Joukovsky f=0% t=18% (joukowsk0018-jf) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: Joukovsky f=0% t=18% (joukowsk0018-jf) Reynolds number: 1,000,000 Max Cl/Cd: 86.44 at α=10.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-joukowsk0018-jf-1000000.txt Download as CSV file: xf-joukowsk0018-jf-1000000.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 = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.3343 0.09531 0.09130 -0.0038 1.0000 0.0469
-19.500 -1.3468 0.08981 0.08574 -0.0066 1.0000 0.0477
-19.250 -1.3571 0.08474 0.08061 -0.0092 1.0000 0.0484
-19.000 -1.3663 0.07992 0.07572 -0.0115 1.0000 0.0491
-18.750 -1.3733 0.07548 0.07120 -0.0136 1.0000 0.0500
-18.500 -1.3783 0.07143 0.06707 -0.0154 1.0000 0.0508
-18.250 -1.3800 0.06789 0.06346 -0.0169 1.0000 0.0514
-18.000 -1.3910 0.06321 0.05870 -0.0189 1.0000 0.0523
-17.750 -1.4004 0.05887 0.05430 -0.0206 1.0000 0.0531
-17.500 -1.4069 0.05500 0.05037 -0.0220 1.0000 0.0540
-17.250 -1.4109 0.05154 0.04685 -0.0232 1.0000 0.0549
-17.000 -1.4127 0.04842 0.04366 -0.0241 1.0000 0.0558
-16.750 -1.4114 0.04572 0.04088 -0.0248 1.0000 0.0566
-16.500 -1.4164 0.04249 0.03759 -0.0255 1.0000 0.0577
-16.250 -1.4199 0.03951 0.03456 -0.0260 1.0000 0.0588
-16.000 -1.4201 0.03695 0.03195 -0.0263 1.0000 0.0598
-15.750 -1.4175 0.03471 0.02966 -0.0264 1.0000 0.0611
-15.500 -1.4121 0.03280 0.02769 -0.0264 1.0000 0.0623
-15.250 -1.4102 0.03063 0.02547 -0.0262 1.0000 0.0636
-15.000 -1.4077 0.02861 0.02342 -0.0259 1.0000 0.0650
-14.750 -1.4021 0.02690 0.02168 -0.0255 1.0000 0.0665
-14.500 -1.3940 0.02546 0.02020 -0.0250 1.0000 0.0679
-14.250 -1.3860 0.02409 0.01878 -0.0243 1.0000 0.0696
-14.000 -1.3802 0.02264 0.01732 -0.0234 1.0000 0.0713
-13.750 -1.3718 0.02145 0.01610 -0.0224 1.0000 0.0731
-13.500 -1.3607 0.02050 0.01512 -0.0213 1.0000 0.0749
-13.250 -1.3516 0.01951 0.01410 -0.0200 1.0000 0.0768
-13.000 -1.3433 0.01858 0.01317 -0.0184 1.0000 0.0789
-12.750 -1.3324 0.01787 0.01243 -0.0167 1.0000 0.0812
-12.500 -1.3202 0.01729 0.01182 -0.0149 1.0000 0.0831
-12.250 -1.3119 0.01664 0.01118 -0.0124 1.0000 0.0856
-12.000 -1.2968 0.01615 0.01069 -0.0107 1.0000 0.0884
-11.750 -1.2770 0.01574 0.01026 -0.0097 1.0000 0.0908
-11.500 -1.2586 0.01521 0.00975 -0.0086 1.0000 0.0943
-11.250 -1.2371 0.01480 0.00935 -0.0078 1.0000 0.0977
-11.000 -1.2153 0.01438 0.00894 -0.0071 1.0000 0.1012
-10.750 -1.1928 0.01396 0.00854 -0.0065 1.0000 0.1052
-10.500 -1.1687 0.01361 0.00820 -0.0060 1.0000 0.1089
-10.250 -1.1402 0.01319 0.00782 -0.0065 0.9724 0.1138
-10.000 -1.1143 0.01298 0.00753 -0.0061 0.9274 0.1178
-9.750 -1.0954 0.01269 0.00720 -0.0045 0.8980 0.1227
-9.500 -1.0724 0.01247 0.00692 -0.0035 0.8769 0.1273
-9.250 -1.0491 0.01218 0.00660 -0.0027 0.8582 0.1325
-9.000 -1.0243 0.01194 0.00632 -0.0021 0.8413 0.1377
-8.750 -0.9992 0.01167 0.00603 -0.0016 0.8260 0.1435
-8.500 -0.9734 0.01144 0.00578 -0.0012 0.8117 0.1492
-8.000 -0.9210 0.01096 0.00527 -0.0005 0.7846 0.1617
-7.750 -0.8945 0.01074 0.00503 -0.0002 0.7718 0.1683
-7.500 -0.8674 0.01053 0.00481 0.0001 0.7591 0.1752
-7.250 -0.8402 0.01032 0.00459 0.0003 0.7473 0.1822
-7.000 -0.8128 0.01013 0.00439 0.0005 0.7349 0.1895
-6.750 -0.7852 0.00993 0.00420 0.0006 0.7238 0.1970
-6.500 -0.7574 0.00977 0.00401 0.0007 0.7117 0.2047
-6.250 -0.7294 0.00958 0.00383 0.0008 0.7011 0.2127
-6.000 -0.7012 0.00943 0.00367 0.0009 0.6894 0.2207
-5.750 -0.6730 0.00925 0.00351 0.0010 0.6789 0.2291
-5.500 -0.6445 0.00913 0.00336 0.0011 0.6676 0.2374
-5.250 -0.6161 0.00896 0.00321 0.0011 0.6574 0.2462
-5.000 -0.5873 0.00885 0.00309 0.0011 0.6462 0.2545
-4.750 -0.5586 0.00870 0.00295 0.0011 0.6362 0.2638
-4.500 -0.5296 0.00861 0.00284 0.0011 0.6252 0.2723
-4.250 -0.5008 0.00847 0.00272 0.0011 0.6152 0.2820
-4.000 -0.4716 0.00839 0.00263 0.0011 0.6047 0.2904
-3.750 -0.4427 0.00828 0.00252 0.0011 0.5944 0.3003
-3.500 -0.4133 0.00820 0.00245 0.0010 0.5843 0.3089
-3.250 -0.3842 0.00811 0.00235 0.0010 0.5737 0.3191
-3.000 -0.3547 0.00804 0.00229 0.0009 0.5640 0.3278
-2.750 -0.3256 0.00796 0.00221 0.0009 0.5532 0.3381
-2.500 -0.2959 0.00791 0.00215 0.0008 0.5439 0.3469
-2.250 -0.2666 0.00784 0.00209 0.0008 0.5332 0.3572
-2.000 -0.2369 0.00780 0.00205 0.0007 0.5240 0.3662
-1.750 -0.2075 0.00774 0.00199 0.0006 0.5134 0.3765
-1.500 -0.1778 0.00771 0.00196 0.0005 0.5041 0.3856
-1.250 -0.1483 0.00767 0.00192 0.0004 0.4937 0.3959
-1.000 -0.1186 0.00765 0.00190 0.0004 0.4843 0.4052
-0.750 -0.0890 0.00762 0.00188 0.0003 0.4740 0.4153
-0.500 -0.0593 0.00761 0.00187 0.0002 0.4645 0.4249
-0.250 -0.0297 0.00759 0.00186 0.0001 0.4544 0.4348
0.000 0.0000 0.00760 0.00186 0.0000 0.4446 0.4446
0.250 0.0297 0.00759 0.00186 -0.0001 0.4348 0.4544
0.500 0.0593 0.00761 0.00187 -0.0002 0.4248 0.4645
0.750 0.0890 0.00762 0.00188 -0.0003 0.4154 0.4740
1.000 0.1185 0.00765 0.00190 -0.0003 0.4051 0.4843
1.250 0.1483 0.00767 0.00192 -0.0004 0.3959 0.4936
1.500 0.1777 0.00771 0.00196 -0.0005 0.3856 0.5041
1.750 0.2075 0.00774 0.00200 -0.0006 0.3766 0.5134
2.000 0.2369 0.00780 0.00205 -0.0007 0.3661 0.5239
2.250 0.2666 0.00784 0.00209 -0.0008 0.3572 0.5332
2.500 0.2958 0.00791 0.00215 -0.0008 0.3469 0.5439
2.750 0.3255 0.00796 0.00221 -0.0009 0.3381 0.5532
3.000 0.3546 0.00804 0.00229 -0.0009 0.3278 0.5640
3.250 0.3842 0.00811 0.00235 -0.0010 0.3191 0.5737
3.500 0.4132 0.00820 0.00245 -0.0010 0.3089 0.5843
3.750 0.4426 0.00828 0.00252 -0.0011 0.3003 0.5944
4.000 0.4716 0.00839 0.00263 -0.0011 0.2904 0.6046
4.250 0.5008 0.00847 0.00272 -0.0011 0.2820 0.6152
4.500 0.5296 0.00861 0.00284 -0.0011 0.2723 0.6252
4.750 0.5586 0.00870 0.00295 -0.0011 0.2638 0.6362
5.000 0.5872 0.00885 0.00309 -0.0011 0.2545 0.6462
5.250 0.6160 0.00896 0.00321 -0.0011 0.2462 0.6573
5.500 0.6445 0.00913 0.00336 -0.0010 0.2373 0.6677
5.750 0.6730 0.00925 0.00351 -0.0010 0.2292 0.6789
6.000 0.7012 0.00943 0.00367 -0.0009 0.2207 0.6895
6.250 0.7294 0.00958 0.00383 -0.0008 0.2127 0.7011
6.500 0.7573 0.00977 0.00401 -0.0007 0.2047 0.7118
6.750 0.7851 0.00993 0.00419 -0.0006 0.1970 0.7238
7.000 0.8128 0.01013 0.00439 -0.0004 0.1895 0.7349
7.250 0.8402 0.01032 0.00459 -0.0003 0.1822 0.7472
7.500 0.8674 0.01053 0.00481 0.0000 0.1752 0.7591
7.750 0.8944 0.01074 0.00503 0.0002 0.1683 0.7718
8.000 0.9210 0.01096 0.00527 0.0005 0.1617 0.7845
8.500 0.9734 0.01143 0.00578 0.0012 0.1492 0.8118
8.750 0.9991 0.01167 0.00603 0.0016 0.1434 0.8261
9.000 1.0242 0.01194 0.00632 0.0021 0.1377 0.8413
9.250 1.0491 0.01218 0.00660 0.0027 0.1325 0.8581
9.500 1.0723 0.01247 0.00692 0.0035 0.1272 0.8768
9.750 1.0953 0.01269 0.00720 0.0045 0.1228 0.8980
10.000 1.1142 0.01298 0.00754 0.0062 0.1177 0.9274
10.250 1.1402 0.01319 0.00781 0.0065 0.1138 0.9721
10.500 1.1687 0.01362 0.00820 0.0060 0.1088 1.0000
10.750 1.1928 0.01396 0.00854 0.0065 0.1051 1.0000
11.000 1.2153 0.01438 0.00893 0.0071 0.1012 1.0000
11.250 1.2371 0.01480 0.00935 0.0078 0.0977 1.0000
11.500 1.2587 0.01520 0.00975 0.0086 0.0944 1.0000
11.750 1.2772 0.01574 0.01025 0.0097 0.0909 1.0000
12.000 1.2970 0.01615 0.01069 0.0107 0.0884 1.0000
12.250 1.3121 0.01664 0.01118 0.0124 0.0857 1.0000
12.500 1.3206 0.01728 0.01182 0.0149 0.0831 1.0000
12.750 1.3328 0.01786 0.01242 0.0167 0.0811 1.0000
13.000 1.3436 0.01857 0.01316 0.0183 0.0790 1.0000
13.250 1.3521 0.01950 0.01408 0.0200 0.0768 1.0000
13.500 1.3610 0.02049 0.01511 0.0213 0.0749 1.0000
13.750 1.3724 0.02143 0.01608 0.0223 0.0732 1.0000
14.000 1.3807 0.02262 0.01729 0.0233 0.0712 1.0000
14.250 1.3862 0.02410 0.01878 0.0242 0.0694 1.0000
14.500 1.3946 0.02545 0.02019 0.0249 0.0680 1.0000
14.750 1.4030 0.02687 0.02164 0.0254 0.0665 1.0000
15.000 1.4083 0.02858 0.02339 0.0259 0.0650 1.0000
15.250 1.4112 0.03059 0.02543 0.0261 0.0635 1.0000
15.500 1.4133 0.03273 0.02762 0.0263 0.0623 1.0000
15.750 1.4190 0.03462 0.02957 0.0263 0.0611 1.0000
16.000 1.4216 0.03686 0.03186 0.0262 0.0599 1.0000
16.250 1.4212 0.03945 0.03449 0.0259 0.0587 1.0000
16.500 1.4177 0.04243 0.03753 0.0254 0.0575 1.0000
16.750 1.4134 0.04559 0.04075 0.0247 0.0566 1.0000
17.000 1.4145 0.04830 0.04353 0.0240 0.0558 1.0000
17.250 1.4126 0.05144 0.04674 0.0231 0.0548 1.0000
17.500 1.4089 0.05485 0.05021 0.0219 0.0539 1.0000
17.750 1.4027 0.05869 0.05412 0.0205 0.0531 1.0000
18.000 1.3932 0.06303 0.05852 0.0188 0.0522 1.0000
18.250 1.3823 0.06768 0.06324 0.0168 0.0514 1.0000
18.500 1.3808 0.07119 0.06683 0.0154 0.0507 1.0000
18.750 1.3759 0.07523 0.07095 0.0136 0.0499 1.0000
19.000 1.3686 0.07971 0.07550 0.0115 0.0490 1.0000
19.250 1.3591 0.08457 0.08044 0.0091 0.0483 1.0000
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