Joukovsky f=0% t=15% (joukowsk0015-jf) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: Joukovsky f=0% t=15% (joukowsk0015-jf) Reynolds number: 500,000 Max Cl/Cd: 70.28 at α=7.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-joukowsk0015-jf-500000.txt Download as CSV file: xf-joukowsk0015-jf-500000.csv |
XFOIL Version 6.96
Calculated polar for: Joukovsky f=0% t=15%
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.250 -1.2527 0.10814 0.10394 0.0084 1.0000 0.0362
-19.000 -1.2591 0.10294 0.09862 0.0053 1.0000 0.0367
-18.750 -1.2655 0.09781 0.09335 0.0024 1.0000 0.0371
-18.500 -1.2655 0.09426 0.08978 0.0008 1.0000 0.0378
-18.250 -1.2678 0.09021 0.08571 -0.0013 1.0000 0.0383
-18.000 -1.2709 0.08598 0.08143 -0.0035 1.0000 0.0389
-17.750 -1.2743 0.08173 0.07711 -0.0057 1.0000 0.0395
-17.500 -1.2781 0.07749 0.07279 -0.0078 1.0000 0.0401
-17.250 -1.2815 0.07336 0.06857 -0.0099 1.0000 0.0408
-17.000 -1.2844 0.06937 0.06446 -0.0118 1.0000 0.0414
-16.750 -1.2872 0.06546 0.06042 -0.0137 1.0000 0.0420
-16.500 -1.2918 0.06172 0.05667 -0.0151 1.0000 0.0427
-16.250 -1.2959 0.05799 0.05291 -0.0167 1.0000 0.0435
-16.000 -1.2989 0.05449 0.04934 -0.0181 1.0000 0.0442
-15.750 -1.3006 0.05123 0.04601 -0.0193 1.0000 0.0449
-15.500 -1.3013 0.04814 0.04283 -0.0203 1.0000 0.0457
-15.250 -1.3005 0.04530 0.03989 -0.0212 1.0000 0.0466
-15.000 -1.2979 0.04271 0.03719 -0.0219 1.0000 0.0473
-14.750 -1.3029 0.03948 0.03393 -0.0225 1.0000 0.0483
-14.500 -1.3032 0.03678 0.03120 -0.0230 1.0000 0.0492
-14.250 -1.2992 0.03460 0.02896 -0.0233 1.0000 0.0504
-14.000 -1.2943 0.03258 0.02686 -0.0233 1.0000 0.0515
-13.750 -1.2865 0.03089 0.02507 -0.0232 1.0000 0.0528
-13.500 -1.2853 0.02877 0.02290 -0.0228 1.0000 0.0539
-13.250 -1.2823 0.02693 0.02104 -0.0222 1.0000 0.0552
-13.000 -1.2751 0.02554 0.01961 -0.0214 1.0000 0.0566
-12.750 -1.2659 0.02439 0.01839 -0.0205 1.0000 0.0582
-12.500 -1.2562 0.02337 0.01730 -0.0192 1.0000 0.0597
-12.250 -1.2536 0.02213 0.01605 -0.0171 1.0000 0.0614
-12.000 -1.2445 0.02133 0.01523 -0.0151 1.0000 0.0633
-11.750 -1.2292 0.02070 0.01455 -0.0137 1.0000 0.0655
-11.500 -1.2145 0.01989 0.01371 -0.0124 1.0000 0.0679
-11.250 -1.1973 0.01918 0.01301 -0.0113 1.0000 0.0705
-11.000 -1.1763 0.01868 0.01246 -0.0105 1.0000 0.0735
-10.750 -1.1578 0.01794 0.01173 -0.0096 1.0000 0.0767
-10.500 -1.1364 0.01739 0.01118 -0.0089 1.0000 0.0803
-10.250 -1.1141 0.01687 0.01062 -0.0083 1.0000 0.0839
-10.000 -1.0923 0.01628 0.01007 -0.0077 1.0000 0.0883
-9.750 -1.0682 0.01586 0.00962 -0.0072 1.0000 0.0926
-9.500 -1.0455 0.01528 0.00909 -0.0067 1.0000 0.0978
-9.250 -1.0207 0.01489 0.00868 -0.0063 1.0000 0.1029
-9.000 -0.9969 0.01437 0.00821 -0.0059 1.0000 0.1091
-8.750 -0.9716 0.01397 0.00781 -0.0056 1.0000 0.1152
-8.500 -0.9466 0.01353 0.00742 -0.0053 1.0000 0.1222
-8.250 -0.9211 0.01312 0.00704 -0.0050 1.0000 0.1295
-8.000 -0.8949 0.01279 0.00673 -0.0048 1.0000 0.1372
-7.750 -0.8694 0.01237 0.00638 -0.0046 1.0000 0.1459
-7.500 -0.8429 0.01204 0.00607 -0.0045 1.0000 0.1546
-7.250 -0.8165 0.01172 0.00580 -0.0044 1.0000 0.1643
-7.000 -0.7796 0.01136 0.00551 -0.0064 0.9743 0.1760
-6.750 -0.7454 0.01108 0.00526 -0.0077 0.9477 0.1876
-6.500 -0.7205 0.01092 0.00506 -0.0068 0.9207 0.1979
-6.250 -0.6974 0.01071 0.00485 -0.0056 0.8972 0.2091
-6.000 -0.6732 0.01052 0.00464 -0.0047 0.8767 0.2203
-5.750 -0.6478 0.01035 0.00444 -0.0039 0.8581 0.2318
-5.500 -0.6218 0.01019 0.00425 -0.0034 0.8408 0.2440
-5.250 -0.5955 0.00999 0.00406 -0.0029 0.8244 0.2565
-5.000 -0.5686 0.00983 0.00388 -0.0025 0.8087 0.2689
-4.500 -0.5138 0.00955 0.00356 -0.0019 0.7779 0.2950
-4.250 -0.4862 0.00939 0.00341 -0.0017 0.7632 0.3081
-4.000 -0.4583 0.00927 0.00328 -0.0015 0.7491 0.3211
-3.750 -0.4303 0.00918 0.00315 -0.0012 0.7348 0.3344
-3.500 -0.4020 0.00906 0.00303 -0.0011 0.7206 0.3480
-3.250 -0.3738 0.00894 0.00293 -0.0010 0.7068 0.3614
-3.000 -0.3455 0.00886 0.00282 -0.0008 0.6935 0.3746
-2.750 -0.3167 0.00879 0.00273 -0.0008 0.6794 0.3879
-2.500 -0.2882 0.00870 0.00266 -0.0007 0.6660 0.4017
-2.250 -0.2597 0.00863 0.00258 -0.0005 0.6529 0.4148
-2.000 -0.2309 0.00858 0.00251 -0.0005 0.6393 0.4281
-1.750 -0.2020 0.00853 0.00246 -0.0004 0.6261 0.4416
-1.500 -0.1734 0.00848 0.00241 -0.0003 0.6131 0.4549
-1.250 -0.1446 0.00844 0.00237 -0.0003 0.5996 0.4679
-1.000 -0.1155 0.00842 0.00233 -0.0002 0.5864 0.4813
-0.750 -0.0868 0.00839 0.00231 -0.0002 0.5735 0.4947
-0.500 -0.0579 0.00836 0.00229 -0.0001 0.5601 0.5076
-0.250 -0.0288 0.00836 0.00228 -0.0001 0.5470 0.5207
0.000 0.0000 0.00836 0.00228 0.0000 0.5341 0.5341
0.250 0.0288 0.00836 0.00228 0.0001 0.5208 0.5470
0.500 0.0579 0.00836 0.00229 0.0001 0.5076 0.5601
0.750 0.0868 0.00839 0.00231 0.0001 0.4946 0.5736
1.250 0.1446 0.00844 0.00237 0.0003 0.4679 0.5996
1.500 0.1734 0.00848 0.00241 0.0003 0.4549 0.6131
1.750 0.2021 0.00853 0.00246 0.0004 0.4416 0.6261
2.000 0.2309 0.00858 0.00251 0.0005 0.4280 0.6393
2.250 0.2597 0.00863 0.00258 0.0005 0.4148 0.6529
2.500 0.2882 0.00870 0.00266 0.0007 0.4017 0.6661
2.750 0.3168 0.00879 0.00273 0.0007 0.3880 0.6794
3.000 0.3455 0.00886 0.00282 0.0008 0.3745 0.6934
3.250 0.3738 0.00894 0.00293 0.0010 0.3614 0.7069
3.500 0.4020 0.00906 0.00303 0.0011 0.3480 0.7205
3.750 0.4303 0.00918 0.00315 0.0012 0.3343 0.7348
4.000 0.4583 0.00927 0.00328 0.0015 0.3211 0.7491
4.250 0.4862 0.00939 0.00341 0.0017 0.3082 0.7632
4.500 0.5138 0.00955 0.00356 0.0019 0.2950 0.7779
5.000 0.5686 0.00983 0.00388 0.0025 0.2690 0.8087
5.250 0.5955 0.00999 0.00406 0.0029 0.2565 0.8244
5.500 0.6218 0.01019 0.00425 0.0034 0.2440 0.8408
5.750 0.6478 0.01035 0.00444 0.0039 0.2318 0.8581
6.000 0.6732 0.01052 0.00464 0.0047 0.2202 0.8767
6.250 0.6974 0.01071 0.00485 0.0056 0.2091 0.8971
6.500 0.7205 0.01092 0.00506 0.0068 0.1979 0.9207
6.750 0.7454 0.01108 0.00526 0.0077 0.1876 0.9477
7.000 0.7796 0.01136 0.00551 0.0064 0.1760 0.9743
7.250 0.8165 0.01172 0.00580 0.0044 0.1643 1.0000
7.500 0.8429 0.01204 0.00607 0.0045 0.1547 1.0000
7.750 0.8694 0.01237 0.00638 0.0046 0.1459 1.0000
8.000 0.8950 0.01279 0.00673 0.0048 0.1372 1.0000
8.250 0.9212 0.01312 0.00704 0.0050 0.1295 1.0000
8.500 0.9466 0.01353 0.00742 0.0053 0.1222 1.0000
8.750 0.9716 0.01397 0.00781 0.0056 0.1151 1.0000
9.000 0.9968 0.01437 0.00821 0.0059 0.1090 1.0000
9.250 1.0206 0.01489 0.00868 0.0063 0.1029 1.0000
9.500 1.0455 0.01528 0.00909 0.0067 0.0978 1.0000
9.750 1.0681 0.01586 0.00962 0.0072 0.0926 1.0000
10.000 1.0922 0.01628 0.01007 0.0077 0.0883 1.0000
10.250 1.1141 0.01687 0.01062 0.0083 0.0839 1.0000
10.500 1.1363 0.01739 0.01118 0.0089 0.0803 1.0000
10.750 1.1578 0.01794 0.01173 0.0096 0.0767 1.0000
11.000 1.1765 0.01867 0.01244 0.0105 0.0734 1.0000
11.250 1.1974 0.01918 0.01300 0.0113 0.0705 1.0000
11.500 1.2146 0.01990 0.01371 0.0123 0.0679 1.0000
11.750 1.2296 0.02070 0.01454 0.0136 0.0655 1.0000
12.000 1.2449 0.02132 0.01523 0.0150 0.0633 1.0000
12.250 1.2540 0.02213 0.01605 0.0170 0.0615 1.0000
12.500 1.2565 0.02338 0.01730 0.0192 0.0597 1.0000
12.750 1.2663 0.02438 0.01839 0.0204 0.0581 1.0000
13.000 1.2755 0.02553 0.01960 0.0214 0.0565 1.0000
13.250 1.2826 0.02692 0.02103 0.0222 0.0552 1.0000
13.500 1.2855 0.02875 0.02289 0.0228 0.0539 1.0000
13.750 1.2876 0.03081 0.02499 0.0232 0.0527 1.0000
14.000 1.2948 0.03254 0.02682 0.0233 0.0515 1.0000
14.250 1.3003 0.03451 0.02887 0.0232 0.0503 1.0000
14.500 1.3037 0.03676 0.03118 0.0230 0.0493 1.0000
14.750 1.3040 0.03940 0.03384 0.0225 0.0482 1.0000
15.000 1.2988 0.04265 0.03713 0.0218 0.0473 1.0000
15.250 1.3016 0.04522 0.03982 0.0211 0.0465 1.0000
15.500 1.3025 0.04807 0.04276 0.0202 0.0457 1.0000
15.750 1.3021 0.05114 0.04592 0.0192 0.0448 1.0000
16.000 1.3004 0.05442 0.04926 0.0180 0.0441 1.0000
16.250 1.2977 0.05788 0.05279 0.0166 0.0434 1.0000
16.500 1.2933 0.06163 0.05658 0.0150 0.0427 1.0000
16.750 1.2887 0.06541 0.06037 0.0136 0.0419 1.0000
17.000 1.2864 0.06928 0.06437 0.0117 0.0413 1.0000
17.250 1.2834 0.07322 0.06842 0.0098 0.0408 1.0000
17.500 1.2798 0.07744 0.07274 0.0077 0.0400 1.0000
17.750 1.2763 0.08161 0.07698 0.0056 0.0394 1.0000
18.000 1.2729 0.08588 0.08133 0.0033 0.0389 1.0000
18.250 1.2701 0.09007 0.08557 0.0012 0.0383 1.0000
18.500 1.2678 0.09410 0.08962 -0.0009 0.0377 1.0000
18.750 1.2678 0.09768 0.09322 -0.0026 0.0371 1.0000
19.000 1.2611 0.10287 0.09855 -0.0055 0.0367 1.0000
19.250 1.2553 0.10791 0.10370 -0.0084 0.0362 1.0000
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