Joukovsky f=0% t=18% (joukowsk0018-jf) Xfoil prediction polar at RE=100,000 Ncrit=9
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Airfoil: Joukovsky f=0% t=18% (joukowsk0018-jf) Reynolds number: 100,000 Max Cl/Cd: 34.1 at α=7° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-joukowsk0018-jf-100000.txt Download as CSV file: xf-joukowsk0018-jf-100000.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 = 0.100 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-14.500 -0.5765 0.16449 0.15845 0.0318 1.0000 0.1950
-14.250 -1.0286 0.07259 0.06597 -0.0246 1.0000 0.1516
-14.000 -1.0867 0.06315 0.05627 -0.0289 1.0000 0.1524
-13.500 -1.0577 0.06041 0.05359 -0.0285 1.0000 0.1597
-13.250 -1.1178 0.05293 0.04576 -0.0302 1.0000 0.1604
-13.000 -1.1557 0.04856 0.04107 -0.0293 1.0000 0.1621
-12.750 -1.1893 0.04546 0.03762 -0.0262 1.0000 0.1637
-12.500 -1.1396 0.04529 0.03779 -0.0276 1.0000 0.1693
-12.250 -1.1444 0.04347 0.03584 -0.0256 1.0000 0.1730
-12.000 -1.1595 0.04121 0.03327 -0.0228 1.0000 0.1763
-11.750 -1.1362 0.04009 0.03227 -0.0225 1.0000 0.1811
-11.500 -1.1218 0.03909 0.03126 -0.0215 1.0000 0.1862
-11.250 -1.1252 0.03723 0.02908 -0.0193 1.0000 0.1911
-11.000 -1.0965 0.03643 0.02849 -0.0194 1.0000 0.1966
-10.750 -1.0831 0.03537 0.02735 -0.0182 1.0000 0.2026
-10.500 -1.0729 0.03389 0.02570 -0.0169 1.0000 0.2085
-10.250 -1.0462 0.03336 0.02536 -0.0167 1.0000 0.2149
-10.000 -1.0379 0.03207 0.02377 -0.0151 1.0000 0.2219
-9.750 -1.0097 0.03142 0.02337 -0.0151 1.0000 0.2285
-9.500 -0.9938 0.03051 0.02234 -0.0141 1.0000 0.2362
-9.250 -0.9713 0.02967 0.02158 -0.0136 1.0000 0.2434
-9.000 -0.9507 0.02902 0.02093 -0.0129 1.0000 0.2515
-8.750 -0.9308 0.02815 0.02005 -0.0122 1.0000 0.2594
-8.500 -0.9081 0.02766 0.01964 -0.0116 1.0000 0.2677
-8.250 -0.8903 0.02683 0.01876 -0.0106 1.0000 0.2761
-8.000 -0.8687 0.02646 0.01853 -0.0098 1.0000 0.2843
-7.750 -0.8617 0.02574 0.01767 -0.0073 1.0000 0.2925
-7.500 -0.8494 0.02551 0.01767 -0.0051 1.0000 0.2990
-7.250 -0.8484 0.02512 0.01719 -0.0018 1.0000 0.3064
-7.000 -0.8426 0.02472 0.01682 0.0008 1.0000 0.3133
-6.750 -0.7984 0.02441 0.01649 -0.0030 0.9891 0.3263
-6.500 -0.7453 0.02418 0.01642 -0.0078 0.9784 0.3389
-6.250 -0.6959 0.02376 0.01599 -0.0122 0.9663 0.3525
-6.000 -0.6488 0.02339 0.01549 -0.0163 0.9538 0.3672
-5.750 -0.6007 0.02327 0.01561 -0.0195 0.9417 0.3789
-5.500 -0.5602 0.02296 0.01527 -0.0218 0.9280 0.3916
-5.250 -0.5247 0.02277 0.01504 -0.0230 0.9136 0.4045
-5.000 -0.4929 0.02269 0.01506 -0.0230 0.8983 0.4145
-4.750 -0.4707 0.02248 0.01467 -0.0219 0.8814 0.4271
-4.500 -0.4437 0.02251 0.01489 -0.0208 0.8657 0.4358
-4.250 -0.4226 0.02232 0.01454 -0.0195 0.8505 0.4482
-4.000 -0.3971 0.02236 0.01470 -0.0178 0.8379 0.4570
-3.750 -0.3757 0.02216 0.01439 -0.0166 0.8222 0.4694
-3.500 -0.3504 0.02222 0.01457 -0.0153 0.8080 0.4784
-3.250 -0.3286 0.02203 0.01423 -0.0136 0.7966 0.4907
-3.000 -0.3028 0.02209 0.01442 -0.0126 0.7814 0.5001
-2.750 -0.2795 0.02193 0.01417 -0.0115 0.7689 0.5124
-2.500 -0.2542 0.02196 0.01426 -0.0101 0.7564 0.5221
-2.250 -0.2299 0.02184 0.01409 -0.0092 0.7429 0.5343
-2.000 -0.2047 0.02185 0.01412 -0.0077 0.7322 0.5444
-1.750 -0.1795 0.02176 0.01402 -0.0071 0.7181 0.5564
-1.500 -0.1542 0.02176 0.01400 -0.0055 0.7084 0.5668
-1.250 -0.1286 0.02171 0.01397 -0.0050 0.6940 0.5788
-1.000 -0.1030 0.02172 0.01397 -0.0037 0.6836 0.5896
-0.750 -0.0773 0.02166 0.01392 -0.0030 0.6704 0.6013
-0.500 -0.0516 0.02169 0.01395 -0.0018 0.6596 0.6126
-0.250 -0.0258 0.02163 0.01390 -0.0010 0.6470 0.6240
0.000 0.0000 0.02169 0.01394 0.0000 0.6360 0.6360
0.250 0.0258 0.02163 0.01389 0.0010 0.6240 0.6470
0.500 0.0515 0.02169 0.01395 0.0018 0.6126 0.6596
0.750 0.0773 0.02166 0.01392 0.0030 0.6013 0.6703
1.000 0.1030 0.02172 0.01397 0.0037 0.5896 0.6836
1.250 0.1286 0.02171 0.01397 0.0050 0.5788 0.6940
1.500 0.1542 0.02176 0.01400 0.0055 0.5668 0.7084
1.750 0.1795 0.02176 0.01402 0.0071 0.5564 0.7181
2.000 0.2046 0.02185 0.01412 0.0077 0.5444 0.7322
2.250 0.2298 0.02184 0.01409 0.0093 0.5343 0.7429
2.500 0.2542 0.02196 0.01426 0.0101 0.5221 0.7564
2.750 0.2795 0.02193 0.01417 0.0115 0.5124 0.7689
3.000 0.3028 0.02209 0.01442 0.0126 0.5001 0.7814
3.250 0.3286 0.02203 0.01424 0.0136 0.4907 0.7966
3.500 0.3504 0.02222 0.01457 0.0153 0.4784 0.8080
3.750 0.3757 0.02216 0.01439 0.0166 0.4694 0.8222
4.000 0.3971 0.02236 0.01470 0.0178 0.4570 0.8378
4.250 0.4226 0.02232 0.01454 0.0195 0.4482 0.8505
4.500 0.4436 0.02251 0.01489 0.0208 0.4358 0.8657
4.750 0.4707 0.02248 0.01467 0.0219 0.4271 0.8814
5.000 0.4929 0.02269 0.01505 0.0230 0.4145 0.8983
5.250 0.5247 0.02277 0.01503 0.0230 0.4046 0.9136
5.500 0.5601 0.02295 0.01527 0.0218 0.3916 0.9280
5.750 0.6008 0.02327 0.01560 0.0195 0.3789 0.9418
6.000 0.6489 0.02339 0.01549 0.0162 0.3672 0.9538
6.250 0.6959 0.02376 0.01599 0.0122 0.3525 0.9663
6.500 0.7453 0.02417 0.01641 0.0078 0.3389 0.9784
6.750 0.7985 0.02441 0.01649 0.0030 0.3263 0.9892
7.000 0.8425 0.02471 0.01681 -0.0008 0.3133 1.0000
7.250 0.8483 0.02512 0.01719 0.0018 0.3064 1.0000
7.500 0.8493 0.02551 0.01766 0.0051 0.2990 1.0000
7.750 0.8616 0.02574 0.01767 0.0074 0.2925 1.0000
8.000 0.8687 0.02646 0.01853 0.0098 0.2843 1.0000
8.250 0.8903 0.02683 0.01875 0.0106 0.2761 1.0000
8.500 0.9082 0.02766 0.01964 0.0116 0.2677 1.0000
8.750 0.9309 0.02815 0.02005 0.0121 0.2594 1.0000
9.000 0.9508 0.02902 0.02093 0.0128 0.2514 1.0000
9.250 0.9714 0.02967 0.02157 0.0136 0.2434 1.0000
9.500 0.9939 0.03051 0.02234 0.0140 0.2362 1.0000
9.750 1.0098 0.03141 0.02336 0.0151 0.2285 1.0000
10.000 1.0379 0.03207 0.02377 0.0151 0.2219 1.0000
10.250 1.0463 0.03336 0.02536 0.0167 0.2149 1.0000
10.500 1.0730 0.03389 0.02570 0.0169 0.2085 1.0000
10.750 1.0832 0.03537 0.02735 0.0182 0.2026 1.0000
11.000 1.0968 0.03641 0.02848 0.0193 0.1966 1.0000
11.250 1.1251 0.03724 0.02908 0.0193 0.1910 1.0000
11.500 1.1220 0.03909 0.03126 0.0215 0.1862 1.0000
11.750 1.1363 0.04010 0.03229 0.0225 0.1811 1.0000
12.000 1.1596 0.04122 0.03328 0.0227 0.1763 1.0000
12.250 1.1447 0.04346 0.03584 0.0255 0.1729 1.0000
12.500 1.1404 0.04527 0.03777 0.0275 0.1693 1.0000
12.750 1.1894 0.04546 0.03762 0.0262 0.1637 1.0000
13.000 1.1560 0.04858 0.04108 0.0292 0.1621 1.0000
13.250 1.1187 0.05294 0.04576 0.0301 0.1604 1.0000
13.500 1.0582 0.06044 0.05362 0.0283 0.1597 1.0000
14.000 1.0828 0.06360 0.05674 0.0285 0.1525 1.0000
14.250 1.0253 0.07310 0.06649 0.0242 0.1516 1.0000
14.500 0.5784 0.16458 0.15853 -0.0319 0.1949 1.0000
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