Joukovsky f=0% t=21% (joukowsk0021-jf) Xfoil prediction polar at RE=100,000 Ncrit=5
| Details | Polar file |
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Airfoil: Joukovsky f=0% t=21% (joukowsk0021-jf) Reynolds number: 100,000 Max Cl/Cd: 32.4 at α=9.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-joukowsk0021-jf-100000-n5.txt Download as CSV file: xf-joukowsk0021-jf-100000-n5.csv |
XFOIL Version 6.96
Calculated polar for: Joukovsky f=0% t=21%
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.100 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-16.000 -0.9698 0.08798 0.08051 -0.0173 1.0000 0.1383
-15.750 -0.9319 0.09038 0.08306 -0.0155 1.0000 0.1399
-15.500 -0.9199 0.08873 0.08144 -0.0160 1.0000 0.1425
-15.250 -0.9982 0.07382 0.06610 -0.0238 1.0000 0.1476
-15.000 -1.0036 0.06992 0.06214 -0.0254 1.0000 0.1505
-14.750 -0.9927 0.06828 0.06055 -0.0258 1.0000 0.1534
-14.500 -1.0032 0.06392 0.05608 -0.0276 1.0000 0.1568
-14.250 -1.0265 0.05827 0.05018 -0.0298 1.0000 0.1604
-14.000 -1.0157 0.05675 0.04873 -0.0300 1.0000 0.1633
-13.750 -1.0104 0.05467 0.04665 -0.0304 1.0000 0.1665
-13.500 -1.0159 0.05146 0.04333 -0.0313 1.0000 0.1702
-13.250 -1.0239 0.04812 0.03984 -0.0320 1.0000 0.1739
-13.000 -1.0110 0.04692 0.03873 -0.0319 1.0000 0.1771
-12.750 -1.0067 0.04495 0.03673 -0.0321 1.0000 0.1808
-12.500 -1.0091 0.04241 0.03407 -0.0323 1.0000 0.1850
-12.250 -1.0027 0.04072 0.03237 -0.0321 1.0000 0.1887
-12.000 -0.9930 0.03938 0.03106 -0.0319 1.0000 0.1924
-11.750 -0.9886 0.03764 0.02927 -0.0316 1.0000 0.1967
-11.500 -0.9869 0.03576 0.02729 -0.0313 1.0000 0.2012
-11.250 -0.9731 0.03483 0.02645 -0.0308 1.0000 0.2051
-11.000 -0.9647 0.03358 0.02519 -0.0302 1.0000 0.2096
-10.750 -0.9598 0.03214 0.02366 -0.0295 1.0000 0.2146
-10.500 -0.9466 0.03125 0.02284 -0.0288 1.0000 0.2188
-10.250 -0.9355 0.03033 0.02196 -0.0280 1.0000 0.2235
-10.000 -0.9275 0.02931 0.02088 -0.0270 1.0000 0.2287
-9.750 -0.9155 0.02853 0.02015 -0.0260 1.0000 0.2335
-9.500 -0.9037 0.02790 0.01960 -0.0248 1.0000 0.2382
-9.250 -0.8783 0.02714 0.01873 -0.0262 0.9486 0.2451
-9.000 -0.8506 0.02657 0.01817 -0.0271 0.9195 0.2510
-8.750 -0.8309 0.02611 0.01765 -0.0264 0.8953 0.2569
-8.500 -0.8170 0.02559 0.01695 -0.0248 0.8743 0.2633
-8.250 -0.7991 0.02526 0.01667 -0.0232 0.8565 0.2685
-8.000 -0.7826 0.02490 0.01625 -0.0216 0.8406 0.2746
-7.750 -0.7672 0.02446 0.01564 -0.0199 0.8263 0.2813
-7.500 -0.7469 0.02417 0.01542 -0.0187 0.8121 0.2868
-7.250 -0.7277 0.02384 0.01502 -0.0174 0.7993 0.2935
-7.000 -0.7085 0.02346 0.01455 -0.0161 0.7872 0.3003
-6.750 -0.6864 0.02320 0.01433 -0.0151 0.7750 0.3065
-6.500 -0.6659 0.02289 0.01391 -0.0139 0.7639 0.3138
-6.250 -0.6434 0.02260 0.01360 -0.0131 0.7526 0.3205
-6.000 -0.6208 0.02236 0.01335 -0.0121 0.7417 0.3273
-5.750 -0.5986 0.02206 0.01293 -0.0113 0.7313 0.3353
-5.500 -0.5741 0.02185 0.01277 -0.0106 0.7205 0.3418
-5.250 -0.5507 0.02163 0.01249 -0.0097 0.7113 0.3493
-5.000 -0.5263 0.02138 0.01219 -0.0092 0.7001 0.3572
-4.750 -0.5017 0.02121 0.01203 -0.0083 0.6912 0.3641
-4.500 -0.4769 0.02100 0.01176 -0.0078 0.6809 0.3723
-4.250 -0.4516 0.02082 0.01158 -0.0072 0.6710 0.3795
-4.000 -0.4263 0.02067 0.01140 -0.0066 0.6625 0.3873
-3.750 -0.4008 0.02048 0.01113 -0.0062 0.6520 0.3959
-3.500 -0.3748 0.02036 0.01105 -0.0055 0.6433 0.4028
-3.250 -0.3488 0.02023 0.01088 -0.0051 0.6338 0.4113
-3.000 -0.3225 0.02009 0.01073 -0.0047 0.6242 0.4191
-2.750 -0.2964 0.01999 0.01059 -0.0040 0.6165 0.4269
-2.500 -0.2698 0.01987 0.01044 -0.0038 0.6062 0.4360
-2.250 -0.2430 0.01979 0.01039 -0.0033 0.5974 0.4431
-2.000 -0.2164 0.01972 0.01029 -0.0029 0.5889 0.4517
-1.750 -0.1895 0.01962 0.01017 -0.0026 0.5792 0.4602
-1.500 -0.1626 0.01957 0.01012 -0.0021 0.5714 0.4678
-1.250 -0.1356 0.01952 0.01005 -0.0018 0.5619 0.4770
-1.000 -0.1085 0.01947 0.01002 -0.0014 0.5530 0.4846
-0.750 -0.0815 0.01945 0.00996 -0.0010 0.5454 0.4931
-0.500 -0.0544 0.01941 0.00991 -0.0008 0.5355 0.5025
-0.250 -0.0272 0.01940 0.00993 -0.0003 0.5274 0.5098
0.000 0.0000 0.01941 0.00992 0.0000 0.5190 0.5190
0.250 0.0272 0.01940 0.00993 0.0003 0.5098 0.5274
0.500 0.0544 0.01941 0.00991 0.0008 0.5025 0.5355
0.750 0.0815 0.01945 0.00995 0.0010 0.4931 0.5454
1.000 0.1085 0.01947 0.01002 0.0014 0.4846 0.5529
1.250 0.1356 0.01952 0.01005 0.0018 0.4770 0.5619
1.500 0.1626 0.01957 0.01012 0.0021 0.4678 0.5714
1.750 0.1895 0.01962 0.01017 0.0026 0.4602 0.5792
2.000 0.2164 0.01972 0.01029 0.0029 0.4517 0.5888
2.250 0.2430 0.01979 0.01039 0.0033 0.4431 0.5974
2.500 0.2698 0.01987 0.01044 0.0038 0.4360 0.6062
2.750 0.2964 0.01999 0.01059 0.0040 0.4269 0.6165
3.000 0.3225 0.02009 0.01073 0.0047 0.4191 0.6242
3.250 0.3488 0.02023 0.01088 0.0051 0.4113 0.6338
3.500 0.3748 0.02036 0.01105 0.0055 0.4028 0.6433
3.750 0.4009 0.02048 0.01114 0.0062 0.3959 0.6520
4.000 0.4264 0.02067 0.01140 0.0065 0.3873 0.6625
4.250 0.4516 0.02082 0.01158 0.0072 0.3795 0.6710
4.500 0.4769 0.02100 0.01176 0.0078 0.3723 0.6809
4.750 0.5018 0.02121 0.01203 0.0083 0.3641 0.6912
5.000 0.5264 0.02137 0.01219 0.0092 0.3571 0.7001
5.250 0.5507 0.02163 0.01249 0.0097 0.3493 0.7113
5.500 0.5741 0.02185 0.01277 0.0106 0.3418 0.7205
5.750 0.5986 0.02206 0.01293 0.0113 0.3353 0.7313
6.000 0.6208 0.02236 0.01335 0.0121 0.3273 0.7417
6.250 0.6434 0.02259 0.01360 0.0131 0.3205 0.7525
6.500 0.6659 0.02289 0.01391 0.0139 0.3138 0.7639
6.750 0.6865 0.02320 0.01433 0.0151 0.3065 0.7750
7.000 0.7086 0.02346 0.01454 0.0161 0.3003 0.7872
7.250 0.7278 0.02383 0.01502 0.0174 0.2935 0.7993
7.500 0.7470 0.02417 0.01542 0.0186 0.2868 0.8122
7.750 0.7673 0.02446 0.01564 0.0199 0.2813 0.8263
8.000 0.7828 0.02490 0.01625 0.0216 0.2746 0.8405
8.250 0.7993 0.02526 0.01667 0.0232 0.2685 0.8565
8.500 0.8172 0.02559 0.01695 0.0247 0.2633 0.8744
8.750 0.8311 0.02610 0.01765 0.0264 0.2569 0.8953
9.000 0.8509 0.02657 0.01816 0.0271 0.2510 0.9196
9.250 0.8786 0.02714 0.01873 0.0262 0.2450 0.9487
9.500 0.9040 0.02790 0.01960 0.0247 0.2382 1.0000
9.750 0.9159 0.02852 0.02014 0.0259 0.2334 1.0000
10.000 0.9278 0.02930 0.02088 0.0269 0.2287 1.0000
10.250 0.9360 0.03032 0.02195 0.0279 0.2234 1.0000
10.500 0.9472 0.03124 0.02283 0.0287 0.2188 1.0000
10.750 0.9603 0.03214 0.02366 0.0294 0.2145 1.0000
11.000 0.9652 0.03357 0.02518 0.0301 0.2095 1.0000
11.250 0.9738 0.03481 0.02643 0.0307 0.2050 1.0000
11.500 0.9878 0.03574 0.02726 0.0312 0.2012 1.0000
11.750 0.9894 0.03762 0.02926 0.0315 0.1967 1.0000
12.000 0.9939 0.03935 0.03103 0.0318 0.1923 1.0000
12.250 1.0038 0.04068 0.03232 0.0320 0.1886 1.0000
12.500 1.0098 0.04241 0.03407 0.0322 0.1849 1.0000
12.750 1.0077 0.04492 0.03669 0.0319 0.1807 1.0000
13.000 1.0123 0.04688 0.03868 0.0318 0.1771 1.0000
13.250 1.0256 0.04803 0.03974 0.0320 0.1738 1.0000
13.500 1.0172 0.05142 0.04329 0.0311 0.1702 1.0000
13.750 1.0119 0.05459 0.04657 0.0303 0.1665 1.0000
14.000 1.0175 0.05665 0.04862 0.0299 0.1632 1.0000
14.250 1.0285 0.05816 0.05007 0.0298 0.1604 1.0000
14.500 1.0047 0.06386 0.05602 0.0274 0.1567 1.0000
14.750 0.9950 0.06811 0.06037 0.0257 0.1533 1.0000
15.000 1.0063 0.06970 0.06191 0.0254 0.1505 1.0000
15.250 1.0001 0.07371 0.06599 0.0237 0.1476 1.0000
15.500 0.9241 0.08824 0.08093 0.0161 0.1425 1.0000
15.750 0.9356 0.08997 0.08264 0.0155 0.1399 1.0000
16.000 0.9721 0.08780 0.08033 0.0172 0.1383 1.0000
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