Joukovsky f=0% t=18% (joukowsk0018-jf) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: Joukovsky f=0% t=18% (joukowsk0018-jf) Reynolds number: 500,000 Max Cl/Cd: 67.21 at α=9.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-joukowsk0018-jf-500000-n5.txt Download as CSV file: xf-joukowsk0018-jf-500000-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 = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.250 -1.2541 0.08581 0.08085 -0.0078 1.0000 0.0521
-18.000 -1.2616 0.08113 0.07611 -0.0101 1.0000 0.0529
-17.750 -1.2677 0.07674 0.07165 -0.0122 1.0000 0.0538
-17.500 -1.2721 0.07270 0.06754 -0.0140 1.0000 0.0548
-17.250 -1.2751 0.06892 0.06368 -0.0156 1.0000 0.0558
-17.000 -1.2772 0.06532 0.05999 -0.0171 1.0000 0.0567
-16.750 -1.2824 0.06141 0.05602 -0.0187 1.0000 0.0576
-16.500 -1.2875 0.05762 0.05217 -0.0201 1.0000 0.0587
-16.250 -1.2902 0.05421 0.04870 -0.0213 1.0000 0.0599
-16.000 -1.2912 0.05111 0.04553 -0.0223 1.0000 0.0610
-15.750 -1.2904 0.04830 0.04265 -0.0231 1.0000 0.0622
-15.500 -1.2919 0.04535 0.03963 -0.0238 1.0000 0.0632
-15.250 -1.2935 0.04246 0.03669 -0.0244 1.0000 0.0645
-15.000 -1.2927 0.03989 0.03407 -0.0249 1.0000 0.0659
-14.750 -1.2897 0.03759 0.03172 -0.0251 1.0000 0.0673
-14.500 -1.2848 0.03555 0.02960 -0.0252 1.0000 0.0688
-14.250 -1.2827 0.03330 0.02732 -0.0253 1.0000 0.0702
-14.000 -1.2783 0.03133 0.02531 -0.0252 1.0000 0.0718
-13.750 -1.2718 0.02960 0.02354 -0.0250 1.0000 0.0736
-13.500 -1.2635 0.02809 0.02197 -0.0246 1.0000 0.0753
-13.250 -1.2574 0.02647 0.02032 -0.0241 1.0000 0.0770
-13.000 -1.2497 0.02504 0.01887 -0.0235 1.0000 0.0791
-12.750 -1.2399 0.02384 0.01763 -0.0228 1.0000 0.0813
-12.500 -1.2298 0.02272 0.01648 -0.0219 1.0000 0.0834
-12.250 -1.2210 0.02161 0.01535 -0.0208 1.0000 0.0857
-12.000 -1.2100 0.02070 0.01442 -0.0196 1.0000 0.0882
-11.750 -1.1978 0.01993 0.01363 -0.0183 1.0000 0.0907
-11.500 -1.1882 0.01912 0.01282 -0.0166 1.0000 0.0933
-11.250 -1.1764 0.01850 0.01218 -0.0148 1.0000 0.0962
-10.750 -1.1453 0.01742 0.01110 -0.0118 1.0000 0.1023
-10.500 -1.1255 0.01694 0.01062 -0.0109 1.0000 0.1060
-10.250 -1.0951 0.01648 0.01012 -0.0120 0.9288 0.1102
-10.000 -1.0779 0.01614 0.00971 -0.0103 0.8939 0.1142
-9.750 -1.0587 0.01584 0.00933 -0.0088 0.8696 0.1180
-9.500 -1.0391 0.01547 0.00891 -0.0075 0.8495 0.1225
-9.250 -1.0172 0.01517 0.00855 -0.0066 0.8324 0.1271
-9.000 -0.9951 0.01483 0.00817 -0.0056 0.8162 0.1317
-8.750 -0.9716 0.01452 0.00782 -0.0050 0.8012 0.1372
-8.500 -0.9478 0.01421 0.00748 -0.0043 0.7875 0.1424
-8.250 -0.9235 0.01393 0.00716 -0.0037 0.7739 0.1482
-8.000 -0.8984 0.01364 0.00685 -0.0033 0.7609 0.1537
-7.750 -0.8732 0.01337 0.00655 -0.0028 0.7488 0.1601
-7.500 -0.8474 0.01312 0.00627 -0.0024 0.7362 0.1661
-7.250 -0.8215 0.01285 0.00599 -0.0021 0.7248 0.1730
-7.000 -0.7951 0.01263 0.00574 -0.0017 0.7127 0.1795
-6.750 -0.7686 0.01238 0.00549 -0.0015 0.7018 0.1869
-6.500 -0.7417 0.01218 0.00525 -0.0012 0.6901 0.1938
-6.250 -0.7148 0.01195 0.00503 -0.0010 0.6794 0.2017
-6.000 -0.6874 0.01177 0.00482 -0.0008 0.6681 0.2089
-5.750 -0.6601 0.01157 0.00462 -0.0006 0.6578 0.2172
-5.500 -0.6324 0.01140 0.00443 -0.0005 0.6467 0.2249
-5.250 -0.6047 0.01122 0.00424 -0.0003 0.6368 0.2335
-5.000 -0.5767 0.01106 0.00407 -0.0002 0.6257 0.2415
-4.750 -0.5487 0.01090 0.00391 -0.0001 0.6159 0.2504
-4.500 -0.5204 0.01076 0.00376 -0.0001 0.6053 0.2586
-4.250 -0.4922 0.01063 0.00362 0.0000 0.5952 0.2678
-4.000 -0.4637 0.01050 0.00349 0.0001 0.5849 0.2763
-3.750 -0.4353 0.01039 0.00336 0.0001 0.5747 0.2857
-3.500 -0.4065 0.01027 0.00325 0.0002 0.5647 0.2944
-3.250 -0.3780 0.01018 0.00315 0.0002 0.5545 0.3039
-3.000 -0.3490 0.01008 0.00305 0.0002 0.5448 0.3126
-2.750 -0.3203 0.00999 0.00296 0.0002 0.5345 0.3225
-2.500 -0.2913 0.00992 0.00288 0.0002 0.5250 0.3313
-2.250 -0.2624 0.00984 0.00281 0.0002 0.5146 0.3412
-2.000 -0.2333 0.00979 0.00275 0.0002 0.5054 0.3501
-1.750 -0.2043 0.00972 0.00269 0.0002 0.4951 0.3601
-1.500 -0.1751 0.00969 0.00264 0.0002 0.4857 0.3693
-1.250 -0.1460 0.00963 0.00260 0.0001 0.4756 0.3791
-1.000 -0.1168 0.00963 0.00256 0.0001 0.4660 0.3882
-0.750 -0.0877 0.00958 0.00254 0.0001 0.4562 0.3982
-0.500 -0.0584 0.00959 0.00252 0.0001 0.4464 0.4075
-0.250 -0.0292 0.00955 0.00251 0.0000 0.4369 0.4175
0.000 0.0000 0.00958 0.00250 0.0000 0.4269 0.4269
0.250 0.0292 0.00955 0.00251 0.0000 0.4175 0.4369
0.500 0.0584 0.00959 0.00252 -0.0001 0.4075 0.4464
0.750 0.0876 0.00958 0.00254 -0.0001 0.3982 0.4562
1.000 0.1168 0.00963 0.00256 -0.0001 0.3882 0.4660
1.250 0.1460 0.00963 0.00260 -0.0001 0.3791 0.4755
1.500 0.1751 0.00969 0.00264 -0.0002 0.3691 0.4857
1.750 0.2042 0.00972 0.00269 -0.0002 0.3600 0.4950
2.000 0.2332 0.00979 0.00275 -0.0002 0.3502 0.5054
2.250 0.2623 0.00984 0.00281 -0.0002 0.3412 0.5146
2.500 0.2912 0.00992 0.00288 -0.0002 0.3313 0.5250
2.750 0.3203 0.00999 0.00296 -0.0002 0.3225 0.5345
3.000 0.3490 0.01008 0.00305 -0.0002 0.3127 0.5448
3.250 0.3779 0.01017 0.00314 -0.0002 0.3040 0.5545
3.500 0.4065 0.01027 0.00325 -0.0002 0.2944 0.5647
3.750 0.4353 0.01039 0.00336 -0.0001 0.2858 0.5747
4.000 0.4636 0.01050 0.00349 -0.0001 0.2763 0.5851
4.250 0.4922 0.01063 0.00362 0.0000 0.2678 0.5952
4.500 0.5204 0.01076 0.00376 0.0001 0.2587 0.6052
4.750 0.5487 0.01090 0.00391 0.0001 0.2504 0.6158
5.000 0.5766 0.01106 0.00407 0.0002 0.2415 0.6257
5.250 0.6047 0.01122 0.00424 0.0003 0.2335 0.6368
5.500 0.6323 0.01140 0.00443 0.0005 0.2249 0.6467
5.750 0.6601 0.01157 0.00462 0.0006 0.2172 0.6579
6.000 0.6874 0.01177 0.00482 0.0008 0.2090 0.6682
6.250 0.7148 0.01195 0.00503 0.0010 0.2018 0.6794
6.500 0.7417 0.01218 0.00525 0.0012 0.1939 0.6901
6.750 0.7686 0.01238 0.00549 0.0015 0.1870 0.7018
7.000 0.7950 0.01263 0.00574 0.0018 0.1795 0.7127
7.250 0.8215 0.01285 0.00599 0.0021 0.1730 0.7249
7.500 0.8473 0.01312 0.00627 0.0024 0.1661 0.7361
7.750 0.8732 0.01337 0.00655 0.0028 0.1601 0.7488
8.000 0.8983 0.01364 0.00685 0.0033 0.1537 0.7610
8.250 0.9235 0.01392 0.00715 0.0037 0.1482 0.7739
8.500 0.9477 0.01421 0.00748 0.0043 0.1423 0.7874
8.750 0.9716 0.01452 0.00782 0.0050 0.1371 0.8012
9.000 0.9951 0.01483 0.00817 0.0057 0.1318 0.8163
9.250 1.0171 0.01517 0.00855 0.0066 0.1270 0.8322
9.500 1.0391 0.01546 0.00891 0.0075 0.1225 0.8494
9.750 1.0587 0.01584 0.00933 0.0088 0.1180 0.8694
10.000 1.0779 0.01614 0.00971 0.0103 0.1142 0.8941
10.250 1.0952 0.01648 0.01012 0.0120 0.1102 0.9289
10.500 1.1257 0.01694 0.01062 0.0109 0.1060 1.0000
10.750 1.1453 0.01742 0.01110 0.0118 0.1023 1.0000
11.250 1.1766 0.01850 0.01218 0.0147 0.0960 1.0000
11.500 1.1885 0.01912 0.01281 0.0165 0.0932 1.0000
12.000 1.2105 0.02069 0.01441 0.0196 0.0882 1.0000
12.250 1.2213 0.02160 0.01535 0.0207 0.0856 1.0000
12.500 1.2304 0.02271 0.01646 0.0218 0.0834 1.0000
12.750 1.2405 0.02382 0.01761 0.0227 0.0814 1.0000
13.000 1.2503 0.02502 0.01885 0.0234 0.0791 1.0000
13.250 1.2582 0.02643 0.02028 0.0241 0.0771 1.0000
13.500 1.2643 0.02806 0.02194 0.0245 0.0753 1.0000
13.750 1.2727 0.02956 0.02350 0.0249 0.0736 1.0000
14.000 1.2792 0.03129 0.02527 0.0251 0.0718 1.0000
14.250 1.2836 0.03326 0.02727 0.0252 0.0702 1.0000
14.500 1.2859 0.03549 0.02954 0.0252 0.0687 1.0000
14.750 1.2910 0.03753 0.03165 0.0250 0.0672 1.0000
15.000 1.2937 0.03985 0.03402 0.0248 0.0657 1.0000
15.250 1.2948 0.04239 0.03662 0.0243 0.0644 1.0000
15.500 1.2933 0.04527 0.03955 0.0237 0.0632 1.0000
15.750 1.2924 0.04816 0.04250 0.0230 0.0621 1.0000
16.000 1.2929 0.05100 0.04542 0.0222 0.0610 1.0000
16.250 1.2919 0.05411 0.04859 0.0212 0.0598 1.0000
16.500 1.2895 0.05747 0.05202 0.0200 0.0587 1.0000
16.750 1.2849 0.06122 0.05582 0.0186 0.0577 1.0000
17.000 1.2790 0.06521 0.05988 0.0170 0.0567 1.0000
17.250 1.2772 0.06877 0.06353 0.0155 0.0557 1.0000
17.500 1.2743 0.07253 0.06736 0.0139 0.0547 1.0000
17.750 1.2699 0.07657 0.07147 0.0121 0.0538 1.0000
18.000 1.2637 0.08097 0.07594 0.0100 0.0529 1.0000
18.250 1.2562 0.08564 0.08068 0.0077 0.0521 1.0000
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