0.6731 0.0376
-7.250 -0.1867 0.01044 0.00406 -0.0846 0.6524 0.0382
-7.000 -0.1614 0.01033 0.00386 -0.0839 0.6332 0.0387
-6.750 -0.1357 0.01022 0.00368 -0.0833 0.6163 0.0392
-6.500 -0.1099 0.01014 0.00352 -0.0827 0.5973 0.0396
-6.250 -0.0845 0.01010 0.00338 -0.0820 0.5727 0.0401
-6.000 -0.0595 0.01009 0.00325 -0.0813 0.5410 0.0407
-5.750 -0.0400 0.01048 0.00320 -0.0796 0.4303 0.0411
-5.500 -0.0171 0.01067 0.00314 -0.0785 0.3720 0.0417
-5.250 0.0085 0.01065 0.00303 -0.0779 0.3524 0.0422
-4.750 0.0613 0.01059 0.00286 -0.0770 0.3336 0.0433
-4.500 0.0880 0.01054 0.00276 -0.0766 0.3280 0.0436
-4.000 0.1406 0.01031 0.00248 -0.0757 0.3194 0.0454
-3.750 0.1674 0.01025 0.00241 -0.0754 0.3166 0.0462
-3.500 0.1942 0.01020 0.00235 -0.0750 0.3138 0.0470
-3.250 0.2210 0.01016 0.00229 -0.0746 0.3110 0.0479
-3.000 0.2477 0.01013 0.00225 -0.0743 0.3084 0.0488
-2.750 0.2745 0.01012 0.00222 -0.0739 0.3056 0.0497
-2.500 0.3013 0.01011 0.00219 -0.0736 0.3036 0.0506
-2.250 0.3284 0.01009 0.00217 -0.0733 0.3024 0.0511
-2.000 0.3551 0.01003 0.00211 -0.0730 0.3012 0.0525
-1.750 0.3819 0.01000 0.00208 -0.0727 0.2995 0.0542
-1.500 0.4087 0.00998 0.00207 -0.0724 0.2972 0.0558
-1.250 0.4353 0.00999 0.00207 -0.0721 0.2945 0.0574
-1.000 0.4619 0.01000 0.00208 -0.0718 0.2922 0.0593
-0.750 0.4884 0.01003 0.00210 -0.0714 0.2897 0.0608
-0.500 0.5147 0.01005 0.00212 -0.0711 0.2875 0.0652
-0.250 0.5414 0.01005 0.00215 -0.0708 0.2864 0.0704
0.000 0.5673 0.00994 0.00218 -0.0704 0.2851 0.1220
0.250 0.5938 0.00993 0.00224 -0.0702 0.2839 0.1450
0.500 0.6203 0.00994 0.00229 -0.0699 0.2828 0.1576
0.750 0.6467 0.00996 0.00234 -0.0696 0.2813 0.1706
1.000 0.6728 0.00995 0.00240 -0.0693 0.2795 0.1962
1.250 0.6880 0.00894 0.00255 -0.0673 0.2780 0.6413
1.500 0.7011 0.00834 0.00269 -0.0640 0.2768 0.8860
1.750 0.7837 0.00848 0.00292 -0.0761 0.2740 0.9841
2.000 0.8257 0.00864 0.00306 -0.0794 0.2718 0.9978
2.250 0.8597 0.00874 0.00314 -0.0808 0.2696 1.0000
2.500 0.8836 0.00882 0.00322 -0.0801 0.2668 1.0000
2.750 0.9072 0.00892 0.00331 -0.0793 0.2638 1.0000
3.000 0.9306 0.00903 0.00340 -0.0784 0.2606 1.0000
3.250 0.9536 0.00917 0.00350 -0.0776 0.2566 1.0000
3.500 0.9775 0.00927 0.00361 -0.0768 0.2534 1.0000
3.750 1.0011 0.00939 0.00372 -0.0761 0.2492 1.0000
4.000 1.0240 0.00955 0.00383 -0.0752 0.2425 1.0000
4.250 1.0472 0.00970 0.00396 -0.0745 0.2343 1.0000
4.500 1.0575 0.01057 0.00444 -0.0715 0.1653 1.0000
4.750 1.0750 0.01105 0.00482 -0.0698 0.1463 1.0000
5.250 1.1160 0.01166 0.00537 -0.0674 0.1300 1.0000
5.500 1.1368 0.01194 0.00562 -0.0663 0.1246 1.0000
5.750 1.1576 0.01222 0.00588 -0.0652 0.1193 1.0000
6.000 1.1787 0.01246 0.00613 -0.0641 0.1150 1.0000
6.250 1.1991 0.01275 0.00640 -0.0630 0.1105 1.0000
6.500 1.2189 0.01305 0.00668 -0.0618 0.1053 1.0000
6.750 1.2392 0.01330 0.00694 -0.0607 0.1017 1.0000
7.250 1.2635 0.01446 0.00785 -0.0556 0.0613 1.0000
7.500 1.2766 0.01499 0.00834 -0.0534 0.0527 1.0000
7.750 1.2920 0.01543 0.00879 -0.0515 0.0491 1.0000
8.000 1.3068 0.01591 0.00928 -0.0497 0.0456 1.0000
8.250 1.3234 0.01632 0.00971 -0.0482 0.0437 1.0000
8.500 1.3400 0.01674 0.01015 -0.0467 0.0423 1.0000
8.750 1.3558 0.01721 0.01064 -0.0452 0.0407 1.0000
9.000 1.3703 0.01777 0.01122 -0.0436 0.0387 1.0000
9.250 1.3846 0.01835 0.01182 -0.0421 0.0370 1.0000
9.500 1.4004 0.01886 0.01237 -0.0408 0.0362 1.0000
9.750 1.4154 0.01943 0.01297 -0.0395 0.0349 1.0000
10.000 1.4296 0.02008 0.01365 -0.0382 0.0335 1.0000
10.250 1.4424 0.02082 0.01441 -0.0368 0.0322 1.0000
10.500 1.4547 0.02162 0.01524 -0.0355 0.0309 1.0000
10.750 1.4684 0.02236 0.01602 -0.0343 0.0296 1.0000
11.000 1.4809 0.02321 0.01690 -0.0332 0.0285 1.0000
11.250 1.4916 0.02419 0.01791 -0.0320 0.0269 1.0000
11.500 1.5019 0.02526 0.01901 -0.0308 0.0256 1.0000
11.750 1.5126 0.02631 0.02012 -0.0298 0.0245 1.0000
12.000 1.5217 0.02754 0.02138 -0.0287 0.0229 1.0000
12.250 1.5293 0.02893 0.02279 -0.0277 0.0215 1.0000
12.500 1.5367 0.03037 0.02429 -0.0268 0.0200 1.0000
12.750 1.5425 0.03201 0.02597 -0.0260 0.0187 1.0000
13.000 1.5469 0.03385 0.02786 -0.0252 0.0175 1.0000
13.250 1.5508 0.03579 0.02985 -0.0246 0.0164 1.0000
13.500 1.5528 0.03800 0.03212 -0.0241 0.0154 1.0000
13.750 1.5532 0.04047 0.03465 -0.0237 0.0146 1.0000
14.000 1.5540 0.04299 0.03725 -0.0235 0.0141 1.0000
14.250 1.5531 0.04578 0.04013 -0.0234 0.0134 1.0000
14.500 1.5500 0.04893 0.04336 -0.0235 0.0129 1.0000
14.750 1.5458 0.05232 0.04682 -0.0238 0.0125 1.0000
15.000 1.5396 0.05602 0.05062 -0.0242 0.0121 1.0000
15.250 1.5309 0.06017 0.05486 -0.0249 0.0118 1.0000
15.500 1.5234 0.06428 0.05907 -0.0257 0.0115 1.0000
15.750 1.5142 0.06871 0.06359 -0.0266 0.0112 1.0000
16.000 1.5038 0.07338 0.06837 -0.0277 0.0111 1.0000
16.250 1.4924 0.07828 0.07337 -0.0289 0.0107 1.0000
16.500 1.4811 0.08318 0.07836 -0.0302 0.0106 1.0000
16.750 1.4694 0.08812 0.08339 -0.0315 0.0103 1.0000
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Polar data table (+)
Polar graphs
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