Joukovsky f=0% t=18% (joukowsk0018-jf) Xfoil prediction polar at RE=200,000 Ncrit=9
| Details | Polar file |
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Airfoil: Joukovsky f=0% t=18% (joukowsk0018-jf) Reynolds number: 200,000 Max Cl/Cd: 49.17 at α=8.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-joukowsk0018-jf-200000.txt Download as CSV file: xf-joukowsk0018-jf-200000.csv |
XFOIL Version 6.96
Calculated polar for: Joukovsky f=0% t=18%
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
------ -------- --------- --------- -------- -------- --------
-18.750 -1.2128 0.09747 0.09199 -0.0107 1.0000 0.0815
-18.500 -1.2537 0.08760 0.08177 -0.0169 1.0000 0.0823
-18.250 -1.2529 0.08424 0.07837 -0.0183 1.0000 0.0837
-18.000 -1.2333 0.08371 0.07795 -0.0179 1.0000 0.0854
-17.750 -1.2381 0.07963 0.07379 -0.0200 1.0000 0.0868
-17.500 -1.2525 0.07436 0.06833 -0.0228 1.0000 0.0882
-17.250 -1.2703 0.06893 0.06266 -0.0255 1.0000 0.0895
-17.000 -1.2838 0.06429 0.05781 -0.0276 1.0000 0.0908
-16.750 -1.2607 0.06395 0.05763 -0.0270 1.0000 0.0928
-16.500 -1.2568 0.06149 0.05514 -0.0277 1.0000 0.0947
-16.250 -1.2612 0.05817 0.05169 -0.0289 1.0000 0.0965
-16.000 -1.2709 0.05447 0.04778 -0.0303 1.0000 0.0981
-15.750 -1.2645 0.05234 0.04562 -0.0305 1.0000 0.1001
-15.500 -1.2526 0.05088 0.04423 -0.0305 1.0000 0.1022
-15.250 -1.2496 0.04863 0.04191 -0.0308 1.0000 0.1044
-15.000 -1.2526 0.04593 0.03904 -0.0313 1.0000 0.1066
-14.750 -1.2480 0.04383 0.03688 -0.0313 1.0000 0.1089
-14.500 -1.2357 0.04250 0.03562 -0.0311 1.0000 0.1114
-14.250 -1.2305 0.04069 0.03376 -0.0310 1.0000 0.1140
-14.000 -1.2299 0.03860 0.03151 -0.0309 1.0000 0.1166
-13.750 -1.2189 0.03713 0.03005 -0.0305 1.0000 0.1194
-13.500 -1.2089 0.03580 0.02876 -0.0300 1.0000 0.1223
-13.250 -1.2029 0.03427 0.02716 -0.0295 1.0000 0.1254
-13.000 -1.1989 0.03268 0.02541 -0.0287 1.0000 0.1284
-12.750 -1.1840 0.03161 0.02446 -0.0281 1.0000 0.1318
-12.500 -1.1752 0.03043 0.02325 -0.0273 1.0000 0.1353
-12.250 -1.1701 0.02918 0.02185 -0.0261 1.0000 0.1389
-12.000 -1.1549 0.02816 0.02095 -0.0253 1.0000 0.1428
-11.750 -1.1449 0.02723 0.02001 -0.0240 1.0000 0.1468
-11.500 -1.1377 0.02631 0.01894 -0.0223 1.0000 0.1509
-11.250 -1.1224 0.02541 0.01818 -0.0212 1.0000 0.1552
-11.000 -1.1112 0.02471 0.01746 -0.0194 1.0000 0.1598
-10.750 -1.0980 0.02398 0.01664 -0.0179 1.0000 0.1648
-10.500 -1.0805 0.02325 0.01602 -0.0170 1.0000 0.1699
-10.250 -1.0638 0.02265 0.01536 -0.0158 1.0000 0.1758
-10.000 -1.0448 0.02192 0.01470 -0.0150 1.0000 0.1815
-9.750 -1.0256 0.02138 0.01416 -0.0141 1.0000 0.1878
-9.500 -1.0054 0.02076 0.01353 -0.0134 1.0000 0.1943
-9.250 -0.9845 0.02023 0.01307 -0.0127 1.0000 0.2009
-9.000 -0.9631 0.01972 0.01251 -0.0121 1.0000 0.2082
-8.750 -0.9412 0.01920 0.01211 -0.0116 1.0000 0.2152
-8.500 -0.9196 0.01880 0.01164 -0.0110 1.0000 0.2230
-8.250 -0.9003 0.01831 0.01131 -0.0101 1.0000 0.2301
-8.000 -0.8800 0.01804 0.01098 -0.0097 0.9942 0.2382
-7.750 -0.8355 0.01751 0.01057 -0.0134 0.9787 0.2486
-7.500 -0.7942 0.01708 0.01013 -0.0163 0.9618 0.2593
-7.250 -0.7592 0.01679 0.00984 -0.0177 0.9422 0.2696
-7.000 -0.7324 0.01650 0.00956 -0.0174 0.9217 0.2786
-6.750 -0.7108 0.01636 0.00937 -0.0160 0.9020 0.2877
-6.500 -0.6900 0.01613 0.00914 -0.0144 0.8840 0.2963
-6.250 -0.6683 0.01600 0.00895 -0.0129 0.8673 0.3057
-6.000 -0.6460 0.01578 0.00872 -0.0116 0.8522 0.3146
-5.750 -0.6234 0.01566 0.00854 -0.0103 0.8384 0.3243
-5.500 -0.5987 0.01543 0.00832 -0.0095 0.8233 0.3337
-5.250 -0.5740 0.01531 0.00815 -0.0087 0.8098 0.3440
-5.000 -0.5495 0.01511 0.00794 -0.0077 0.7974 0.3535
-4.750 -0.5233 0.01500 0.00778 -0.0072 0.7836 0.3641
-4.500 -0.4977 0.01482 0.00762 -0.0064 0.7718 0.3737
-4.250 -0.4711 0.01472 0.00745 -0.0059 0.7588 0.3847
-4.000 -0.4446 0.01456 0.00732 -0.0054 0.7470 0.3943
-3.750 -0.4179 0.01448 0.00716 -0.0049 0.7348 0.4055
-3.500 -0.3907 0.01433 0.00707 -0.0045 0.7229 0.4152
-3.250 -0.3636 0.01428 0.00690 -0.0040 0.7115 0.4266
-3.000 -0.3361 0.01414 0.00685 -0.0037 0.6994 0.4363
-2.750 -0.3087 0.01410 0.00668 -0.0032 0.6885 0.4478
-2.500 -0.2809 0.01398 0.00666 -0.0029 0.6765 0.4576
-2.250 -0.2533 0.01394 0.00651 -0.0025 0.6658 0.4690
-2.000 -0.2252 0.01385 0.00651 -0.0023 0.6539 0.4790
-1.750 -0.1974 0.01381 0.00637 -0.0019 0.6433 0.4904
-1.500 -0.1692 0.01375 0.00639 -0.0017 0.6315 0.5005
-1.250 -0.1412 0.01372 0.00627 -0.0013 0.6210 0.5119
-1.000 -0.1129 0.01367 0.00631 -0.0011 0.6094 0.5221
-0.750 -0.0848 0.01366 0.00620 -0.0008 0.5990 0.5335
-0.500 -0.0565 0.01363 0.00626 -0.0005 0.5873 0.5438
-0.250 -0.0283 0.01363 0.00617 -0.0003 0.5770 0.5552
0.000 0.0000 0.01362 0.00624 0.0000 0.5655 0.5655
0.250 0.0283 0.01363 0.00617 0.0003 0.5552 0.5771
0.500 0.0565 0.01363 0.00626 0.0005 0.5438 0.5873
0.750 0.0848 0.01366 0.00620 0.0008 0.5335 0.5990
1.000 0.1129 0.01367 0.00631 0.0011 0.5221 0.6094
1.250 0.1412 0.01372 0.00627 0.0013 0.5119 0.6210
1.500 0.1692 0.01375 0.00639 0.0017 0.5005 0.6315
1.750 0.1973 0.01381 0.00637 0.0019 0.4904 0.6433
2.000 0.2252 0.01385 0.00651 0.0023 0.4790 0.6539
2.250 0.2532 0.01394 0.00651 0.0025 0.4690 0.6658
2.500 0.2809 0.01398 0.00666 0.0029 0.4576 0.6765
2.750 0.3087 0.01410 0.00668 0.0032 0.4478 0.6885
3.000 0.3361 0.01414 0.00685 0.0037 0.4363 0.6995
3.250 0.3636 0.01428 0.00690 0.0040 0.4266 0.7115
3.500 0.3907 0.01433 0.00707 0.0045 0.4152 0.7229
3.750 0.4178 0.01448 0.00716 0.0049 0.4055 0.7348
4.000 0.4446 0.01456 0.00732 0.0054 0.3943 0.7470
4.250 0.4711 0.01472 0.00745 0.0060 0.3847 0.7588
4.500 0.4977 0.01482 0.00762 0.0064 0.3737 0.7718
4.750 0.5232 0.01500 0.00778 0.0072 0.3641 0.7836
5.000 0.5494 0.01511 0.00794 0.0077 0.3535 0.7974
5.250 0.5740 0.01531 0.00815 0.0087 0.3440 0.8098
5.500 0.5987 0.01543 0.00832 0.0095 0.3338 0.8233
5.750 0.6234 0.01566 0.00854 0.0103 0.3244 0.8384
6.000 0.6460 0.01578 0.00872 0.0116 0.3147 0.8522
6.250 0.6683 0.01600 0.00895 0.0129 0.3057 0.8674
6.500 0.6900 0.01613 0.00914 0.0144 0.2963 0.8840
6.750 0.7108 0.01636 0.00937 0.0160 0.2878 0.9020
7.000 0.7324 0.01650 0.00956 0.0174 0.2786 0.9217
7.250 0.7592 0.01679 0.00984 0.0177 0.2696 0.9422
7.500 0.7942 0.01708 0.01013 0.0163 0.2594 0.9618
7.750 0.8356 0.01751 0.01057 0.0133 0.2486 0.9787
8.000 0.8801 0.01804 0.01097 0.0097 0.2382 0.9943
8.250 0.9003 0.01831 0.01131 0.0101 0.2301 1.0000
8.500 0.9196 0.01880 0.01164 0.0110 0.2230 1.0000
8.750 0.9412 0.01920 0.01211 0.0116 0.2152 1.0000
9.000 0.9631 0.01972 0.01251 0.0121 0.2082 1.0000
9.250 0.9845 0.02023 0.01307 0.0127 0.2009 1.0000
9.500 1.0054 0.02076 0.01353 0.0134 0.1943 1.0000
9.750 1.0256 0.02138 0.01416 0.0141 0.1877 1.0000
10.000 1.0449 0.02192 0.01470 0.0150 0.1814 1.0000
10.250 1.0639 0.02265 0.01535 0.0158 0.1757 1.0000
10.500 1.0807 0.02325 0.01602 0.0169 0.1698 1.0000
10.750 1.0982 0.02398 0.01664 0.0179 0.1648 1.0000
11.000 1.1115 0.02471 0.01746 0.0194 0.1597 1.0000
11.250 1.1227 0.02541 0.01817 0.0211 0.1551 1.0000
11.500 1.1379 0.02631 0.01895 0.0222 0.1508 1.0000
11.750 1.1453 0.02722 0.02001 0.0239 0.1467 1.0000
12.000 1.1555 0.02816 0.02095 0.0252 0.1428 1.0000
12.250 1.1707 0.02918 0.02185 0.0260 0.1389 1.0000
12.500 1.1758 0.03042 0.02324 0.0272 0.1353 1.0000
12.750 1.1847 0.03159 0.02445 0.0281 0.1318 1.0000
13.000 1.1998 0.03266 0.02539 0.0287 0.1284 1.0000
13.250 1.2037 0.03425 0.02713 0.0294 0.1254 1.0000
13.500 1.2098 0.03578 0.02874 0.0299 0.1222 1.0000
13.750 1.2200 0.03710 0.03003 0.0303 0.1194 1.0000
14.000 1.2306 0.03859 0.03150 0.0308 0.1165 1.0000
14.250 1.2312 0.04068 0.03375 0.0309 0.1139 1.0000
14.500 1.2369 0.04247 0.03559 0.0310 0.1113 1.0000
14.750 1.2494 0.04378 0.03681 0.0312 0.1088 1.0000
15.000 1.2536 0.04590 0.03902 0.0312 0.1065 1.0000
15.250 1.2509 0.04859 0.04188 0.0307 0.1044 1.0000
15.500 1.2540 0.05082 0.04417 0.0304 0.1022 1.0000
15.750 1.2662 0.05224 0.04551 0.0304 0.1000 1.0000
16.000 1.2726 0.05438 0.04769 0.0302 0.0981 1.0000
16.250 1.2624 0.05814 0.05166 0.0288 0.0964 1.0000
16.500 1.2581 0.06143 0.05508 0.0276 0.0946 1.0000
16.750 1.2625 0.06385 0.05753 0.0269 0.0928 1.0000
17.000 1.2872 0.06403 0.05752 0.0277 0.0907 1.0000
17.250 1.2718 0.06886 0.06259 0.0254 0.0894 1.0000
17.500 1.2535 0.07436 0.06833 0.0226 0.0881 1.0000
17.750 1.2400 0.07952 0.07366 0.0199 0.0868 1.0000
18.000 1.2360 0.08348 0.07771 0.0179 0.0853 1.0000
18.250 1.2578 0.08369 0.07779 0.0185 0.0836 1.0000
18.500 1.2548 0.08759 0.08177 0.0167 0.0823 1.0000
18.750 1.2140 0.09747 0.09199 0.0105 0.0815 1.0000
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