J5012 12% (j5012-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: J5012 12% (j5012-il) Reynolds number: 500,000 Max Cl/Cd: 58.91 at α=8.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-j5012-il-500000-n5.txt Download as CSV file: xf-j5012-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: J5012 12%
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
------ -------- --------- --------- -------- -------- --------
-18.750 -0.9158 0.13871 0.13579 -0.0039 1.0000 0.0119
-18.500 -0.9533 0.12634 0.12324 -0.0105 1.0000 0.0118
-18.250 -0.9811 0.11650 0.11327 -0.0157 1.0000 0.0118
-18.000 -1.0057 0.10768 0.10432 -0.0204 1.0000 0.0118
-17.750 -1.0286 0.09942 0.09591 -0.0247 1.0000 0.0118
-17.500 -1.0477 0.09199 0.08835 -0.0287 1.0000 0.0119
-17.250 -1.0703 0.08430 0.08051 -0.0327 1.0000 0.0118
-17.000 -1.0842 0.07811 0.07421 -0.0360 1.0000 0.0119
-16.750 -1.0995 0.07197 0.06792 -0.0392 1.0000 0.0119
-16.500 -1.1120 0.06639 0.06221 -0.0421 1.0000 0.0121
-16.250 -1.1230 0.06131 0.05699 -0.0446 1.0000 0.0121
-16.000 -1.1326 0.05663 0.05218 -0.0467 1.0000 0.0122
-15.750 -1.1409 0.05235 0.04776 -0.0484 1.0000 0.0122
-15.500 -1.1443 0.04890 0.04419 -0.0497 1.0000 0.0124
-15.250 -1.1489 0.04548 0.04063 -0.0506 1.0000 0.0126
-15.000 -1.1489 0.04276 0.03779 -0.0510 1.0000 0.0128
-14.750 -1.1516 0.03994 0.03483 -0.0511 1.0000 0.0130
-14.500 -1.1491 0.03778 0.03256 -0.0509 1.0000 0.0132
-14.250 -1.1483 0.03561 0.03026 -0.0504 1.0000 0.0133
-14.000 -1.1451 0.03376 0.02830 -0.0495 1.0000 0.0135
-13.750 -1.1412 0.03211 0.02652 -0.0484 1.0000 0.0136
-13.500 -1.1406 0.03029 0.02462 -0.0468 1.0000 0.0139
-13.250 -1.1383 0.02874 0.02298 -0.0450 1.0000 0.0141
-13.000 -1.1343 0.02741 0.02157 -0.0431 1.0000 0.0143
-12.750 -1.1287 0.02626 0.02034 -0.0410 1.0000 0.0145
-12.500 -1.1214 0.02528 0.01929 -0.0388 1.0000 0.0148
-12.250 -1.1133 0.02441 0.01834 -0.0365 1.0000 0.0151
-12.000 -1.1058 0.02356 0.01742 -0.0339 1.0000 0.0153
-11.750 -1.0968 0.02285 0.01665 -0.0314 1.0000 0.0157
-11.500 -1.0889 0.02215 0.01587 -0.0285 1.0000 0.0161
-11.250 -1.0802 0.02157 0.01523 -0.0255 1.0000 0.0166
-11.000 -1.0728 0.02101 0.01460 -0.0222 1.0000 0.0169
-10.750 -1.0648 0.02050 0.01401 -0.0188 1.0000 0.0171
-10.500 -1.0566 0.01981 0.01327 -0.0156 1.0000 0.0176
-10.250 -1.0466 0.01919 0.01261 -0.0126 1.0000 0.0180
-10.000 -1.0351 0.01866 0.01204 -0.0098 1.0000 0.0186
-9.750 -1.0227 0.01818 0.01152 -0.0072 1.0000 0.0192
-9.500 -1.0100 0.01772 0.01102 -0.0045 1.0000 0.0198
-9.250 -0.9968 0.01729 0.01053 -0.0019 1.0000 0.0204
-9.000 -0.9833 0.01689 0.01007 0.0006 1.0000 0.0211
-8.750 -0.9657 0.01644 0.00958 0.0023 0.9996 0.0219
-8.500 -0.9366 0.01589 0.00903 0.0015 0.9975 0.0234
-8.250 -0.9066 0.01545 0.00854 0.0006 0.9951 0.0253
-8.000 -0.8772 0.01501 0.00807 -0.0001 0.9928 0.0272
-7.750 -0.8492 0.01454 0.00760 -0.0005 0.9898 0.0297
-7.500 -0.8193 0.01416 0.00719 -0.0013 0.9870 0.0325
-7.250 -0.7887 0.01374 0.00678 -0.0022 0.9846 0.0363
-7.000 -0.7567 0.01340 0.00642 -0.0034 0.9827 0.0407
-6.750 -0.7308 0.01301 0.00606 -0.0032 0.9783 0.0458
-6.500 -0.7011 0.01266 0.00571 -0.0038 0.9748 0.0513
-6.250 -0.6698 0.01231 0.00539 -0.0048 0.9722 0.0583
-6.000 -0.6374 0.01195 0.00506 -0.0060 0.9701 0.0670
-5.750 -0.6109 0.01162 0.00477 -0.0059 0.9652 0.0770
-5.500 -0.5815 0.01126 0.00447 -0.0065 0.9610 0.0918
-5.250 -0.5495 0.01088 0.00418 -0.0076 0.9580 0.1112
-5.000 -0.5164 0.01048 0.00390 -0.0090 0.9554 0.1341
-4.750 -0.4914 0.01015 0.00366 -0.0086 0.9483 0.1570
-4.500 -0.4607 0.00981 0.00341 -0.0093 0.9434 0.1830
-4.250 -0.4305 0.00943 0.00317 -0.0101 0.9384 0.2156
-4.000 -0.4038 0.00910 0.00296 -0.0100 0.9305 0.2481
-3.750 -0.3730 0.00877 0.00275 -0.0107 0.9244 0.2818
-3.500 -0.3474 0.00849 0.00258 -0.0103 0.9150 0.3146
-3.250 -0.3199 0.00819 0.00241 -0.0103 0.9067 0.3524
-3.000 -0.2941 0.00791 0.00226 -0.0099 0.8966 0.3917
-2.750 -0.2691 0.00767 0.00213 -0.0093 0.8858 0.4288
-2.500 -0.2435 0.00745 0.00201 -0.0088 0.8749 0.4623
-2.250 -0.2180 0.00728 0.00190 -0.0082 0.8629 0.4927
-2.000 -0.1937 0.00712 0.00181 -0.0074 0.8496 0.5236
-1.750 -0.1694 0.00698 0.00174 -0.0065 0.8358 0.5536
-1.500 -0.1450 0.00686 0.00167 -0.0057 0.8217 0.5821
-1.250 -0.1210 0.00676 0.00162 -0.0047 0.8068 0.6090
-1.000 -0.0967 0.00668 0.00157 -0.0038 0.7914 0.6335
-0.750 -0.0725 0.00662 0.00154 -0.0029 0.7752 0.6573
-0.500 -0.0482 0.00658 0.00152 -0.0020 0.7581 0.6786
-0.250 -0.0241 0.00656 0.00150 -0.0010 0.7400 0.7001
0.000 0.0000 0.00655 0.00150 0.0000 0.7210 0.7209
0.250 0.0241 0.00655 0.00150 0.0010 0.7003 0.7402
0.500 0.0482 0.00658 0.00152 0.0020 0.6789 0.7581
0.750 0.0724 0.00662 0.00154 0.0029 0.6569 0.7752
1.000 0.0966 0.00668 0.00157 0.0038 0.6335 0.7915
1.250 0.1209 0.00676 0.00162 0.0048 0.6087 0.8069
1.500 0.1450 0.00686 0.00167 0.0057 0.5820 0.8218
1.750 0.1694 0.00698 0.00174 0.0065 0.5539 0.8359
2.000 0.1938 0.00711 0.00181 0.0074 0.5245 0.8496
2.500 0.2435 0.00745 0.00201 0.0088 0.4626 0.8748
2.750 0.2689 0.00767 0.00213 0.0094 0.4279 0.8858
3.000 0.2942 0.00790 0.00226 0.0099 0.3926 0.8965
3.250 0.3199 0.00819 0.00241 0.0103 0.3527 0.9066
3.500 0.3473 0.00849 0.00258 0.0103 0.3145 0.9150
3.750 0.3730 0.00877 0.00275 0.0107 0.2819 0.9244
4.000 0.4037 0.00911 0.00296 0.0100 0.2473 0.9305
4.250 0.4304 0.00944 0.00317 0.0101 0.2150 0.9383
4.500 0.4607 0.00980 0.00341 0.0093 0.1839 0.9434
4.750 0.4914 0.01016 0.00366 0.0086 0.1566 0.9482
5.000 0.5163 0.01048 0.00390 0.0090 0.1340 0.9554
5.250 0.5494 0.01088 0.00418 0.0076 0.1112 0.9580
5.500 0.5816 0.01125 0.00447 0.0065 0.0923 0.9610
5.750 0.6110 0.01161 0.00476 0.0059 0.0777 0.9651
6.000 0.6375 0.01195 0.00506 0.0060 0.0672 0.9702
6.250 0.6698 0.01231 0.00539 0.0048 0.0584 0.9722
6.500 0.7011 0.01267 0.00572 0.0038 0.0513 0.9749
6.750 0.7307 0.01301 0.00606 0.0032 0.0454 0.9783
7.000 0.7567 0.01339 0.00642 0.0034 0.0403 0.9827
7.250 0.7887 0.01374 0.00678 0.0022 0.0361 0.9846
7.500 0.8194 0.01416 0.00720 0.0012 0.0324 0.9870
7.750 0.8492 0.01454 0.00760 0.0005 0.0296 0.9898
8.000 0.8771 0.01503 0.00808 0.0001 0.0268 0.9928
8.250 0.9067 0.01544 0.00854 -0.0007 0.0252 0.9952
8.500 0.9366 0.01590 0.00903 -0.0015 0.0236 0.9975
8.750 0.9657 0.01645 0.00959 -0.0023 0.0219 0.9996
9.000 0.9832 0.01690 0.01008 -0.0006 0.0210 1.0000
9.250 0.9967 0.01730 0.01054 0.0020 0.0203 1.0000
9.500 1.0097 0.01774 0.01103 0.0046 0.0197 1.0000
9.750 1.0226 0.01818 0.01152 0.0072 0.0191 1.0000
10.000 1.0349 0.01867 0.01205 0.0099 0.0186 1.0000
10.250 1.0465 0.01920 0.01261 0.0126 0.0180 1.0000
10.500 1.0565 0.01982 0.01327 0.0156 0.0176 1.0000
10.750 1.0644 0.02052 0.01403 0.0189 0.0171 1.0000
11.000 1.0721 0.02105 0.01464 0.0223 0.0169 1.0000
11.250 1.0799 0.02159 0.01525 0.0256 0.0165 1.0000
11.500 1.0879 0.02221 0.01594 0.0286 0.0162 1.0000
11.750 1.0971 0.02284 0.01664 0.0313 0.0157 1.0000
12.000 1.1053 0.02360 0.01747 0.0340 0.0154 1.0000
12.250 1.1135 0.02441 0.01835 0.0365 0.0151 1.0000
12.500 1.1217 0.02528 0.01929 0.0387 0.0148 1.0000
12.750 1.1287 0.02628 0.02037 0.0409 0.0145 1.0000
13.000 1.1349 0.02740 0.02157 0.0430 0.0144 1.0000
13.250 1.1394 0.02870 0.02295 0.0449 0.0142 1.0000
13.500 1.1405 0.03035 0.02467 0.0468 0.0138 1.0000
13.750 1.1404 0.03222 0.02663 0.0484 0.0136 1.0000
14.000 1.1452 0.03381 0.02834 0.0494 0.0135 1.0000
14.250 1.1482 0.03568 0.03033 0.0503 0.0134 1.0000
14.500 1.1497 0.03780 0.03257 0.0508 0.0132 1.0000
14.750 1.1507 0.04011 0.03500 0.0510 0.0131 1.0000
15.000 1.1500 0.04275 0.03777 0.0509 0.0129 1.0000
15.250 1.1489 0.04559 0.04074 0.0504 0.0127 1.0000
15.500 1.1438 0.04906 0.04436 0.0495 0.0126 1.0000
15.750 1.1413 0.05244 0.04785 0.0483 0.0124 1.0000
16.000 1.1333 0.05668 0.05223 0.0465 0.0123 1.0000
16.250 1.1242 0.06131 0.05700 0.0444 0.0122 1.0000
16.500 1.1129 0.06645 0.06228 0.0419 0.0121 1.0000
16.750 1.0993 0.07219 0.06815 0.0389 0.0120 1.0000
17.000 1.0858 0.07810 0.07419 0.0358 0.0120 1.0000
17.250 1.0668 0.08510 0.08134 0.0321 0.0119 1.0000
17.500 1.0524 0.09155 0.08791 0.0286 0.0118 1.0000
17.750 1.0301 0.09947 0.09597 0.0244 0.0118 1.0000
18.000 1.0076 0.10771 0.10434 0.0200 0.0118 1.0000
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