Rhode St. Genese 30 (rhodesg30-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
|---|---|
|
Airfoil: Rhode St. Genese 30 (rhodesg30-il) Reynolds number: 1,000,000 Max Cl/Cd: 85.38 at α=5.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-rhodesg30-il-1000000-n5.txt Download as CSV file: xf-rhodesg30-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: Rhode St. Genese 30
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
------ -------- --------- --------- -------- -------- --------
-14.000 -0.5056 0.11388 0.11213 -0.0209 1.0000 0.0038
-13.750 -0.5290 0.10388 0.10209 -0.0254 1.0000 0.0037
-13.500 -0.5472 0.09567 0.09384 -0.0295 1.0000 0.0037
-13.250 -0.5643 0.08817 0.08631 -0.0335 1.0000 0.0037
-13.000 -0.5796 0.08150 0.07961 -0.0373 1.0000 0.0036
-12.750 -0.6035 0.07353 0.07161 -0.0421 1.0000 0.0035
-12.500 -0.6259 0.06611 0.06418 -0.0468 1.0000 0.0035
-12.250 -0.6807 0.05530 0.05335 -0.0548 1.0000 0.0034
-11.750 -0.7138 0.03277 0.03012 -0.0718 0.9888 0.0034
-11.500 -0.6953 0.02952 0.02663 -0.0740 0.9804 0.0034
-11.250 -0.6709 0.02687 0.02376 -0.0764 0.9743 0.0035
-11.000 -0.6449 0.02468 0.02137 -0.0782 0.9665 0.0035
-10.750 -0.6170 0.02270 0.01919 -0.0800 0.9576 0.0036
-10.500 -0.5884 0.02112 0.01744 -0.0815 0.9468 0.0037
-10.250 -0.5623 0.01985 0.01599 -0.0820 0.9332 0.0039
-9.750 -0.5189 0.01765 0.01344 -0.0807 0.9079 0.0041
-9.500 -0.4972 0.01671 0.01234 -0.0798 0.8988 0.0042
-9.250 -0.4746 0.01591 0.01139 -0.0790 0.8907 0.0043
-9.000 -0.4514 0.01519 0.01055 -0.0783 0.8828 0.0043
-8.750 -0.4288 0.01436 0.00957 -0.0774 0.8740 0.0044
-8.500 -0.4052 0.01363 0.00871 -0.0767 0.8654 0.0047
-8.250 -0.3804 0.01310 0.00808 -0.0761 0.8586 0.0048
-8.000 -0.3552 0.01261 0.00749 -0.0755 0.8504 0.0050
-7.750 -0.3300 0.01217 0.00695 -0.0749 0.8426 0.0051
-7.500 -0.3045 0.01175 0.00645 -0.0743 0.8326 0.0053
-7.250 -0.2789 0.01137 0.00597 -0.0738 0.8219 0.0055
-7.000 -0.2532 0.01103 0.00553 -0.0732 0.8107 0.0058
-6.750 -0.2272 0.01076 0.00516 -0.0727 0.7983 0.0060
-6.500 -0.2011 0.01055 0.00487 -0.0721 0.7846 0.0063
-6.250 -0.1749 0.01039 0.00463 -0.0716 0.7692 0.0068
-6.000 -0.1490 0.01018 0.00433 -0.0711 0.7529 0.0073
-5.750 -0.1232 0.00995 0.00400 -0.0705 0.7361 0.0077
-5.500 -0.0976 0.00972 0.00365 -0.0699 0.7172 0.0082
-5.250 -0.0723 0.00952 0.00332 -0.0693 0.6950 0.0086
-5.000 -0.0474 0.00924 0.00288 -0.0686 0.6733 0.0093
-4.750 -0.0223 0.00906 0.00255 -0.0679 0.6491 0.0103
-4.500 0.0036 0.00894 0.00231 -0.0674 0.6297 0.0114
-4.250 0.0297 0.00880 0.00208 -0.0669 0.6133 0.0128
-4.000 0.0559 0.00868 0.00186 -0.0664 0.5961 0.0153
-3.750 0.0820 0.00860 0.00180 -0.0660 0.5764 0.0353
-3.500 0.1089 0.00877 0.00195 -0.0658 0.5517 0.0380
-3.250 0.1349 0.00892 0.00198 -0.0653 0.5152 0.0391
-3.000 0.1601 0.00921 0.00208 -0.0648 0.4641 0.0398
-2.750 0.1852 0.00934 0.00205 -0.0642 0.4238 0.0405
-2.500 0.2110 0.00941 0.00203 -0.0638 0.3978 0.0415
-2.250 0.2376 0.00952 0.00209 -0.0635 0.3787 0.0423
-2.000 0.2640 0.00955 0.00207 -0.0632 0.3637 0.0429
-1.750 0.2904 0.00955 0.00201 -0.0629 0.3507 0.0433
-1.500 0.3168 0.00955 0.00196 -0.0625 0.3396 0.0438
-1.250 0.3437 0.00951 0.00190 -0.0623 0.3332 0.0443
-1.000 0.3703 0.00952 0.00187 -0.0620 0.3266 0.0448
-0.750 0.3974 0.00950 0.00184 -0.0618 0.3214 0.0453
-0.500 0.4243 0.00948 0.00182 -0.0616 0.3174 0.0457
-0.250 0.4512 0.00950 0.00182 -0.0614 0.3131 0.0462
0.000 0.4781 0.00950 0.00182 -0.0612 0.3079 0.0465
0.250 0.5048 0.00953 0.00184 -0.0610 0.3012 0.0468
0.500 0.5315 0.00957 0.00186 -0.0608 0.2959 0.0470
0.750 0.5583 0.00953 0.00182 -0.0605 0.2934 0.0484
1.000 0.5852 0.00953 0.00183 -0.0604 0.2893 0.0498
1.250 0.6119 0.00956 0.00186 -0.0602 0.2841 0.0512
1.500 0.6385 0.00962 0.00191 -0.0600 0.2780 0.0527
1.750 0.6654 0.00966 0.00197 -0.0598 0.2728 0.0541
2.000 0.6919 0.00973 0.00203 -0.0596 0.2669 0.0554
2.250 0.7185 0.00980 0.00211 -0.0594 0.2601 0.0564
2.500 0.7446 0.00991 0.00219 -0.0591 0.2500 0.0573
2.750 0.7703 0.01005 0.00229 -0.0588 0.2354 0.0607
3.000 0.7869 0.01100 0.00279 -0.0571 0.1368 0.0684
3.250 0.8092 0.01095 0.00309 -0.0564 0.1175 0.2937
3.750 0.8782 0.01042 0.00393 -0.0607 0.0547 1.0000
4.000 0.9011 0.01073 0.00420 -0.0599 0.0432 1.0000
4.250 0.9245 0.01100 0.00444 -0.0592 0.0391 1.0000
4.500 0.9481 0.01125 0.00470 -0.0585 0.0358 1.0000
4.750 0.9719 0.01149 0.00495 -0.0578 0.0341 1.0000
5.000 0.9957 0.01172 0.00519 -0.0572 0.0336 1.0000
5.250 1.0194 0.01197 0.00546 -0.0566 0.0331 1.0000
5.500 1.0430 0.01222 0.00574 -0.0560 0.0326 1.0000
5.750 1.0664 0.01249 0.00604 -0.0553 0.0319 1.0000
6.000 1.0896 0.01277 0.00632 -0.0547 0.0305 1.0000
6.250 1.1123 0.01308 0.00664 -0.0540 0.0290 1.0000
6.500 1.1346 0.01341 0.00699 -0.0532 0.0276 1.0000
6.750 1.1564 0.01378 0.00738 -0.0524 0.0262 1.0000
7.000 1.1776 0.01419 0.00784 -0.0514 0.0250 1.0000
7.250 1.2006 0.01443 0.00809 -0.0509 0.0246 1.0000
7.500 1.2233 0.01468 0.00838 -0.0502 0.0240 1.0000
7.750 1.2455 0.01495 0.00868 -0.0495 0.0228 1.0000
8.000 1.2669 0.01528 0.00901 -0.0487 0.0202 1.0000
8.250 1.2864 0.01571 0.00939 -0.0477 0.0158 1.0000
8.500 1.3047 0.01621 0.00985 -0.0464 0.0119 1.0000
8.750 1.3222 0.01674 0.01039 -0.0450 0.0099 1.0000
9.000 1.3386 0.01728 0.01096 -0.0435 0.0083 1.0000
9.250 1.3530 0.01780 0.01152 -0.0415 0.0075 1.0000
9.500 1.3650 0.01840 0.01215 -0.0392 0.0067 1.0000
9.750 1.3763 0.01904 0.01284 -0.0368 0.0060 1.0000
10.000 1.3889 0.01963 0.01349 -0.0348 0.0057 1.0000
10.250 1.4005 0.02031 0.01422 -0.0328 0.0053 1.0000
10.500 1.4112 0.02105 0.01503 -0.0308 0.0050 1.0000
10.750 1.4201 0.02193 0.01596 -0.0287 0.0046 1.0000
11.000 1.4281 0.02292 0.01701 -0.0266 0.0043 1.0000
11.250 1.4369 0.02390 0.01807 -0.0249 0.0041 1.0000
11.500 1.4453 0.02496 0.01920 -0.0232 0.0040 1.0000
11.750 1.4527 0.02614 0.02046 -0.0216 0.0038 1.0000
12.000 1.4593 0.02744 0.02183 -0.0201 0.0036 1.0000
12.250 1.4646 0.02891 0.02339 -0.0187 0.0036 1.0000
12.500 1.4689 0.03055 0.02511 -0.0175 0.0033 1.0000
12.750 1.4729 0.03230 0.02695 -0.0165 0.0033 1.0000
13.000 1.4743 0.03440 0.02913 -0.0156 0.0031 1.0000
13.250 1.4759 0.03658 0.03140 -0.0150 0.0030 1.0000
13.500 1.4759 0.03908 0.03400 -0.0146 0.0030 1.0000
13.750 1.4737 0.04193 0.03695 -0.0144 0.0029 1.0000
14.000 1.4661 0.04555 0.04069 -0.0145 0.0028 1.0000
14.250 1.4622 0.04893 0.04417 -0.0150 0.0027 1.0000
14.500 1.4564 0.05268 0.04803 -0.0157 0.0027 1.0000
14.750 1.4507 0.05660 0.05207 -0.0166 0.0027 1.0000
15.000 1.4452 0.06064 0.05622 -0.0178 0.0026 1.0000
15.250 1.4362 0.06533 0.06103 -0.0193 0.0026 1.0000
15.500 1.4287 0.06993 0.06574 -0.0209 0.0025 1.0000
15.750 1.4164 0.07542 0.07135 -0.0229 0.0025 1.0000
16.000 1.4090 0.08018 0.07621 -0.0247 0.0025 1.0000
16.250 1.3946 0.08613 0.08228 -0.0270 0.0025 1.0000
16.500 1.3820 0.09190 0.08817 -0.0293 0.0025 1.0000
16.750 1.3694 0.09769 0.09406 -0.0317 0.0025 1.0000
|
Polar data table (+)
Polar graphs
<< Back to Rhode St. Genese 30 (rhodesg30-il)