Joukovsky f=0% t=18% (joukowsk0018-jf) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: Joukovsky f=0% t=18% (joukowsk0018-jf) Reynolds number: 200,000 Max Cl/Cd: 49.81 at α=9° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-joukowsk0018-jf-200000-n5.txt Download as CSV file: xf-joukowsk0018-jf-200000-n5.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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.1163 0.13017 0.12480 0.0144 1.0000 0.0609
-19.500 -1.1309 0.12340 0.11786 0.0102 1.0000 0.0622
-19.250 -1.1320 0.11930 0.11371 0.0079 1.0000 0.0633
-19.000 -1.1327 0.11528 0.10967 0.0056 1.0000 0.0644
-18.750 -1.1368 0.11067 0.10499 0.0030 1.0000 0.0657
-18.500 -1.1432 0.10568 0.09989 0.0002 1.0000 0.0670
-18.250 -1.1501 0.10065 0.09472 -0.0025 1.0000 0.0684
-18.000 -1.1514 0.09672 0.09075 -0.0045 1.0000 0.0697
-17.750 -1.1532 0.09274 0.08673 -0.0066 1.0000 0.0709
-17.500 -1.1564 0.08857 0.08249 -0.0087 1.0000 0.0723
-17.250 -1.1594 0.08446 0.07828 -0.0107 1.0000 0.0738
-17.000 -1.1628 0.08033 0.07401 -0.0127 1.0000 0.0753
-16.750 -1.1634 0.07683 0.07050 -0.0143 1.0000 0.0767
-16.500 -1.1650 0.07317 0.06680 -0.0160 1.0000 0.0781
-16.250 -1.1668 0.06954 0.06309 -0.0176 1.0000 0.0798
-16.000 -1.1672 0.06617 0.05962 -0.0190 1.0000 0.0815
-15.750 -1.1671 0.06297 0.05634 -0.0202 1.0000 0.0832
-15.500 -1.1683 0.05971 0.05307 -0.0215 1.0000 0.0848
-15.250 -1.1687 0.05661 0.04991 -0.0226 1.0000 0.0866
-15.000 -1.1674 0.05379 0.04700 -0.0235 1.0000 0.0885
-14.750 -1.1650 0.05117 0.04429 -0.0242 1.0000 0.0906
-14.500 -1.1653 0.04839 0.04150 -0.0250 1.0000 0.0924
-14.250 -1.1640 0.04581 0.03888 -0.0256 1.0000 0.0944
-14.000 -1.1606 0.04351 0.03650 -0.0260 1.0000 0.0967
-13.750 -1.1555 0.04140 0.03431 -0.0263 1.0000 0.0991
-13.500 -1.1534 0.03912 0.03202 -0.0265 1.0000 0.1011
-13.250 -1.1491 0.03707 0.02994 -0.0266 1.0000 0.1036
-13.000 -1.1422 0.03530 0.02809 -0.0266 1.0000 0.1064
-12.750 -1.1361 0.03354 0.02629 -0.0264 1.0000 0.1091
-12.500 -1.1306 0.03180 0.02454 -0.0262 1.0000 0.1117
-12.250 -1.1225 0.03032 0.02302 -0.0258 1.0000 0.1149
-12.000 -1.1128 0.02900 0.02163 -0.0253 1.0000 0.1181
-11.750 -1.1060 0.02758 0.02023 -0.0246 1.0000 0.1211
-11.500 -1.0963 0.02641 0.01902 -0.0238 1.0000 0.1247
-11.250 -1.0845 0.02542 0.01798 -0.0230 1.0000 0.1284
-11.000 -1.0761 0.02433 0.01691 -0.0218 1.0000 0.1319
-10.750 -1.0649 0.02346 0.01602 -0.0205 1.0000 0.1360
-10.500 -1.0525 0.02271 0.01523 -0.0192 1.0000 0.1402
-10.250 -1.0421 0.02195 0.01451 -0.0174 1.0000 0.1442
-10.000 -1.0266 0.02136 0.01389 -0.0161 1.0000 0.1492
-9.750 -1.0098 0.02074 0.01328 -0.0151 1.0000 0.1540
-9.500 -0.9915 0.02016 0.01272 -0.0142 1.0000 0.1594
-9.250 -0.9712 0.01966 0.01221 -0.0134 1.0000 0.1650
-9.000 -0.9517 0.01911 0.01171 -0.0127 1.0000 0.1708
-8.750 -0.9196 0.01866 0.01122 -0.0141 0.9535 0.1780
-8.500 -0.8913 0.01818 0.01075 -0.0147 0.9210 0.1851
-8.000 -0.8479 0.01750 0.00998 -0.0126 0.8738 0.1986
-7.750 -0.8262 0.01723 0.00962 -0.0115 0.8550 0.2058
-7.500 -0.8053 0.01690 0.00927 -0.0103 0.8381 0.2127
-7.250 -0.7823 0.01662 0.00894 -0.0094 0.8222 0.2206
-7.000 -0.7594 0.01632 0.00862 -0.0085 0.8074 0.2279
-6.750 -0.7357 0.01607 0.00830 -0.0077 0.7939 0.2362
-6.500 -0.7115 0.01579 0.00801 -0.0070 0.7802 0.2440
-6.250 -0.6866 0.01555 0.00773 -0.0064 0.7673 0.2527
-6.000 -0.6618 0.01531 0.00745 -0.0058 0.7549 0.2608
-5.750 -0.6359 0.01509 0.00721 -0.0053 0.7423 0.2700
-5.500 -0.6105 0.01488 0.00695 -0.0048 0.7308 0.2784
-5.250 -0.5839 0.01468 0.00673 -0.0044 0.7185 0.2879
-5.000 -0.5579 0.01449 0.00651 -0.0040 0.7074 0.2967
-4.750 -0.5309 0.01431 0.00631 -0.0037 0.6954 0.3064
-4.500 -0.5043 0.01414 0.00612 -0.0033 0.6848 0.3153
-4.250 -0.4769 0.01398 0.00594 -0.0031 0.6729 0.3253
-4.000 -0.4500 0.01384 0.00577 -0.0027 0.6626 0.3344
-3.750 -0.4223 0.01370 0.00562 -0.0025 0.6510 0.3445
-3.500 -0.3950 0.01357 0.00546 -0.0022 0.6408 0.3537
-3.250 -0.3670 0.01345 0.00534 -0.0021 0.6295 0.3640
-2.750 -0.3113 0.01325 0.00510 -0.0017 0.6082 0.3837
-2.500 -0.2836 0.01316 0.00499 -0.0014 0.5980 0.3931
-2.250 -0.2552 0.01308 0.00491 -0.0013 0.5871 0.4036
-2.000 -0.2272 0.01301 0.00482 -0.0011 0.5768 0.4131
-1.750 -0.1988 0.01294 0.00475 -0.0010 0.5663 0.4236
-1.500 -0.1707 0.01289 0.00469 -0.0008 0.5559 0.4333
-1.250 -0.1421 0.01284 0.00464 -0.0007 0.5457 0.4437
-1.000 -0.1139 0.01280 0.00459 -0.0005 0.5351 0.4534
-0.750 -0.0853 0.01278 0.00456 -0.0004 0.5252 0.4639
-0.500 -0.0570 0.01275 0.00454 -0.0002 0.5145 0.4738
-0.250 -0.0285 0.01274 0.00453 -0.0001 0.5046 0.4842
0.000 0.0000 0.01274 0.00452 0.0000 0.4941 0.4941
0.250 0.0284 0.01274 0.00453 0.0001 0.4842 0.5047
0.500 0.0570 0.01275 0.00454 0.0003 0.4738 0.5145
0.750 0.0853 0.01278 0.00456 0.0004 0.4639 0.5251
1.000 0.1139 0.01280 0.00459 0.0005 0.4534 0.5351
1.250 0.1421 0.01284 0.00464 0.0007 0.4437 0.5457
1.500 0.1706 0.01289 0.00469 0.0008 0.4332 0.5559
1.750 0.1987 0.01294 0.00475 0.0010 0.4236 0.5663
2.000 0.2272 0.01301 0.00482 0.0011 0.4131 0.5768
2.250 0.2551 0.01308 0.00491 0.0013 0.4036 0.5871
2.500 0.2835 0.01316 0.00499 0.0014 0.3931 0.5980
2.750 0.3113 0.01325 0.00510 0.0017 0.3838 0.6083
3.250 0.3670 0.01345 0.00534 0.0021 0.3640 0.6295
3.500 0.3950 0.01357 0.00546 0.0022 0.3538 0.6408
3.750 0.4222 0.01370 0.00562 0.0025 0.3445 0.6510
4.000 0.4500 0.01383 0.00577 0.0027 0.3344 0.6625
4.250 0.4769 0.01398 0.00594 0.0031 0.3253 0.6729
4.500 0.5043 0.01414 0.00612 0.0033 0.3154 0.6848
4.750 0.5308 0.01431 0.00631 0.0037 0.3064 0.6954
5.000 0.5579 0.01449 0.00651 0.0040 0.2967 0.7074
5.250 0.5839 0.01467 0.00673 0.0044 0.2879 0.7185
5.500 0.6105 0.01488 0.00695 0.0048 0.2784 0.7308
5.750 0.6359 0.01509 0.00721 0.0053 0.2700 0.7423
6.000 0.6618 0.01531 0.00745 0.0058 0.2609 0.7548
6.250 0.6865 0.01555 0.00773 0.0064 0.2527 0.7673
6.500 0.7115 0.01579 0.00801 0.0070 0.2440 0.7801
6.750 0.7356 0.01607 0.00830 0.0077 0.2362 0.7939
7.000 0.7593 0.01632 0.00862 0.0085 0.2279 0.8074
7.250 0.7822 0.01662 0.00894 0.0094 0.2205 0.8222
7.500 0.8053 0.01690 0.00927 0.0103 0.2127 0.8381
7.750 0.8262 0.01723 0.00962 0.0115 0.2058 0.8550
8.000 0.8479 0.01750 0.00998 0.0126 0.1986 0.8737
8.500 0.8913 0.01818 0.01075 0.0146 0.1851 0.9211
8.750 0.9197 0.01866 0.01122 0.0140 0.1780 0.9536
9.000 0.9518 0.01911 0.01170 0.0127 0.1708 1.0000
9.250 0.9713 0.01966 0.01221 0.0134 0.1650 1.0000
9.500 0.9917 0.02016 0.01272 0.0141 0.1594 1.0000
9.750 1.0099 0.02074 0.01328 0.0150 0.1540 1.0000
10.000 1.0268 0.02136 0.01389 0.0161 0.1491 1.0000
10.250 1.0424 0.02195 0.01451 0.0174 0.1442 1.0000
10.500 1.0528 0.02271 0.01523 0.0191 0.1401 1.0000
10.750 1.0652 0.02345 0.01601 0.0205 0.1359 1.0000
11.000 1.0765 0.02432 0.01690 0.0217 0.1318 1.0000
11.250 1.0848 0.02541 0.01797 0.0229 0.1283 1.0000
11.500 1.0968 0.02640 0.01902 0.0237 0.1247 1.0000
11.750 1.1066 0.02757 0.02021 0.0245 0.1211 1.0000
12.000 1.1135 0.02899 0.02162 0.0252 0.1181 1.0000
12.250 1.1233 0.03030 0.02299 0.0257 0.1149 1.0000
12.500 1.1313 0.03178 0.02452 0.0261 0.1117 1.0000
12.750 1.1369 0.03351 0.02626 0.0263 0.1090 1.0000
13.000 1.1431 0.03527 0.02806 0.0265 0.1064 1.0000
13.250 1.1501 0.03703 0.02990 0.0265 0.1036 1.0000
13.500 1.1543 0.03909 0.03199 0.0264 0.1011 1.0000
13.750 1.1564 0.04138 0.03428 0.0262 0.0990 1.0000
14.000 1.1617 0.04347 0.03645 0.0259 0.0966 1.0000
14.250 1.1651 0.04578 0.03884 0.0255 0.0943 1.0000
14.500 1.1665 0.04836 0.04146 0.0249 0.0923 1.0000
14.750 1.1663 0.05112 0.04423 0.0241 0.0906 1.0000
15.000 1.1687 0.05373 0.04695 0.0234 0.0884 1.0000
15.250 1.1702 0.05655 0.04984 0.0225 0.0865 1.0000
15.500 1.1698 0.05964 0.05299 0.0214 0.0847 1.0000
15.750 1.1688 0.06287 0.05624 0.0201 0.0832 1.0000
16.000 1.1689 0.06608 0.05953 0.0188 0.0814 1.0000
16.250 1.1687 0.06943 0.06298 0.0175 0.0797 1.0000
16.500 1.1667 0.07308 0.06671 0.0158 0.0780 1.0000
16.750 1.1651 0.07673 0.07039 0.0142 0.0766 1.0000
17.000 1.1647 0.08019 0.07386 0.0126 0.0753 1.0000
17.250 1.1614 0.08431 0.07812 0.0106 0.0737 1.0000
17.500 1.1581 0.08846 0.08238 0.0086 0.0722 1.0000
17.750 1.1555 0.09256 0.08654 0.0065 0.0709 1.0000
18.000 1.1533 0.09660 0.09062 0.0044 0.0696 1.0000
18.250 1.1524 0.10044 0.09449 0.0025 0.0684 1.0000
18.500 1.1452 0.10556 0.09976 -0.0003 0.0670 1.0000
18.750 1.1389 0.11054 0.10485 -0.0031 0.0656 1.0000
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