Joukovsky f=0% t=15% (joukowsk0015-jf) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: Joukovsky f=0% t=15% (joukowsk0015-jf) Reynolds number: 200,000 Max Cl/Cd: 50.78 at α=8° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-joukowsk0015-jf-200000-n5.txt Download as CSV file: xf-joukowsk0015-jf-200000-n5.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 = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-17.250 -1.1475 0.09484 0.08924 0.0008 1.0000 0.0455
-17.000 -1.1544 0.08978 0.08404 -0.0020 1.0000 0.0463
-16.750 -1.1615 0.08473 0.07883 -0.0047 1.0000 0.0471
-16.500 -1.1646 0.08059 0.07465 -0.0068 1.0000 0.0479
-16.250 -1.1683 0.07640 0.07040 -0.0089 1.0000 0.0486
-16.000 -1.1724 0.07222 0.06615 -0.0110 1.0000 0.0495
-15.750 -1.1757 0.06826 0.06209 -0.0129 1.0000 0.0504
-15.500 -1.1786 0.06447 0.05819 -0.0147 1.0000 0.0514
-15.250 -1.1809 0.06090 0.05448 -0.0162 1.0000 0.0525
-15.000 -1.1827 0.05750 0.05100 -0.0175 1.0000 0.0534
-14.750 -1.1851 0.05412 0.04758 -0.0189 1.0000 0.0544
-14.500 -1.1862 0.05096 0.04436 -0.0201 1.0000 0.0555
-14.250 -1.1859 0.04805 0.04136 -0.0210 1.0000 0.0566
-14.000 -1.1843 0.04534 0.03855 -0.0218 1.0000 0.0581
-13.750 -1.1811 0.04289 0.03597 -0.0223 1.0000 0.0595
-13.500 -1.1805 0.04027 0.03333 -0.0229 1.0000 0.0607
-13.250 -1.1780 0.03794 0.03095 -0.0232 1.0000 0.0621
-13.000 -1.1733 0.03590 0.02883 -0.0233 1.0000 0.0637
-12.750 -1.1670 0.03408 0.02691 -0.0232 1.0000 0.0656
-12.500 -1.1618 0.03227 0.02505 -0.0229 1.0000 0.0673
-12.250 -1.1567 0.03058 0.02333 -0.0225 1.0000 0.0691
-12.000 -1.1492 0.02916 0.02184 -0.0218 1.0000 0.0712
-11.750 -1.1398 0.02795 0.02054 -0.0209 1.0000 0.0736
-11.500 -1.1329 0.02672 0.01929 -0.0196 1.0000 0.0758
-11.250 -1.1245 0.02568 0.01823 -0.0181 1.0000 0.0783
-11.000 -1.1128 0.02485 0.01732 -0.0165 1.0000 0.0813
-10.750 -1.0990 0.02399 0.01644 -0.0153 1.0000 0.0842
-10.500 -1.0833 0.02318 0.01561 -0.0142 1.0000 0.0878
-10.250 -1.0646 0.02251 0.01487 -0.0134 1.0000 0.0917
-10.000 -1.0470 0.02173 0.01411 -0.0125 1.0000 0.0956
-9.750 -1.0268 0.02109 0.01344 -0.0117 1.0000 0.1004
-9.500 -1.0066 0.02042 0.01277 -0.0110 1.0000 0.1050
-9.250 -0.9852 0.01983 0.01216 -0.0104 1.0000 0.1105
-9.000 -0.9633 0.01924 0.01157 -0.0099 1.0000 0.1161
-8.750 -0.9407 0.01869 0.01103 -0.0094 1.0000 0.1226
-8.500 -0.9179 0.01815 0.01049 -0.0089 1.0000 0.1290
-8.250 -0.8942 0.01766 0.01001 -0.0084 1.0000 0.1365
-8.000 -0.8707 0.01715 0.00954 -0.0080 1.0000 0.1438
-7.750 -0.8461 0.01673 0.00911 -0.0077 1.0000 0.1520
-7.500 -0.8222 0.01625 0.00869 -0.0073 1.0000 0.1607
-7.250 -0.7975 0.01584 0.00830 -0.0070 1.0000 0.1696
-7.000 -0.7724 0.01546 0.00795 -0.0067 0.9983 0.1795
-6.750 -0.7365 0.01506 0.00759 -0.0086 0.9601 0.1913
-6.500 -0.7030 0.01472 0.00726 -0.0099 0.9337 0.2028
-6.250 -0.6743 0.01446 0.00697 -0.0100 0.9088 0.2143
-5.750 -0.6244 0.01397 0.00646 -0.0085 0.8663 0.2372
-5.500 -0.5997 0.01376 0.00622 -0.0077 0.8477 0.2488
-5.250 -0.5747 0.01357 0.00598 -0.0069 0.8301 0.2611
-5.000 -0.5496 0.01335 0.00577 -0.0062 0.8134 0.2732
-4.750 -0.5238 0.01316 0.00555 -0.0057 0.7970 0.2855
-4.500 -0.4975 0.01300 0.00535 -0.0051 0.7815 0.2984
-4.250 -0.4713 0.01282 0.00517 -0.0046 0.7666 0.3114
-4.000 -0.4448 0.01267 0.00499 -0.0041 0.7522 0.3242
-3.750 -0.4179 0.01252 0.00483 -0.0038 0.7374 0.3371
-3.250 -0.3634 0.01227 0.00454 -0.0031 0.7093 0.3638
-3.000 -0.3362 0.01216 0.00440 -0.0027 0.6955 0.3767
-2.750 -0.3084 0.01205 0.00428 -0.0025 0.6815 0.3901
-2.500 -0.2807 0.01196 0.00418 -0.0022 0.6680 0.4037
-2.250 -0.2531 0.01188 0.00408 -0.0019 0.6549 0.4168
-2.000 -0.2251 0.01180 0.00400 -0.0017 0.6409 0.4298
-1.750 -0.1969 0.01174 0.00392 -0.0015 0.6278 0.4435
-1.500 -0.1692 0.01169 0.00385 -0.0012 0.6148 0.4565
-1.250 -0.1410 0.01163 0.00381 -0.0010 0.6012 0.4696
-1.000 -0.1127 0.01160 0.00376 -0.0008 0.5880 0.4828
-0.750 -0.0847 0.01157 0.00372 -0.0006 0.5753 0.4963
-0.500 -0.0565 0.01154 0.00370 -0.0004 0.5616 0.5090
-0.250 -0.0282 0.01153 0.00368 -0.0002 0.5487 0.5223
0.000 0.0000 0.01154 0.00367 0.0000 0.5357 0.5357
0.250 0.0282 0.01153 0.00368 0.0002 0.5223 0.5486
0.500 0.0565 0.01154 0.00370 0.0004 0.5090 0.5616
0.750 0.0847 0.01157 0.00372 0.0006 0.4962 0.5753
1.000 0.1127 0.01160 0.00376 0.0008 0.4828 0.5880
1.250 0.1410 0.01163 0.00381 0.0010 0.4695 0.6012
1.500 0.1692 0.01169 0.00385 0.0012 0.4565 0.6148
1.750 0.1970 0.01174 0.00392 0.0015 0.4435 0.6279
2.000 0.2251 0.01180 0.00400 0.0017 0.4297 0.6410
2.250 0.2531 0.01188 0.00408 0.0019 0.4168 0.6550
2.500 0.2807 0.01196 0.00418 0.0022 0.4037 0.6680
2.750 0.3084 0.01205 0.00429 0.0025 0.3902 0.6815
3.000 0.3362 0.01216 0.00440 0.0027 0.3767 0.6955
3.250 0.3634 0.01227 0.00454 0.0031 0.3638 0.7094
3.750 0.4179 0.01252 0.00483 0.0038 0.3371 0.7374
4.000 0.4448 0.01267 0.00499 0.0041 0.3242 0.7522
4.250 0.4713 0.01282 0.00517 0.0046 0.3114 0.7666
4.500 0.4975 0.01300 0.00535 0.0051 0.2984 0.7815
4.750 0.5238 0.01316 0.00555 0.0057 0.2855 0.7970
5.000 0.5496 0.01335 0.00577 0.0062 0.2732 0.8134
5.250 0.5747 0.01357 0.00598 0.0069 0.2611 0.8301
5.500 0.5997 0.01376 0.00622 0.0077 0.2487 0.8477
5.750 0.6244 0.01397 0.00646 0.0085 0.2372 0.8663
6.250 0.6743 0.01446 0.00697 0.0100 0.2143 0.9088
6.500 0.7030 0.01472 0.00726 0.0099 0.2028 0.9336
6.750 0.7365 0.01506 0.00759 0.0086 0.1913 0.9601
7.000 0.7724 0.01546 0.00795 0.0067 0.1795 0.9984
7.250 0.7975 0.01584 0.00830 0.0070 0.1696 1.0000
7.500 0.8222 0.01625 0.00869 0.0073 0.1608 1.0000
7.750 0.8461 0.01673 0.00910 0.0077 0.1520 1.0000
8.000 0.8708 0.01715 0.00954 0.0080 0.1438 1.0000
8.250 0.8942 0.01766 0.01001 0.0084 0.1364 1.0000
8.500 0.9179 0.01815 0.01049 0.0089 0.1290 1.0000
8.750 0.9407 0.01869 0.01103 0.0093 0.1226 1.0000
9.000 0.9633 0.01924 0.01157 0.0099 0.1161 1.0000
9.250 0.9852 0.01983 0.01216 0.0104 0.1105 1.0000
9.500 1.0066 0.02042 0.01277 0.0110 0.1050 1.0000
9.750 1.0269 0.02109 0.01343 0.0117 0.1003 1.0000
10.000 1.0470 0.02172 0.01411 0.0125 0.0955 1.0000
10.250 1.0646 0.02250 0.01487 0.0134 0.0917 1.0000
10.500 1.0834 0.02318 0.01561 0.0142 0.0877 1.0000
10.750 1.0991 0.02399 0.01643 0.0153 0.0842 1.0000
11.000 1.1130 0.02485 0.01732 0.0165 0.0812 1.0000
11.250 1.1247 0.02568 0.01822 0.0180 0.0783 1.0000
11.500 1.1330 0.02672 0.01929 0.0196 0.0758 1.0000
11.750 1.1401 0.02795 0.02053 0.0208 0.0736 1.0000
12.000 1.1496 0.02915 0.02183 0.0217 0.0712 1.0000
12.250 1.1571 0.03057 0.02332 0.0224 0.0691 1.0000
12.500 1.1623 0.03227 0.02504 0.0229 0.0673 1.0000
12.750 1.1677 0.03406 0.02689 0.0231 0.0656 1.0000
13.000 1.1741 0.03588 0.02881 0.0232 0.0637 1.0000
13.250 1.1788 0.03793 0.03093 0.0231 0.0620 1.0000
13.500 1.1814 0.04025 0.03331 0.0228 0.0606 1.0000
14.000 1.1853 0.04531 0.03852 0.0217 0.0580 1.0000
14.250 1.1870 0.04801 0.04132 0.0209 0.0566 1.0000
14.500 1.1874 0.05091 0.04430 0.0200 0.0554 1.0000
14.750 1.1864 0.05406 0.04751 0.0188 0.0543 1.0000
15.000 1.1839 0.05744 0.05093 0.0174 0.0534 1.0000
15.250 1.1820 0.06084 0.05442 0.0161 0.0524 1.0000
15.500 1.1800 0.06437 0.05809 0.0146 0.0514 1.0000
15.750 1.1771 0.06818 0.06201 0.0128 0.0504 1.0000
16.000 1.1739 0.07213 0.06605 0.0109 0.0495 1.0000
16.250 1.1699 0.07630 0.07030 0.0088 0.0486 1.0000
16.500 1.1662 0.08048 0.07453 0.0067 0.0478 1.0000
16.750 1.1624 0.08475 0.07885 0.0045 0.0470 1.0000
17.000 1.1561 0.08966 0.08392 0.0019 0.0462 1.0000
17.250 1.1491 0.09477 0.08917 -0.0009 0.0454 1.0000
17.500 1.1420 0.10000 0.09452 -0.0039 0.0446 1.0000
17.750 1.1354 0.10521 0.09982 -0.0068 0.0439 1.0000
18.000 1.1295 0.11038 0.10508 -0.0098 0.0432 1.0000
18.250 1.1255 0.11521 0.10996 -0.0125 0.0426 1.0000
18.500 1.1232 0.11971 0.11449 -0.0151 0.0419 1.0000
18.750 1.1057 0.12756 0.12255 -0.0200 0.0413 1.0000
19.000 1.0833 0.13667 0.13187 -0.0258 0.0406 1.0000
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