Joukovsky f=0% t=18% (joukowsk0018-jf) Xfoil prediction polar at RE=100,000 Ncrit=5
| Details | Polar file |
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Airfoil: Joukovsky f=0% t=18% (joukowsk0018-jf) Reynolds number: 100,000 Max Cl/Cd: 36.57 at α=8.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-joukowsk0018-jf-100000-n5.txt Download as CSV file: xf-joukowsk0018-jf-100000-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 = 0.100 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-16.500 -1.0196 0.09628 0.08923 -0.0081 1.0000 0.0984
-16.250 -1.0171 0.09304 0.08597 -0.0096 1.0000 0.1002
-16.000 -1.0160 0.08958 0.08250 -0.0112 1.0000 0.1022
-15.750 -1.0376 0.08250 0.07524 -0.0151 1.0000 0.1045
-15.500 -1.0637 0.07509 0.06756 -0.0192 1.0000 0.1068
-15.250 -1.0693 0.07100 0.06339 -0.0210 1.0000 0.1089
-15.000 -1.0649 0.06847 0.06087 -0.0219 1.0000 0.1112
-14.750 -1.0698 0.06472 0.05703 -0.0235 1.0000 0.1136
-14.500 -1.0791 0.06051 0.05264 -0.0252 1.0000 0.1162
-14.250 -1.0808 0.05740 0.04945 -0.0263 1.0000 0.1187
-14.000 -1.0764 0.05515 0.04720 -0.0268 1.0000 0.1212
-13.750 -1.0768 0.05235 0.04432 -0.0276 1.0000 0.1241
-13.500 -1.0800 0.04928 0.04109 -0.0284 1.0000 0.1272
-13.250 -1.0746 0.04726 0.03907 -0.0285 1.0000 0.1300
-13.000 -1.0703 0.04521 0.03701 -0.0287 1.0000 0.1330
-12.750 -1.0683 0.04296 0.03466 -0.0289 1.0000 0.1366
-12.500 -1.0645 0.04092 0.03252 -0.0289 1.0000 0.1401
-12.250 -1.0574 0.03932 0.03097 -0.0286 1.0000 0.1433
-12.000 -1.0520 0.03761 0.02919 -0.0283 1.0000 0.1473
-11.750 -1.0468 0.03590 0.02736 -0.0279 1.0000 0.1515
-11.500 -1.0379 0.03462 0.02614 -0.0273 1.0000 0.1551
-11.250 -1.0302 0.03329 0.02477 -0.0265 1.0000 0.1595
-11.000 -1.0225 0.03198 0.02335 -0.0256 1.0000 0.1643
-10.750 -1.0126 0.03094 0.02240 -0.0245 1.0000 0.1683
-10.500 -1.0035 0.02993 0.02135 -0.0232 1.0000 0.1733
-10.250 -0.9935 0.02899 0.02034 -0.0218 1.0000 0.1785
-10.000 -0.9818 0.02820 0.01962 -0.0203 1.0000 0.1833
-9.750 -0.9676 0.02740 0.01876 -0.0192 1.0000 0.1895
-9.500 -0.9518 0.02666 0.01805 -0.0182 1.0000 0.1952
-9.250 -0.9353 0.02597 0.01737 -0.0172 1.0000 0.2015
-9.000 -0.9174 0.02529 0.01665 -0.0163 1.0000 0.2082
-8.750 -0.8992 0.02469 0.01613 -0.0155 1.0000 0.2147
-8.500 -0.8801 0.02409 0.01544 -0.0147 1.0000 0.2224
-8.250 -0.8611 0.02355 0.01503 -0.0139 1.0000 0.2289
-8.000 -0.8424 0.02304 0.01450 -0.0130 1.0000 0.2368
-7.750 -0.8179 0.02256 0.01409 -0.0133 0.9835 0.2444
-7.500 -0.7812 0.02207 0.01352 -0.0156 0.9558 0.2549
-7.250 -0.7467 0.02164 0.01315 -0.0172 0.9334 0.2639
-7.000 -0.7173 0.02126 0.01266 -0.0177 0.9118 0.2739
-6.750 -0.6920 0.02096 0.01240 -0.0173 0.8915 0.2822
-6.500 -0.6686 0.02067 0.01200 -0.0165 0.8728 0.2918
-6.250 -0.6460 0.02043 0.01178 -0.0154 0.8560 0.3000
-5.750 -0.6004 0.01994 0.01122 -0.0133 0.8241 0.3182
-5.500 -0.5770 0.01971 0.01086 -0.0124 0.8098 0.3284
-5.250 -0.5536 0.01951 0.01070 -0.0113 0.7967 0.3369
-5.000 -0.5290 0.01928 0.01038 -0.0107 0.7823 0.3475
-4.750 -0.5045 0.01910 0.01024 -0.0098 0.7697 0.3562
-4.500 -0.4796 0.01890 0.00993 -0.0091 0.7567 0.3670
-4.250 -0.4543 0.01874 0.00983 -0.0084 0.7442 0.3759
-3.750 -0.4030 0.01842 0.00946 -0.0071 0.7197 0.3959
-3.500 -0.3774 0.01828 0.00920 -0.0064 0.7091 0.4070
-3.250 -0.3508 0.01815 0.00915 -0.0059 0.6961 0.4163
-3.000 -0.3248 0.01803 0.00890 -0.0053 0.6860 0.4274
-2.750 -0.2980 0.01792 0.00888 -0.0049 0.6731 0.4368
-2.500 -0.2716 0.01782 0.00866 -0.0043 0.6630 0.4480
-2.250 -0.2445 0.01773 0.00866 -0.0039 0.6506 0.4576
-2.000 -0.2179 0.01765 0.00846 -0.0033 0.6406 0.4689
-1.750 -0.1906 0.01758 0.00848 -0.0030 0.6283 0.4783
-1.500 -0.1638 0.01752 0.00830 -0.0024 0.6186 0.4899
-1.250 -0.1364 0.01747 0.00834 -0.0021 0.6063 0.4993
-1.000 -0.1094 0.01742 0.00819 -0.0016 0.5969 0.5110
-0.750 -0.0820 0.01740 0.00826 -0.0012 0.5846 0.5204
-0.500 -0.0547 0.01737 0.00812 -0.0008 0.5751 0.5322
-0.250 -0.0273 0.01736 0.00822 -0.0004 0.5631 0.5418
0.000 0.0000 0.01735 0.00810 0.0000 0.5535 0.5535
0.250 0.0273 0.01736 0.00822 0.0004 0.5418 0.5631
0.500 0.0547 0.01737 0.00812 0.0008 0.5322 0.5751
0.750 0.0819 0.01740 0.00826 0.0012 0.5205 0.5846
1.000 0.1093 0.01743 0.00819 0.0016 0.5110 0.5969
1.250 0.1364 0.01747 0.00834 0.0021 0.4993 0.6063
1.500 0.1637 0.01752 0.00830 0.0025 0.4899 0.6187
1.750 0.1906 0.01758 0.00848 0.0030 0.4783 0.6283
2.000 0.2179 0.01765 0.00846 0.0033 0.4689 0.6406
2.250 0.2445 0.01773 0.00866 0.0039 0.4575 0.6506
2.500 0.2716 0.01782 0.00866 0.0043 0.4480 0.6630
2.750 0.2979 0.01792 0.00888 0.0049 0.4368 0.6731
3.000 0.3248 0.01803 0.00890 0.0053 0.4274 0.6859
3.250 0.3508 0.01815 0.00915 0.0059 0.4163 0.6961
3.500 0.3774 0.01828 0.00920 0.0064 0.4070 0.7091
3.750 0.4030 0.01842 0.00946 0.0071 0.3960 0.7197
4.250 0.4543 0.01874 0.00983 0.0084 0.3759 0.7442
4.500 0.4796 0.01890 0.00993 0.0091 0.3670 0.7567
4.750 0.5044 0.01910 0.01024 0.0098 0.3562 0.7697
5.000 0.5289 0.01928 0.01037 0.0107 0.3475 0.7823
5.250 0.5536 0.01951 0.01070 0.0113 0.3369 0.7967
5.500 0.5770 0.01971 0.01086 0.0124 0.3284 0.8098
5.750 0.6004 0.01994 0.01122 0.0133 0.3182 0.8241
6.250 0.6460 0.02043 0.01178 0.0154 0.3000 0.8560
6.500 0.6686 0.02067 0.01200 0.0165 0.2918 0.8728
6.750 0.6920 0.02096 0.01240 0.0173 0.2822 0.8915
7.000 0.7174 0.02126 0.01266 0.0177 0.2739 0.9118
7.250 0.7467 0.02164 0.01314 0.0172 0.2639 0.9335
7.500 0.7813 0.02207 0.01352 0.0156 0.2549 0.9559
7.750 0.8180 0.02255 0.01409 0.0132 0.2444 0.9835
8.000 0.8424 0.02304 0.01450 0.0130 0.2368 1.0000
8.250 0.8612 0.02355 0.01503 0.0139 0.2289 1.0000
8.500 0.8802 0.02409 0.01544 0.0147 0.2224 1.0000
8.750 0.8993 0.02469 0.01612 0.0155 0.2147 1.0000
9.000 0.9175 0.02529 0.01665 0.0163 0.2082 1.0000
9.250 0.9354 0.02597 0.01737 0.0172 0.2015 1.0000
9.500 0.9520 0.02666 0.01805 0.0182 0.1951 1.0000
9.750 0.9678 0.02740 0.01876 0.0192 0.1895 1.0000
10.000 0.9820 0.02820 0.01962 0.0203 0.1833 1.0000
10.250 0.9938 0.02898 0.02034 0.0217 0.1785 1.0000
10.500 1.0039 0.02993 0.02135 0.0232 0.1733 1.0000
10.750 1.0131 0.03094 0.02239 0.0245 0.1683 1.0000
11.000 1.0230 0.03197 0.02334 0.0256 0.1642 1.0000
11.250 1.0307 0.03328 0.02477 0.0265 0.1594 1.0000
11.500 1.0385 0.03461 0.02613 0.0272 0.1550 1.0000
11.750 1.0475 0.03588 0.02734 0.0278 0.1514 1.0000
12.000 1.0527 0.03760 0.02918 0.0283 0.1472 1.0000
12.250 1.0582 0.03931 0.03095 0.0285 0.1433 1.0000
12.500 1.0654 0.04089 0.03250 0.0288 0.1400 1.0000
12.750 1.0691 0.04295 0.03465 0.0288 0.1365 1.0000
13.000 1.0714 0.04517 0.03697 0.0286 0.1330 1.0000
13.250 1.0758 0.04721 0.03902 0.0284 0.1299 1.0000
13.500 1.0810 0.04926 0.04107 0.0282 0.1271 1.0000
13.750 1.0781 0.05231 0.04428 0.0274 0.1240 1.0000
14.000 1.0777 0.05510 0.04714 0.0267 0.1211 1.0000
14.250 1.0825 0.05731 0.04935 0.0261 0.1186 1.0000
14.500 1.0807 0.06045 0.05258 0.0251 0.1161 1.0000
14.750 1.0713 0.06467 0.05697 0.0233 0.1135 1.0000
15.000 1.0668 0.06836 0.06076 0.0218 0.1111 1.0000
15.250 1.0716 0.07084 0.06322 0.0210 0.1089 1.0000
15.500 1.0649 0.07508 0.06756 0.0190 0.1067 1.0000
15.750 1.0394 0.08242 0.07515 0.0150 0.1045 1.0000
16.000 1.0184 0.08941 0.08232 0.0111 0.1022 1.0000
16.250 1.0211 0.09259 0.08551 0.0097 0.1002 1.0000
16.500 1.0177 0.09686 0.08982 0.0076 0.0982 1.0000
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