Rhode St. Genese 34 (rhodesg34-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: Rhode St. Genese 34 (rhodesg34-il) Reynolds number: 200,000 Max Cl/Cd: 59.06 at α=6.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-rhodesg34-il-200000-n5.txt Download as CSV file: xf-rhodesg34-il-200000-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 = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-14.250 -0.2572 0.12983 0.12594 -0.0416 1.0000 0.0461
-14.000 -0.2582 0.12683 0.12297 -0.0426 1.0000 0.0473
-13.750 -0.2632 0.12374 0.11993 -0.0438 1.0000 0.0478
-13.500 -0.2590 0.11938 0.11559 -0.0474 0.9931 0.0479
-13.250 -0.2525 0.11432 0.11052 -0.0525 0.9833 0.0481
-13.000 -0.2436 0.10954 0.10572 -0.0571 0.9726 0.0482
-12.500 -0.2100 0.10057 0.09669 -0.0628 0.9544 0.0423
-12.250 -0.1904 0.09708 0.09317 -0.0661 0.9455 0.0415
-12.000 -0.1739 0.09255 0.08860 -0.0712 0.9368 0.0407
-11.750 -0.1607 0.08743 0.08344 -0.0769 0.9278 0.0399
-11.500 -0.1479 0.08205 0.07802 -0.0832 0.9188 0.0395
-11.250 -0.1339 0.07720 0.07311 -0.0892 0.9091 0.0400
-11.000 -0.1247 0.07186 0.06772 -0.0954 0.8983 0.0401
-10.750 -0.1223 0.06572 0.06152 -0.1022 0.8866 0.0399
-10.500 -0.2527 0.04086 0.03597 -0.1174 0.8674 0.0385
-10.250 -0.2606 0.03696 0.03170 -0.1161 0.8590 0.0386
-10.000 -0.2557 0.03415 0.02855 -0.1150 0.8524 0.0389
-9.750 -0.2490 0.03178 0.02588 -0.1133 0.8452 0.0392
-9.500 -0.2359 0.03003 0.02386 -0.1119 0.8386 0.0397
-9.250 -0.2199 0.02835 0.02186 -0.1108 0.8332 0.0404
-9.000 -0.2058 0.02672 0.01993 -0.1090 0.8263 0.0410
-8.750 -0.1888 0.02514 0.01800 -0.1076 0.8201 0.0417
-8.500 -0.1689 0.02371 0.01620 -0.1064 0.8146 0.0422
-8.250 -0.1496 0.02255 0.01474 -0.1050 0.8078 0.0426
-8.000 -0.1268 0.02170 0.01381 -0.1041 0.8015 0.0431
-7.750 -0.1027 0.02103 0.01303 -0.1033 0.7958 0.0436
-7.500 -0.0801 0.02040 0.01234 -0.1023 0.7885 0.0442
-7.250 -0.0557 0.01976 0.01159 -0.1014 0.7820 0.0448
-7.000 -0.0319 0.01920 0.01092 -0.1005 0.7749 0.0458
-6.750 -0.0079 0.01863 0.01023 -0.0996 0.7671 0.0469
-6.500 0.0168 0.01809 0.00951 -0.0987 0.7591 0.0481
-6.250 0.0407 0.01753 0.00898 -0.0978 0.7498 0.0490
-6.000 0.0651 0.01707 0.00851 -0.0969 0.7406 0.0499
-5.750 0.0896 0.01663 0.00803 -0.0960 0.7305 0.0510
-5.500 0.1135 0.01621 0.00756 -0.0950 0.7180 0.0522
-5.250 0.1378 0.01581 0.00709 -0.0941 0.7041 0.0537
-5.000 0.1620 0.01542 0.00667 -0.0931 0.6900 0.0553
-4.750 0.1863 0.01512 0.00632 -0.0922 0.6748 0.0572
-4.500 0.2105 0.01485 0.00595 -0.0912 0.6580 0.0596
-4.250 0.2342 0.01461 0.00559 -0.0901 0.6399 0.0617
-4.000 0.2572 0.01439 0.00529 -0.0890 0.6211 0.0641
-3.750 0.2803 0.01426 0.00505 -0.0878 0.6013 0.0672
-3.500 0.3027 0.01413 0.00482 -0.0866 0.5793 0.0707
-3.250 0.3247 0.01406 0.00463 -0.0853 0.5532 0.0751
-3.000 0.3454 0.01402 0.00445 -0.0838 0.5168 0.0800
-2.750 0.3633 0.01412 0.00433 -0.0818 0.4698 0.0869
-2.500 0.3810 0.01421 0.00434 -0.0798 0.4372 0.1012
-2.250 0.4009 0.01433 0.00445 -0.0783 0.4169 0.1430
-2.000 0.4220 0.01443 0.00450 -0.0770 0.4033 0.1650
-1.500 0.4654 0.01455 0.00460 -0.0746 0.3852 0.2047
-1.250 0.4868 0.01456 0.00468 -0.0734 0.3785 0.2387
-1.000 0.5068 0.01443 0.00478 -0.0721 0.3733 0.3247
-0.750 0.5235 0.01394 0.00491 -0.0701 0.3690 0.5161
-0.500 0.5401 0.01337 0.00513 -0.0675 0.3648 0.7646
-0.250 0.6640 0.01381 0.00564 -0.0873 0.3564 1.0000
0.000 0.6841 0.01399 0.00575 -0.0858 0.3535 1.0000
0.250 0.7048 0.01416 0.00586 -0.0844 0.3507 1.0000
0.500 0.7255 0.01435 0.00599 -0.0831 0.3478 1.0000
0.750 0.7461 0.01456 0.00612 -0.0818 0.3449 1.0000
1.000 0.7666 0.01478 0.00627 -0.0804 0.3421 1.0000
1.250 0.7868 0.01503 0.00643 -0.0790 0.3391 1.0000
1.500 0.8074 0.01533 0.00662 -0.0778 0.3363 1.0000
1.750 0.8291 0.01551 0.00679 -0.0767 0.3341 1.0000
2.000 0.8506 0.01571 0.00698 -0.0756 0.3316 1.0000
2.250 0.8725 0.01593 0.00718 -0.0745 0.3297 1.0000
2.500 0.8942 0.01616 0.00739 -0.0735 0.3276 1.0000
2.750 0.9156 0.01639 0.00760 -0.0724 0.3251 1.0000
3.000 0.9370 0.01665 0.00782 -0.0714 0.3228 1.0000
3.250 0.9584 0.01693 0.00805 -0.0704 0.3206 1.0000
3.500 0.9808 0.01724 0.00832 -0.0696 0.3187 1.0000
3.750 1.0032 0.01755 0.00860 -0.0688 0.3167 1.0000
4.000 1.0245 0.01777 0.00886 -0.0678 0.3148 1.0000
4.250 1.0454 0.01801 0.00914 -0.0667 0.3125 1.0000
4.500 1.0651 0.01824 0.00940 -0.0655 0.3095 1.0000
4.750 1.0833 0.01848 0.00965 -0.0640 0.3063 1.0000
5.000 1.1014 0.01875 0.00991 -0.0625 0.3033 1.0000
5.250 1.1203 0.01907 0.01020 -0.0612 0.3006 1.0000
5.500 1.1403 0.01940 0.01052 -0.0601 0.2983 1.0000
5.750 1.1588 0.01966 0.01086 -0.0587 0.2961 1.0000
6.000 1.1774 0.01994 0.01121 -0.0575 0.2937 1.0000
6.250 1.1954 0.02024 0.01156 -0.0561 0.2909 1.0000
6.500 1.2125 0.02054 0.01191 -0.0547 0.2878 1.0000
6.750 1.2296 0.02088 0.01227 -0.0533 0.2849 1.0000
7.000 1.2478 0.02126 0.01266 -0.0522 0.2828 1.0000
7.250 1.2660 0.02164 0.01308 -0.0511 0.2805 1.0000
7.500 1.2835 0.02200 0.01355 -0.0499 0.2779 1.0000
7.750 1.3002 0.02238 0.01404 -0.0486 0.2746 1.0000
8.000 1.3145 0.02280 0.01452 -0.0471 0.2701 1.0000
8.250 1.3281 0.02327 0.01501 -0.0456 0.2663 1.0000
8.500 1.3437 0.02375 0.01558 -0.0444 0.2622 1.0000
8.750 1.3592 0.02424 0.01619 -0.0432 0.2576 1.0000
9.000 1.3730 0.02480 0.01682 -0.0419 0.2532 1.0000
9.250 1.3861 0.02542 0.01750 -0.0406 0.2486 1.0000
9.500 1.4005 0.02603 0.01823 -0.0395 0.2414 1.0000
9.750 1.4118 0.02678 0.01904 -0.0382 0.2333 1.0000
10.000 1.4230 0.02759 0.01991 -0.0370 0.2222 1.0000
10.250 1.4290 0.02869 0.02099 -0.0353 0.2013 1.0000
10.500 1.4179 0.03093 0.02299 -0.0326 0.1716 1.0000
10.750 1.4125 0.03312 0.02510 -0.0305 0.1573 1.0000
11.000 1.4102 0.03522 0.02721 -0.0289 0.1480 1.0000
11.250 1.4073 0.03748 0.02950 -0.0275 0.1403 1.0000
11.500 1.4074 0.03960 0.03167 -0.0264 0.1351 1.0000
11.750 1.4045 0.04209 0.03422 -0.0254 0.1307 1.0000
12.000 1.4052 0.04437 0.03660 -0.0247 0.1265 1.0000
12.250 1.4033 0.04700 0.03932 -0.0242 0.1225 1.0000
12.500 1.3975 0.05018 0.04259 -0.0238 0.1186 1.0000
12.750 1.3938 0.05328 0.04579 -0.0237 0.1150 1.0000
13.000 1.3892 0.05659 0.04921 -0.0237 0.1107 1.0000
13.250 1.3809 0.06048 0.05319 -0.0239 0.1069 1.0000
13.500 1.3710 0.06471 0.05752 -0.0244 0.1033 1.0000
13.750 1.3636 0.06877 0.06170 -0.0250 0.0976 1.0000
14.000 1.3508 0.07370 0.06673 -0.0260 0.0929 1.0000
14.250 1.3425 0.07813 0.07128 -0.0270 0.0842 1.0000
14.500 1.3247 0.08401 0.07721 -0.0284 0.0743 1.0000
14.750 1.3049 0.09030 0.08350 -0.0301 0.0695 1.0000
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