Rhode St. Genese 34 (rhodesg34-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: Rhode St. Genese 34 (rhodesg34-il) Reynolds number: 1,000,000 Max Cl/Cd: 103.64 at α=4.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-rhodesg34-il-1000000-n5.txt Download as CSV file: xf-rhodesg34-il-1000000-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 = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.500 -0.4110 0.17882 0.17688 -0.0211 1.0000 0.0138
-19.250 -0.4024 0.17639 0.17445 -0.0223 1.0000 0.0140
-16.750 -0.8722 0.03375 0.03065 -0.1255 0.9515 0.0234
-16.500 -0.8274 0.02952 0.02613 -0.1380 0.9310 0.0235
-16.250 -0.7985 0.02739 0.02367 -0.1430 0.8847 0.0237
-16.000 -0.8021 0.02622 0.02228 -0.1399 0.8589 0.0238
-15.750 -0.8058 0.02514 0.02103 -0.1361 0.8467 0.0238
-15.500 -0.8038 0.02433 0.02010 -0.1327 0.8384 0.0240
-15.250 -0.7953 0.02348 0.01912 -0.1303 0.8324 0.0241
-15.000 -0.7843 0.02261 0.01815 -0.1281 0.8278 0.0242
-14.750 -0.7712 0.02179 0.01722 -0.1262 0.8237 0.0243
-14.500 -0.7557 0.02110 0.01642 -0.1244 0.8201 0.0244
-14.250 -0.7386 0.02047 0.01569 -0.1228 0.8166 0.0246
-14.000 -0.7208 0.01981 0.01493 -0.1213 0.8136 0.0248
-13.750 -0.7023 0.01916 0.01420 -0.1199 0.8097 0.0249
-13.500 -0.6828 0.01857 0.01351 -0.1185 0.8058 0.0250
-13.250 -0.6630 0.01803 0.01286 -0.1171 0.8007 0.0251
-13.000 -0.6424 0.01750 0.01223 -0.1159 0.7971 0.0252
-12.750 -0.6206 0.01698 0.01164 -0.1148 0.7947 0.0253
-12.500 -0.5983 0.01650 0.01109 -0.1137 0.7918 0.0254
-12.250 -0.5770 0.01591 0.01043 -0.1125 0.7883 0.0255
-12.000 -0.5555 0.01536 0.00981 -0.1113 0.7843 0.0257
-11.750 -0.5330 0.01489 0.00927 -0.1102 0.7809 0.0259
-11.500 -0.5094 0.01447 0.00880 -0.1093 0.7781 0.0261
-11.250 -0.4851 0.01409 0.00839 -0.1085 0.7751 0.0263
-11.000 -0.4606 0.01374 0.00800 -0.1076 0.7713 0.0265
-10.750 -0.4359 0.01342 0.00764 -0.1068 0.7675 0.0267
-10.500 -0.4110 0.01312 0.00729 -0.1060 0.7637 0.0270
-10.250 -0.3858 0.01281 0.00695 -0.1053 0.7596 0.0272
-10.000 -0.3605 0.01252 0.00661 -0.1046 0.7530 0.0274
-9.750 -0.3355 0.01224 0.00628 -0.1038 0.7469 0.0276
-9.500 -0.3098 0.01197 0.00596 -0.1031 0.7414 0.0279
-9.250 -0.2842 0.01171 0.00566 -0.1024 0.7335 0.0282
-9.000 -0.2587 0.01147 0.00536 -0.1016 0.7255 0.0284
-8.750 -0.2332 0.01125 0.00508 -0.1009 0.7140 0.0287
-8.500 -0.2082 0.01107 0.00482 -0.1000 0.6967 0.0289
-8.250 -0.1836 0.01095 0.00459 -0.0991 0.6747 0.0291
-8.000 -0.1599 0.01075 0.00429 -0.0980 0.6534 0.0296
-7.750 -0.1358 0.01064 0.00408 -0.0970 0.6324 0.0300
-7.500 -0.1113 0.01054 0.00390 -0.0961 0.6136 0.0304
-7.250 -0.0860 0.01044 0.00373 -0.0954 0.5996 0.0308
-7.000 -0.0606 0.01035 0.00358 -0.0946 0.5864 0.0312
-6.750 -0.0350 0.01026 0.00343 -0.0939 0.5717 0.0317
-6.500 -0.0097 0.01020 0.00329 -0.0932 0.5534 0.0322
-6.250 0.0150 0.01018 0.00316 -0.0923 0.5270 0.0327
-6.000 0.0343 0.01048 0.00312 -0.0905 0.4478 0.0331
-5.750 0.0567 0.01059 0.00306 -0.0893 0.4065 0.0336
-5.500 0.0809 0.01061 0.00299 -0.0884 0.3835 0.0344
-5.250 0.1059 0.01061 0.00292 -0.0877 0.3680 0.0352
-4.750 0.1573 0.01058 0.00279 -0.0864 0.3480 0.0372
-4.500 0.1830 0.01055 0.00273 -0.0858 0.3405 0.0384
-4.250 0.2090 0.01052 0.00268 -0.0852 0.3347 0.0399
-4.000 0.2353 0.01048 0.00264 -0.0847 0.3305 0.0414
-3.750 0.2614 0.01046 0.00259 -0.0842 0.3260 0.0429
-3.500 0.2872 0.01045 0.00256 -0.0837 0.3214 0.0449
-3.250 0.3131 0.01045 0.00255 -0.0831 0.3165 0.0471
-3.000 0.3395 0.01042 0.00252 -0.0827 0.3137 0.0492
-2.750 0.3654 0.01041 0.00251 -0.0822 0.3097 0.0519
-2.500 0.3915 0.01042 0.00250 -0.0817 0.3068 0.0545
-2.250 0.4172 0.01042 0.00250 -0.0811 0.3042 0.0579
-2.000 0.4430 0.01043 0.00251 -0.0806 0.3014 0.0608
-1.750 0.4687 0.01044 0.00252 -0.0801 0.2987 0.0647
-1.500 0.4949 0.01043 0.00252 -0.0797 0.2973 0.0688
-1.250 0.5207 0.01041 0.00252 -0.0792 0.2954 0.0755
-1.000 0.5454 0.01030 0.00256 -0.0786 0.2938 0.1223
-0.750 0.5710 0.01031 0.00261 -0.0781 0.2922 0.1409
-0.500 0.5966 0.01034 0.00266 -0.0776 0.2903 0.1489
-0.250 0.6221 0.01038 0.00271 -0.0771 0.2886 0.1549
0.000 0.6474 0.01044 0.00276 -0.0765 0.2867 0.1598
0.250 0.6724 0.01049 0.00282 -0.0760 0.2849 0.1654
0.500 0.6971 0.01056 0.00290 -0.0754 0.2828 0.1714
0.750 0.7218 0.01060 0.00297 -0.0747 0.2813 0.1819
1.000 0.7465 0.01058 0.00304 -0.0742 0.2804 0.2093
1.250 0.7667 0.01019 0.00315 -0.0729 0.2784 0.4098
1.500 0.7719 0.00927 0.00332 -0.0684 0.2765 0.8010
1.750 0.8778 0.00932 0.00370 -0.0855 0.2715 0.9876
2.000 0.9112 0.00949 0.00383 -0.0869 0.2690 0.9966
2.250 0.9485 0.00968 0.00397 -0.0892 0.2651 0.9999
2.500 0.9713 0.00978 0.00406 -0.0882 0.2633 1.0000
2.750 0.9925 0.00989 0.00416 -0.0870 0.2613 1.0000
3.000 1.0136 0.01000 0.00427 -0.0857 0.2591 1.0000
3.250 1.0342 0.01014 0.00438 -0.0844 0.2557 1.0000
3.500 1.0541 0.01030 0.00451 -0.0830 0.2516 1.0000
3.750 1.0747 0.01045 0.00464 -0.0817 0.2487 1.0000
4.000 1.0955 0.01059 0.00478 -0.0805 0.2450 1.0000
4.250 1.1152 0.01076 0.00492 -0.0790 0.2397 1.0000
4.500 1.1318 0.01096 0.00508 -0.0770 0.2326 1.0000
4.750 1.1467 0.01122 0.00527 -0.0747 0.2211 1.0000
5.000 1.1377 0.01242 0.00607 -0.0683 0.1543 1.0000
5.250 1.1454 0.01314 0.00665 -0.0650 0.1304 1.0000
5.500 1.1619 0.01351 0.00699 -0.0633 0.1234 1.0000
5.750 1.1785 0.01390 0.00735 -0.0617 0.1178 1.0000
6.000 1.1968 0.01422 0.00767 -0.0604 0.1144 1.0000
6.250 1.2150 0.01457 0.00801 -0.0591 0.1115 1.0000
6.500 1.2323 0.01497 0.00840 -0.0578 0.1080 1.0000
6.750 1.2498 0.01538 0.00880 -0.0565 0.1042 1.0000
7.000 1.2682 0.01576 0.00918 -0.0555 0.1014 1.0000
7.250 1.2853 0.01623 0.00964 -0.0543 0.0973 1.0000
7.500 1.3015 0.01675 0.01014 -0.0530 0.0925 1.0000
7.750 1.3085 0.01783 0.01105 -0.0508 0.0626 1.0000
8.000 1.3192 0.01874 0.01193 -0.0490 0.0542 1.0000
8.250 1.3341 0.01942 0.01262 -0.0479 0.0521 1.0000
8.500 1.3483 0.02015 0.01337 -0.0467 0.0505 1.0000
8.750 1.3625 0.02091 0.01415 -0.0456 0.0491 1.0000
9.000 1.3777 0.02162 0.01489 -0.0447 0.0483 1.0000
9.250 1.3926 0.02236 0.01567 -0.0438 0.0477 1.0000
9.500 1.4067 0.02316 0.01650 -0.0429 0.0471 1.0000
9.750 1.4202 0.02403 0.01741 -0.0420 0.0465 1.0000
10.000 1.4328 0.02497 0.01838 -0.0411 0.0458 1.0000
10.250 1.4448 0.02597 0.01942 -0.0401 0.0452 1.0000
10.500 1.4549 0.02712 0.02061 -0.0391 0.0445 1.0000
10.750 1.4640 0.02838 0.02190 -0.0381 0.0436 1.0000
11.000 1.4723 0.02973 0.02329 -0.0371 0.0428 1.0000
11.250 1.4829 0.03091 0.02453 -0.0364 0.0424 1.0000
11.500 1.4937 0.03212 0.02578 -0.0357 0.0418 1.0000
11.750 1.5025 0.03351 0.02723 -0.0350 0.0412 1.0000
12.000 1.5102 0.03506 0.02883 -0.0344 0.0407 1.0000
12.250 1.5171 0.03671 0.03053 -0.0338 0.0400 1.0000
12.500 1.5225 0.03855 0.03242 -0.0332 0.0394 1.0000
12.750 1.5270 0.04056 0.03449 -0.0327 0.0389 1.0000
13.000 1.5301 0.04279 0.03678 -0.0324 0.0385 1.0000
13.250 1.5310 0.04532 0.03938 -0.0321 0.0379 1.0000
13.500 1.5330 0.04779 0.04192 -0.0319 0.0374 1.0000
13.750 1.5349 0.05034 0.04454 -0.0319 0.0371 1.0000
14.000 1.5359 0.05304 0.04732 -0.0319 0.0368 1.0000
14.250 1.5357 0.05592 0.05028 -0.0321 0.0363 1.0000
14.500 1.5334 0.05909 0.05353 -0.0323 0.0360 1.0000
14.750 1.5291 0.06259 0.05713 -0.0326 0.0355 1.0000
15.000 1.5241 0.06626 0.06087 -0.0331 0.0350 1.0000
15.250 1.5166 0.07031 0.06501 -0.0336 0.0348 1.0000
15.500 1.5069 0.07476 0.06956 -0.0344 0.0345 1.0000
15.750 1.4963 0.07940 0.07429 -0.0353 0.0339 1.0000
16.000 1.4852 0.08416 0.07915 -0.0363 0.0336 1.0000
16.250 1.4727 0.08911 0.08418 -0.0374 0.0331 1.0000
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Polar data table (+)
Polar graphs
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