Rhode St. Genese 32 (rhodesg32-il) Xfoil prediction polar at RE=100,000 Ncrit=9
| Details | Polar file |
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Airfoil: Rhode St. Genese 32 (rhodesg32-il) Reynolds number: 100,000 Max Cl/Cd: 45.24 at α=3.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-rhodesg32-il-100000.txt Download as CSV file: xf-rhodesg32-il-100000.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 = 0.100 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-10.750 -0.3100 0.10110 0.09611 -0.0353 1.0000 0.1264
-10.500 -0.3416 0.10080 0.09598 -0.0364 1.0000 0.1298
-10.250 -0.3811 0.10096 0.09632 -0.0350 1.0000 0.1303
-10.000 -0.3544 0.09554 0.09089 -0.0323 1.0000 0.1328
-9.750 -0.3464 0.09325 0.08862 -0.0292 1.0000 0.1355
-9.500 -0.3562 0.09185 0.08730 -0.0264 1.0000 0.1382
-9.250 -0.3756 0.09080 0.08635 -0.0236 1.0000 0.1406
-9.000 -0.4041 0.09010 0.08576 -0.0204 1.0000 0.1423
-8.750 -0.4437 0.08910 0.08486 -0.0212 1.0000 0.1446
-8.500 -0.4789 0.08625 0.08198 -0.0252 1.0000 0.1464
-8.250 -0.4645 0.08332 0.07917 -0.0193 1.0000 0.1481
-8.000 -0.4561 0.08149 0.07738 -0.0157 0.9995 0.1516
-7.750 -0.4336 0.07530 0.07100 -0.0296 0.9888 0.1634
-7.500 -0.4002 0.07220 0.06793 -0.0299 0.9834 0.1685
-7.250 -0.3778 0.06710 0.06262 -0.0391 0.9730 0.1803
-7.000 -0.3483 0.06421 0.05975 -0.0403 0.9660 0.1869
-6.750 -0.3202 0.06022 0.05563 -0.0456 0.9576 0.1999
-6.500 -0.2970 0.05688 0.05211 -0.0496 0.9476 0.2144
-6.250 -0.2607 0.05358 0.04865 -0.0545 0.9411 0.2308
-6.000 -0.2386 0.05119 0.04629 -0.0541 0.9313 0.2377
-5.750 -0.2017 0.04833 0.04325 -0.0585 0.9252 0.2658
-5.500 -0.1626 0.03574 0.02848 -0.0658 0.9152 0.1280
-5.250 -0.1178 0.03270 0.02502 -0.0690 0.9096 0.1243
-5.000 -0.0882 0.03094 0.02293 -0.0692 0.8987 0.1245
-4.750 -0.0366 0.02864 0.02021 -0.0729 0.8932 0.1240
-4.500 -0.0056 0.02726 0.01855 -0.0730 0.8823 0.1243
-4.250 0.0445 0.02578 0.01679 -0.0763 0.8775 0.1274
-4.000 0.0752 0.02499 0.01577 -0.0762 0.8675 0.1303
-3.750 0.1190 0.02354 0.01434 -0.0784 0.8614 0.1337
-3.500 0.1498 0.02274 0.01355 -0.0783 0.8513 0.1378
-3.250 0.1922 0.02181 0.01251 -0.0799 0.8440 0.1456
-3.000 0.2196 0.02096 0.01184 -0.0792 0.8321 0.1536
-2.750 0.2559 0.01992 0.01086 -0.0797 0.8228 0.1654
-2.500 0.2862 0.01894 0.01003 -0.0791 0.8108 0.1860
-2.250 0.4107 0.01502 0.00877 -0.0954 0.7990 1.0000
-2.000 0.4350 0.01472 0.00824 -0.0938 0.7806 1.0000
-1.750 0.4606 0.01439 0.00768 -0.0924 0.7603 1.0000
-1.500 0.4811 0.01420 0.00731 -0.0902 0.7327 1.0000
-1.250 0.5040 0.01401 0.00688 -0.0883 0.6996 1.0000
-1.000 0.5265 0.01397 0.00650 -0.0865 0.6591 1.0000
-0.750 0.5472 0.01415 0.00630 -0.0845 0.6158 1.0000
-0.500 0.5682 0.01446 0.00625 -0.0829 0.5812 1.0000
-0.250 0.5898 0.01481 0.00633 -0.0815 0.5555 1.0000
0.000 0.6123 0.01516 0.00644 -0.0804 0.5374 1.0000
0.250 0.6355 0.01551 0.00658 -0.0794 0.5237 1.0000
0.500 0.6597 0.01587 0.00673 -0.0787 0.5133 1.0000
0.750 0.6833 0.01623 0.00699 -0.0780 0.5037 1.0000
1.000 0.7086 0.01662 0.00721 -0.0775 0.4968 1.0000
1.250 0.7329 0.01701 0.00756 -0.0769 0.4902 1.0000
1.500 0.7584 0.01741 0.00787 -0.0765 0.4850 1.0000
1.750 0.7847 0.01786 0.00821 -0.0763 0.4809 1.0000
2.000 0.8089 0.01830 0.00868 -0.0758 0.4765 1.0000
2.250 0.8340 0.01876 0.00915 -0.0755 0.4727 1.0000
2.500 0.8598 0.01923 0.00957 -0.0752 0.4690 1.0000
2.750 0.8868 0.01975 0.00998 -0.0752 0.4654 1.0000
3.000 0.9089 0.02023 0.01058 -0.0744 0.4609 1.0000
3.250 0.9324 0.02071 0.01110 -0.0738 0.4562 1.0000
3.500 0.9582 0.02118 0.01151 -0.0735 0.4516 1.0000
3.750 0.9826 0.02173 0.01209 -0.0731 0.4474 1.0000
4.000 1.0041 0.02227 0.01275 -0.0723 0.4429 1.0000
4.250 1.0278 0.02282 0.01336 -0.0718 0.4390 1.0000
4.500 1.0531 0.02340 0.01398 -0.0716 0.4360 1.0000
4.750 1.0797 0.02407 0.01465 -0.0716 0.4336 1.0000
5.000 1.1004 0.02479 0.01554 -0.0708 0.4307 1.0000
5.250 1.1204 0.02549 0.01644 -0.0698 0.4270 1.0000
5.500 1.1424 0.02619 0.01726 -0.0692 0.4235 1.0000
5.750 1.1682 0.02674 0.01781 -0.0690 0.4188 1.0000
6.000 1.1875 0.02741 0.01862 -0.0679 0.4128 1.0000
6.250 1.2086 0.02785 0.01915 -0.0669 0.4051 1.0000
6.500 1.2319 0.02835 0.01965 -0.0664 0.3975 1.0000
6.750 1.2503 0.02879 0.02022 -0.0650 0.3892 1.0000
7.000 1.2746 0.02923 0.02067 -0.0646 0.3815 1.0000
7.250 1.2909 0.02972 0.02133 -0.0629 0.3732 1.0000
7.500 1.3167 0.03013 0.02172 -0.0628 0.3655 1.0000
7.750 1.3298 0.03067 0.02251 -0.0607 0.3572 1.0000
8.000 1.3540 0.03093 0.02275 -0.0602 0.3481 1.0000
8.250 1.3683 0.03118 0.02315 -0.0581 0.3377 1.0000
8.500 1.3829 0.03148 0.02359 -0.0562 0.3274 1.0000
8.750 1.4043 0.03134 0.02340 -0.0551 0.3157 1.0000
9.000 1.4097 0.03145 0.02373 -0.0517 0.3038 1.0000
9.250 1.4140 0.03156 0.02402 -0.0482 0.2915 1.0000
9.500 1.4159 0.03152 0.02412 -0.0442 0.2783 1.0000
9.750 1.4095 0.03158 0.02433 -0.0390 0.2643 1.0000
10.000 1.3992 0.03203 0.02499 -0.0338 0.2463 1.0000
10.250 1.3888 0.03278 0.02584 -0.0293 0.2176 1.0000
10.500 1.3734 0.03424 0.02700 -0.0252 0.1889 1.0000
10.750 1.3522 0.03703 0.02946 -0.0217 0.1715 1.0000
11.000 1.3302 0.04057 0.03280 -0.0189 0.1578 1.0000
11.250 1.3119 0.04426 0.03640 -0.0169 0.1456 1.0000
11.500 1.2980 0.04790 0.04004 -0.0155 0.1341 1.0000
11.750 1.2888 0.05126 0.04337 -0.0145 0.1243 1.0000
12.000 1.2859 0.05405 0.04600 -0.0135 0.1159 1.0000
12.250 1.2813 0.05725 0.04937 -0.0132 0.1089 1.0000
12.500 1.2848 0.05954 0.05153 -0.0125 0.1025 1.0000
12.750 1.2825 0.06268 0.05486 -0.0125 0.0973 1.0000
13.000 1.2864 0.06502 0.05712 -0.0122 0.0924 1.0000
13.250 1.2887 0.06781 0.06004 -0.0120 0.0880 1.0000
13.500 1.2904 0.07062 0.06295 -0.0121 0.0841 1.0000
13.750 1.3018 0.07223 0.06441 -0.0115 0.0800 1.0000
14.000 1.3006 0.07569 0.06812 -0.0118 0.0773 1.0000
14.250 1.3015 0.07882 0.07138 -0.0121 0.0744 1.0000
14.500 1.3167 0.08012 0.07254 -0.0115 0.0711 1.0000
14.750 1.3182 0.08350 0.07609 -0.0117 0.0690 1.0000
15.000 1.3124 0.08784 0.08069 -0.0126 0.0676 1.0000
15.250 1.3057 0.09238 0.08546 -0.0137 0.0663 1.0000
15.500 1.2972 0.09723 0.09051 -0.0153 0.0652 1.0000
15.750 1.2884 0.10218 0.09563 -0.0170 0.0641 1.0000
16.000 1.2844 0.10647 0.10003 -0.0184 0.0628 1.0000
16.250 1.2928 0.10942 0.10295 -0.0184 0.0609 1.0000
16.500 1.2677 0.11710 0.11091 -0.0223 0.0609 1.0000
16.750 1.2423 0.12536 0.11940 -0.0268 0.0609 1.0000
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Polar data table (+)
Polar graphs
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