Rhode St. Genese 34 (rhodesg34-il) Xfoil prediction polar at RE=200,000 Ncrit=9
| Details | Polar file |
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Airfoil: Rhode St. Genese 34 (rhodesg34-il) Reynolds number: 200,000 Max Cl/Cd: 58.84 at α=7° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-rhodesg34-il-200000.txt Download as CSV file: xf-rhodesg34-il-200000.csv |
XFOIL Version 6.96
Calculated polar for: Rhode St. Genese 34
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.200 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-11.000 -0.1734 0.09201 0.08846 -0.0656 0.9708 0.0725
-10.750 -0.1571 0.08846 0.08491 -0.0694 0.9659 0.0745
-10.500 -0.1754 0.07950 0.07596 -0.0889 0.9559 0.0788
-10.250 -0.1410 0.07735 0.07380 -0.0864 0.9549 0.0797
-10.000 -0.1193 0.07506 0.07150 -0.0868 0.9490 0.0808
-9.750 -0.0971 0.07180 0.06823 -0.0907 0.9438 0.0830
-9.500 -0.1271 0.06184 0.05805 -0.1094 0.9275 0.0890
-9.250 -0.0916 0.06033 0.05663 -0.1084 0.9246 0.0902
-9.000 -0.0711 0.05882 0.05511 -0.1079 0.9174 0.0921
-8.750 -0.0831 0.05254 0.04846 -0.1151 0.9061 0.1002
-8.500 -0.0660 0.05107 0.04707 -0.1133 0.8972 0.1012
-8.250 -0.0438 0.04939 0.04537 -0.1133 0.8906 0.1034
-8.000 -0.0497 0.04603 0.04164 -0.1136 0.8798 0.1123
-7.750 -0.0268 0.04429 0.03996 -0.1131 0.8733 0.1139
-7.500 -0.0098 0.04287 0.03850 -0.1121 0.8657 0.1172
-7.250 -0.0331 0.02949 0.02347 -0.1092 0.8560 0.0767
-7.000 -0.0145 0.02703 0.02071 -0.1079 0.8492 0.0748
-6.750 -0.0011 0.02409 0.01702 -0.1052 0.8405 0.0710
-6.500 0.0255 0.02269 0.01524 -0.1045 0.8347 0.0706
-6.250 0.0461 0.02163 0.01404 -0.1029 0.8257 0.0709
-6.000 0.0728 0.02056 0.01281 -0.1023 0.8183 0.0717
-5.750 0.0967 0.01981 0.01201 -0.1012 0.8094 0.0733
-5.500 0.1228 0.01907 0.01115 -0.1004 0.8012 0.0753
-5.250 0.1483 0.01841 0.01035 -0.0994 0.7933 0.0769
-5.000 0.1736 0.01783 0.00964 -0.0984 0.7847 0.0782
-4.750 0.2003 0.01686 0.00867 -0.0978 0.7775 0.0803
-4.500 0.2234 0.01627 0.00814 -0.0966 0.7677 0.0830
-4.250 0.2499 0.01576 0.00758 -0.0959 0.7598 0.0870
-4.000 0.2722 0.01516 0.00703 -0.0945 0.7491 0.0907
-3.750 0.2961 0.01467 0.00658 -0.0933 0.7389 0.0956
-3.500 0.3204 0.01419 0.00612 -0.0922 0.7277 0.1022
-3.250 0.3433 0.01386 0.00584 -0.0909 0.7133 0.1120
-3.000 0.3671 0.01353 0.00559 -0.0896 0.6972 0.1277
-2.750 0.3905 0.01315 0.00527 -0.0883 0.6783 0.1637
-2.500 0.4120 0.01272 0.00493 -0.0868 0.6549 0.2160
-2.250 0.4325 0.01244 0.00471 -0.0851 0.6256 0.2742
-2.000 0.4477 0.01200 0.00462 -0.0826 0.5908 0.4167
-1.750 0.4548 0.01111 0.00479 -0.0778 0.5517 0.7719
-1.500 0.5662 0.01181 0.00509 -0.0941 0.4726 0.9859
-1.250 0.6100 0.01228 0.00518 -0.0976 0.4500 1.0000
-1.000 0.6276 0.01256 0.00528 -0.0957 0.4387 1.0000
-0.750 0.6455 0.01289 0.00540 -0.0939 0.4304 1.0000
-0.500 0.6656 0.01312 0.00553 -0.0924 0.4233 1.0000
-0.250 0.6859 0.01341 0.00567 -0.0910 0.4175 1.0000
0.000 0.7075 0.01375 0.00584 -0.0899 0.4126 1.0000
0.250 0.7295 0.01398 0.00602 -0.0888 0.4082 1.0000
0.500 0.7517 0.01423 0.00620 -0.0877 0.4040 1.0000
0.750 0.7743 0.01453 0.00639 -0.0868 0.3999 1.0000
1.000 0.7988 0.01494 0.00663 -0.0863 0.3958 1.0000
1.250 0.8210 0.01517 0.00685 -0.0853 0.3923 1.0000
1.500 0.8440 0.01542 0.00709 -0.0844 0.3891 1.0000
1.750 0.8672 0.01570 0.00733 -0.0837 0.3857 1.0000
2.000 0.8909 0.01601 0.00757 -0.0830 0.3824 1.0000
2.250 0.9161 0.01639 0.00786 -0.0827 0.3795 1.0000
2.500 0.9423 0.01682 0.00822 -0.0826 0.3770 1.0000
2.750 0.9652 0.01710 0.00853 -0.0818 0.3749 1.0000
3.000 0.9889 0.01740 0.00886 -0.0811 0.3729 1.0000
3.250 1.0129 0.01773 0.00921 -0.0806 0.3709 1.0000
3.500 1.0370 0.01806 0.00955 -0.0801 0.3686 1.0000
3.750 1.0611 0.01840 0.00988 -0.0797 0.3661 1.0000
4.000 1.0859 0.01877 0.01019 -0.0793 0.3628 1.0000
4.250 1.1140 0.01937 0.01070 -0.0798 0.3596 1.0000
4.500 1.1333 0.01959 0.01102 -0.0784 0.3570 1.0000
4.750 1.1543 0.01988 0.01139 -0.0774 0.3541 1.0000
5.000 1.1758 0.02018 0.01173 -0.0765 0.3508 1.0000
5.250 1.1987 0.02049 0.01203 -0.0759 0.3475 1.0000
5.500 1.2237 0.02087 0.01238 -0.0757 0.3445 1.0000
5.750 1.2501 0.02144 0.01292 -0.0759 0.3414 1.0000
6.000 1.2674 0.02169 0.01330 -0.0743 0.3387 1.0000
6.250 1.2869 0.02201 0.01372 -0.0732 0.3358 1.0000
6.500 1.3074 0.02233 0.01411 -0.0723 0.3329 1.0000
6.750 1.3290 0.02264 0.01443 -0.0715 0.3296 1.0000
7.000 1.3534 0.02300 0.01477 -0.0713 0.3267 1.0000
7.250 1.3784 0.02355 0.01532 -0.0714 0.3235 1.0000
7.500 1.3921 0.02383 0.01577 -0.0693 0.3208 1.0000
7.750 1.4063 0.02409 0.01615 -0.0673 0.3169 1.0000
8.000 1.4232 0.02432 0.01644 -0.0658 0.3130 1.0000
8.250 1.4442 0.02460 0.01671 -0.0651 0.3097 1.0000
8.500 1.4660 0.02503 0.01714 -0.0646 0.3060 1.0000
8.750 1.4710 0.02530 0.01760 -0.0611 0.3024 1.0000
9.000 1.4783 0.02556 0.01797 -0.0580 0.2984 1.0000
9.250 1.4895 0.02578 0.01824 -0.0556 0.2945 1.0000
9.500 1.5069 0.02603 0.01844 -0.0544 0.2905 1.0000
9.750 1.5092 0.02648 0.01908 -0.0508 0.2868 1.0000
10.000 1.5135 0.02695 0.01970 -0.0478 0.2825 1.0000
10.250 1.5206 0.02734 0.02018 -0.0454 0.2780 1.0000
10.500 1.5331 0.02771 0.02050 -0.0438 0.2737 1.0000
10.750 1.5322 0.02854 0.02158 -0.0407 0.2687 1.0000
11.000 1.5356 0.02928 0.02246 -0.0384 0.2630 1.0000
11.250 1.5411 0.03000 0.02321 -0.0364 0.2575 1.0000
11.500 1.5422 0.03113 0.02456 -0.0344 0.2491 1.0000
11.750 1.5449 0.03224 0.02576 -0.0326 0.2409 1.0000
12.000 1.5464 0.03359 0.02721 -0.0309 0.2299 1.0000
12.250 1.5459 0.03522 0.02891 -0.0294 0.2127 1.0000
12.500 1.5369 0.03756 0.03117 -0.0275 0.1908 1.0000
12.750 1.5197 0.04090 0.03440 -0.0257 0.1739 1.0000
13.000 1.5014 0.04475 0.03818 -0.0244 0.1621 1.0000
13.250 1.4856 0.04872 0.04216 -0.0236 0.1531 1.0000
13.500 1.4700 0.05293 0.04642 -0.0232 0.1457 1.0000
13.750 1.4521 0.05767 0.05119 -0.0231 0.1390 1.0000
14.000 1.4374 0.06225 0.05585 -0.0233 0.1329 1.0000
14.250 1.4184 0.06756 0.06121 -0.0239 0.1267 1.0000
14.500 1.4021 0.07275 0.06648 -0.0248 0.1211 1.0000
14.750 1.3852 0.07821 0.07201 -0.0259 0.1152 1.0000
15.000 1.3692 0.08364 0.07748 -0.0271 0.1098 1.0000
15.250 1.3554 0.08895 0.08286 -0.0285 0.1036 1.0000
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Polar data table (+)
Polar graphs
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