Rhode St. Genese 34 (rhodesg34-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: Rhode St. Genese 34 (rhodesg34-il) Reynolds number: 500,000 Max Cl/Cd: 81.93 at α=5.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-rhodesg34-il-500000-n5.txt Download as CSV file: xf-rhodesg34-il-500000-n5.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 = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-13.750 -0.4869 0.03687 0.03326 -0.1333 0.8800 0.0278
-13.500 -0.5299 0.03256 0.02852 -0.1303 0.8614 0.0279
-13.250 -0.5442 0.03012 0.02575 -0.1269 0.8506 0.0281
-13.000 -0.5480 0.02790 0.02323 -0.1242 0.8426 0.0284
-12.750 -0.5435 0.02615 0.02119 -0.1219 0.8359 0.0286
-12.500 -0.5340 0.02467 0.01946 -0.1199 0.8303 0.0288
-12.250 -0.5210 0.02341 0.01798 -0.1182 0.8255 0.0290
-12.000 -0.5051 0.02236 0.01673 -0.1167 0.8211 0.0291
-11.750 -0.4881 0.02133 0.01553 -0.1152 0.8170 0.0293
-11.500 -0.4693 0.02047 0.01457 -0.1139 0.8127 0.0295
-11.250 -0.4486 0.01981 0.01384 -0.1128 0.8086 0.0297
-11.000 -0.4271 0.01921 0.01316 -0.1117 0.8045 0.0299
-10.750 -0.4049 0.01868 0.01253 -0.1107 0.7999 0.0301
-10.500 -0.3823 0.01815 0.01192 -0.1097 0.7961 0.0304
-10.250 -0.3594 0.01761 0.01133 -0.1088 0.7917 0.0307
-10.000 -0.3361 0.01710 0.01074 -0.1079 0.7878 0.0310
-9.750 -0.3126 0.01659 0.01013 -0.1070 0.7837 0.0312
-9.500 -0.2888 0.01611 0.00955 -0.1061 0.7793 0.0316
-9.250 -0.2647 0.01563 0.00901 -0.1052 0.7743 0.0320
-9.000 -0.2405 0.01520 0.00848 -0.1044 0.7685 0.0324
-8.750 -0.2160 0.01481 0.00799 -0.1035 0.7624 0.0328
-8.500 -0.1912 0.01442 0.00753 -0.1027 0.7558 0.0332
-8.250 -0.1669 0.01397 0.00704 -0.1019 0.7494 0.0336
-8.000 -0.1421 0.01361 0.00666 -0.1011 0.7427 0.0340
-7.750 -0.1170 0.01330 0.00631 -0.1004 0.7342 0.0344
-7.500 -0.0918 0.01302 0.00600 -0.0996 0.7260 0.0349
-7.250 -0.0668 0.01274 0.00567 -0.0988 0.7139 0.0354
-7.000 -0.0421 0.01249 0.00535 -0.0979 0.6978 0.0359
-6.750 -0.0182 0.01228 0.00502 -0.0969 0.6788 0.0365
-6.500 0.0055 0.01211 0.00473 -0.0958 0.6579 0.0372
-6.250 0.0290 0.01199 0.00447 -0.0947 0.6374 0.0377
-6.000 0.0523 0.01184 0.00424 -0.0936 0.6186 0.0385
-5.750 0.0763 0.01177 0.00408 -0.0927 0.6007 0.0393
-5.500 0.1006 0.01172 0.00395 -0.0917 0.5828 0.0404
-5.250 0.1249 0.01165 0.00379 -0.0908 0.5640 0.0415
-5.000 0.1487 0.01162 0.00365 -0.0898 0.5392 0.0426
-4.750 0.1698 0.01166 0.00352 -0.0884 0.4946 0.0437
-4.500 0.1888 0.01190 0.00350 -0.0866 0.4372 0.0449
-4.250 0.2104 0.01204 0.00348 -0.0853 0.4053 0.0464
-4.000 0.2339 0.01210 0.00343 -0.0843 0.3867 0.0480
-3.750 0.2576 0.01211 0.00339 -0.0833 0.3735 0.0500
-3.500 0.2823 0.01211 0.00335 -0.0826 0.3638 0.0524
-3.000 0.3316 0.01210 0.00328 -0.0811 0.3499 0.0577
-2.750 0.3566 0.01211 0.00326 -0.0804 0.3444 0.0607
-2.500 0.3810 0.01211 0.00323 -0.0796 0.3394 0.0639
-2.250 0.4057 0.01213 0.00323 -0.0789 0.3351 0.0680
-2.000 0.4306 0.01209 0.00320 -0.0783 0.3318 0.0731
-1.750 0.4552 0.01207 0.00319 -0.0776 0.3280 0.0816
-1.500 0.4787 0.01197 0.00325 -0.0767 0.3242 0.1300
-1.250 0.5028 0.01203 0.00332 -0.0759 0.3206 0.1476
-1.000 0.5269 0.01211 0.00338 -0.0752 0.3172 0.1580
-0.750 0.5518 0.01211 0.00342 -0.0746 0.3148 0.1685
-0.500 0.5766 0.01214 0.00346 -0.0739 0.3118 0.1770
-0.250 0.6009 0.01217 0.00352 -0.0732 0.3094 0.1883
0.000 0.6245 0.01218 0.00360 -0.0724 0.3072 0.2114
0.250 0.6467 0.01207 0.00370 -0.0714 0.3054 0.2908
0.500 0.6629 0.01154 0.00384 -0.0695 0.3036 0.5340
1.000 0.8013 0.01119 0.00456 -0.0873 0.2984 0.9996
1.250 0.8240 0.01130 0.00466 -0.0863 0.2973 1.0000
1.500 0.8449 0.01142 0.00475 -0.0850 0.2959 1.0000
1.750 0.8658 0.01154 0.00486 -0.0837 0.2939 1.0000
2.000 0.8864 0.01167 0.00497 -0.0823 0.2913 1.0000
2.250 0.9067 0.01181 0.00509 -0.0809 0.2890 1.0000
2.500 0.9266 0.01198 0.00522 -0.0794 0.2866 1.0000
2.750 0.9462 0.01216 0.00536 -0.0779 0.2843 1.0000
3.000 0.9654 0.01235 0.00553 -0.0764 0.2824 1.0000
3.250 0.9853 0.01251 0.00569 -0.0749 0.2806 1.0000
3.500 1.0049 0.01263 0.00582 -0.0734 0.2786 1.0000
3.750 1.0236 0.01277 0.00597 -0.0718 0.2765 1.0000
4.000 1.0422 0.01293 0.00612 -0.0701 0.2735 1.0000
4.250 1.0604 0.01310 0.00630 -0.0685 0.2707 1.0000
4.500 1.0787 0.01331 0.00648 -0.0669 0.2683 1.0000
4.750 1.0968 0.01354 0.00670 -0.0653 0.2659 1.0000
5.000 1.1165 0.01373 0.00691 -0.0640 0.2640 1.0000
5.250 1.1369 0.01392 0.00712 -0.0629 0.2615 1.0000
5.500 1.1569 0.01412 0.00735 -0.0618 0.2582 1.0000
5.750 1.1760 0.01437 0.00759 -0.0605 0.2541 1.0000
6.000 1.1940 0.01466 0.00786 -0.0592 0.2490 1.0000
6.250 1.2141 0.01490 0.00813 -0.0582 0.2442 1.0000
6.500 1.2325 0.01521 0.00842 -0.0570 0.2375 1.0000
6.750 1.2507 0.01555 0.00876 -0.0558 0.2295 1.0000
7.000 1.2663 0.01602 0.00916 -0.0543 0.2131 1.0000
7.250 1.2589 0.01778 0.01048 -0.0500 0.1500 1.0000
7.500 1.2685 0.01871 0.01134 -0.0480 0.1359 1.0000
7.750 1.2817 0.01946 0.01208 -0.0466 0.1292 1.0000
8.000 1.2960 0.02016 0.01279 -0.0453 0.1238 1.0000
8.250 1.3091 0.02095 0.01357 -0.0440 0.1188 1.0000
8.500 1.3231 0.02170 0.01433 -0.0428 0.1147 1.0000
8.750 1.3369 0.02248 0.01514 -0.0417 0.1104 1.0000
9.000 1.3492 0.02338 0.01605 -0.0406 0.1063 1.0000
9.250 1.3625 0.02423 0.01692 -0.0395 0.1026 1.0000
9.500 1.3752 0.02513 0.01784 -0.0385 0.0973 1.0000
9.750 1.3861 0.02619 0.01892 -0.0374 0.0916 1.0000
10.250 1.3879 0.02985 0.02241 -0.0340 0.0585 1.0000
10.500 1.3933 0.03142 0.02402 -0.0328 0.0558 1.0000
10.750 1.4000 0.03295 0.02560 -0.0318 0.0543 1.0000
11.000 1.4067 0.03452 0.02724 -0.0309 0.0533 1.0000
11.250 1.4120 0.03627 0.02906 -0.0301 0.0523 1.0000
11.500 1.4161 0.03819 0.03105 -0.0294 0.0514 1.0000
11.750 1.4185 0.04036 0.03330 -0.0288 0.0507 1.0000
12.000 1.4192 0.04280 0.03581 -0.0282 0.0499 1.0000
12.250 1.4179 0.04554 0.03864 -0.0278 0.0492 1.0000
12.500 1.4159 0.04846 0.04165 -0.0276 0.0486 1.0000
12.750 1.4176 0.05107 0.04435 -0.0276 0.0479 1.0000
13.000 1.4169 0.05401 0.04739 -0.0276 0.0473 1.0000
13.250 1.4137 0.05731 0.05079 -0.0278 0.0465 1.0000
13.500 1.4083 0.06096 0.05454 -0.0281 0.0460 1.0000
13.750 1.4009 0.06498 0.05867 -0.0286 0.0454 1.0000
14.000 1.3914 0.06939 0.06318 -0.0293 0.0449 1.0000
14.250 1.3801 0.07414 0.06804 -0.0301 0.0445 1.0000
14.500 1.3690 0.07895 0.07296 -0.0311 0.0442 1.0000
14.750 1.3557 0.08413 0.07824 -0.0322 0.0437 1.0000
15.000 1.3436 0.08913 0.08333 -0.0333 0.0433 1.0000
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