J5012 12% (j5012-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: J5012 12% (j5012-il) Reynolds number: 1,000,000 Max Cl/Cd: 70.71 at α=8.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-j5012-il-1000000.txt Download as CSV file: xf-j5012-il-1000000.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 = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.250 -0.9944 0.13179 0.12947 -0.0062 1.0000 0.0117
-19.000 -1.0187 0.12268 0.12025 -0.0112 1.0000 0.0117
-18.750 -1.0472 0.11302 0.11045 -0.0164 1.0000 0.0117
-18.500 -1.0728 0.10428 0.10158 -0.0210 1.0000 0.0116
-18.250 -1.0950 0.09633 0.09350 -0.0252 1.0000 0.0116
-18.000 -1.1165 0.08872 0.08576 -0.0293 1.0000 0.0117
-17.750 -1.1366 0.08157 0.07846 -0.0330 1.0000 0.0116
-17.500 -1.1497 0.07562 0.07243 -0.0362 1.0000 0.0118
-17.250 -1.1622 0.06998 0.06668 -0.0392 1.0000 0.0118
-17.000 -1.1746 0.06450 0.06108 -0.0420 1.0000 0.0119
-16.750 -1.1865 0.05937 0.05582 -0.0444 1.0000 0.0119
-16.500 -1.1959 0.05474 0.05108 -0.0465 1.0000 0.0121
-16.250 -1.1972 0.05136 0.04762 -0.0480 1.0000 0.0122
-16.000 -1.2062 0.04725 0.04337 -0.0494 1.0000 0.0123
-15.750 -1.2099 0.04395 0.03996 -0.0502 1.0000 0.0124
-15.500 -1.2104 0.04118 0.03709 -0.0507 1.0000 0.0125
-15.250 -1.2064 0.03903 0.03485 -0.0509 1.0000 0.0129
-15.000 -1.2066 0.03658 0.03229 -0.0507 1.0000 0.0129
-14.750 -1.2063 0.03434 0.02994 -0.0502 1.0000 0.0131
-14.500 -1.2010 0.03267 0.02818 -0.0495 1.0000 0.0133
-14.250 -1.1942 0.03122 0.02664 -0.0487 1.0000 0.0134
-14.000 -1.1911 0.02955 0.02487 -0.0473 1.0000 0.0135
-13.750 -1.1839 0.02830 0.02352 -0.0460 1.0000 0.0136
-13.500 -1.1849 0.02650 0.02160 -0.0437 1.0000 0.0138
-13.250 -1.1857 0.02485 0.01985 -0.0411 1.0000 0.0140
-13.000 -1.1847 0.02347 0.01839 -0.0383 1.0000 0.0144
-12.750 -1.1786 0.02248 0.01734 -0.0357 1.0000 0.0146
-12.500 -1.1697 0.02172 0.01653 -0.0333 1.0000 0.0149
-12.250 -1.1593 0.02111 0.01587 -0.0310 1.0000 0.0153
-12.000 -1.1500 0.02049 0.01521 -0.0282 1.0000 0.0156
-11.750 -1.1423 0.01990 0.01456 -0.0250 1.0000 0.0158
-11.500 -1.1353 0.01940 0.01401 -0.0215 1.0000 0.0162
-11.250 -1.1283 0.01894 0.01349 -0.0179 1.0000 0.0165
-11.000 -1.1179 0.01842 0.01291 -0.0149 1.0000 0.0168
-10.750 -1.1057 0.01798 0.01242 -0.0122 1.0000 0.0170
-10.500 -1.0929 0.01759 0.01198 -0.0095 1.0000 0.0172
-10.250 -1.0881 0.01678 0.01109 -0.0055 1.0000 0.0177
-10.000 -1.0804 0.01612 0.01038 -0.0019 1.0000 0.0183
-9.750 -1.0686 0.01567 0.00992 0.0010 1.0000 0.0189
-9.500 -1.0550 0.01533 0.00955 0.0035 1.0000 0.0195
-9.250 -1.0416 0.01496 0.00915 0.0062 1.0000 0.0200
-9.000 -1.0232 0.01460 0.00874 0.0077 0.9997 0.0207
-8.750 -0.9917 0.01421 0.00831 0.0066 0.9983 0.0213
-8.500 -0.9613 0.01364 0.00769 0.0057 0.9966 0.0224
-8.250 -0.9299 0.01316 0.00721 0.0045 0.9949 0.0242
-8.000 -0.8971 0.01282 0.00684 0.0032 0.9937 0.0259
-7.750 -0.8685 0.01238 0.00639 0.0027 0.9912 0.0282
-7.500 -0.8379 0.01199 0.00603 0.0018 0.9888 0.0317
-7.250 -0.8062 0.01159 0.00564 0.0008 0.9868 0.0364
-7.000 -0.7729 0.01131 0.00536 -0.0006 0.9852 0.0405
-6.750 -0.7396 0.01091 0.00502 -0.0021 0.9839 0.0475
-6.500 -0.7053 0.01058 0.00471 -0.0037 0.9828 0.0547
-6.250 -0.6788 0.01029 0.00444 -0.0035 0.9785 0.0618
-6.000 -0.6475 0.00996 0.00417 -0.0044 0.9758 0.0720
-5.750 -0.6149 0.00960 0.00389 -0.0057 0.9737 0.0870
-5.500 -0.5814 0.00923 0.00362 -0.0071 0.9721 0.1052
-5.250 -0.5466 0.00887 0.00336 -0.0088 0.9708 0.1265
-5.000 -0.5142 0.00851 0.00311 -0.0100 0.9685 0.1528
-4.750 -0.4880 0.00812 0.00288 -0.0098 0.9628 0.1856
-4.500 -0.4572 0.00771 0.00264 -0.0107 0.9589 0.2251
-4.250 -0.4243 0.00734 0.00242 -0.0119 0.9558 0.2623
-4.000 -0.4001 0.00705 0.00226 -0.0112 0.9478 0.2963
-3.750 -0.3706 0.00674 0.00208 -0.0116 0.9419 0.3351
-3.500 -0.3460 0.00647 0.00194 -0.0110 0.9334 0.3726
-3.250 -0.3181 0.00622 0.00180 -0.0110 0.9258 0.4078
-3.000 -0.2939 0.00602 0.00169 -0.0102 0.9157 0.4396
-2.750 -0.2682 0.00583 0.00158 -0.0097 0.9062 0.4740
-2.500 -0.2438 0.00563 0.00148 -0.0089 0.8954 0.5102
-2.250 -0.2196 0.00548 0.00141 -0.0080 0.8839 0.5414
-2.000 -0.1950 0.00535 0.00134 -0.0072 0.8723 0.5709
-1.750 -0.1701 0.00525 0.00128 -0.0064 0.8604 0.5979
-1.500 -0.1458 0.00515 0.00123 -0.0055 0.8475 0.6236
-1.250 -0.1216 0.00507 0.00119 -0.0046 0.8337 0.6486
-1.000 -0.0973 0.00500 0.00116 -0.0037 0.8194 0.6726
-0.750 -0.0729 0.00495 0.00113 -0.0028 0.8043 0.6944
-0.500 -0.0488 0.00492 0.00111 -0.0018 0.7881 0.7157
-0.250 -0.0244 0.00490 0.00110 -0.0009 0.7712 0.7353
0.000 0.0000 0.00491 0.00110 0.0000 0.7536 0.7537
0.250 0.0244 0.00491 0.00110 0.0009 0.7351 0.7709
0.500 0.0487 0.00492 0.00111 0.0018 0.7154 0.7879
0.750 0.0729 0.00495 0.00113 0.0028 0.6944 0.8042
1.000 0.0972 0.00500 0.00116 0.0037 0.6721 0.8194
1.250 0.1216 0.00507 0.00119 0.0046 0.6488 0.8336
1.500 0.1458 0.00515 0.00123 0.0055 0.6236 0.8476
1.750 0.1701 0.00524 0.00128 0.0064 0.5981 0.8604
2.000 0.1948 0.00535 0.00134 0.0072 0.5701 0.8724
2.250 0.2194 0.00548 0.00141 0.0080 0.5407 0.8840
2.500 0.2437 0.00563 0.00148 0.0089 0.5103 0.8954
2.750 0.2682 0.00583 0.00158 0.0097 0.4742 0.9062
3.000 0.2938 0.00603 0.00169 0.0102 0.4391 0.9158
3.250 0.3181 0.00622 0.00179 0.0110 0.4078 0.9258
3.500 0.3460 0.00647 0.00194 0.0110 0.3726 0.9334
3.750 0.3706 0.00674 0.00208 0.0116 0.3354 0.9419
4.000 0.4001 0.00705 0.00226 0.0112 0.2967 0.9478
4.250 0.4242 0.00733 0.00242 0.0120 0.2631 0.9557
4.500 0.4571 0.00772 0.00264 0.0107 0.2239 0.9589
4.750 0.4882 0.00810 0.00287 0.0098 0.1876 0.9628
5.250 0.5467 0.00887 0.00336 0.0088 0.1264 0.9708
5.500 0.5814 0.00923 0.00362 0.0071 0.1053 0.9721
5.750 0.6149 0.00960 0.00389 0.0057 0.0870 0.9737
6.000 0.6475 0.00996 0.00417 0.0044 0.0717 0.9758
6.250 0.6788 0.01029 0.00444 0.0035 0.0618 0.9785
6.500 0.7053 0.01058 0.00471 0.0037 0.0547 0.9828
6.750 0.7396 0.01091 0.00501 0.0021 0.0474 0.9838
7.000 0.7730 0.01130 0.00535 0.0006 0.0404 0.9852
7.250 0.8062 0.01160 0.00564 -0.0008 0.0362 0.9868
7.500 0.8379 0.01199 0.00602 -0.0019 0.0317 0.9888
7.750 0.8685 0.01238 0.00639 -0.0027 0.0282 0.9912
8.000 0.8972 0.01281 0.00683 -0.0032 0.0257 0.9937
8.250 0.9299 0.01315 0.00720 -0.0045 0.0241 0.9949
8.500 0.9614 0.01362 0.00767 -0.0057 0.0226 0.9965
8.750 0.9917 0.01421 0.00831 -0.0066 0.0213 0.9983
9.000 1.0232 0.01461 0.00874 -0.0078 0.0206 0.9997
9.250 1.0414 0.01498 0.00916 -0.0061 0.0199 1.0000
9.500 1.0550 0.01533 0.00954 -0.0035 0.0193 1.0000
9.750 1.0684 0.01569 0.00992 -0.0009 0.0187 1.0000
10.000 1.0798 0.01615 0.01041 0.0020 0.0182 1.0000
10.250 1.0878 0.01679 0.01110 0.0055 0.0176 1.0000
10.500 1.0935 0.01755 0.01194 0.0094 0.0172 1.0000
10.750 1.1049 0.01802 0.01247 0.0123 0.0170 1.0000
11.000 1.1166 0.01849 0.01299 0.0151 0.0168 1.0000
11.250 1.1275 0.01897 0.01353 0.0180 0.0165 1.0000
11.500 1.1336 0.01947 0.01409 0.0218 0.0163 1.0000
11.750 1.1410 0.01997 0.01463 0.0252 0.0160 1.0000
12.000 1.1488 0.02057 0.01529 0.0284 0.0157 1.0000
12.250 1.1588 0.02115 0.01592 0.0310 0.0153 1.0000
12.500 1.1688 0.02179 0.01661 0.0335 0.0150 1.0000
12.750 1.1769 0.02261 0.01748 0.0360 0.0147 1.0000
13.000 1.1855 0.02344 0.01837 0.0382 0.0145 1.0000
13.250 1.1898 0.02461 0.01961 0.0407 0.0142 1.0000
13.500 1.1832 0.02666 0.02177 0.0438 0.0138 1.0000
13.750 1.1803 0.02864 0.02388 0.0462 0.0137 1.0000
14.000 1.1899 0.02970 0.02502 0.0473 0.0136 1.0000
14.250 1.1968 0.03105 0.02647 0.0484 0.0134 1.0000
14.500 1.2004 0.03279 0.02830 0.0495 0.0133 1.0000
14.750 1.2048 0.03455 0.03016 0.0502 0.0132 1.0000
15.000 1.2077 0.03656 0.03227 0.0506 0.0130 1.0000
15.250 1.2095 0.03881 0.03462 0.0507 0.0128 1.0000
15.500 1.2137 0.04092 0.03682 0.0505 0.0125 1.0000
15.750 1.2103 0.04402 0.04004 0.0501 0.0125 1.0000
16.000 1.2096 0.04697 0.04308 0.0492 0.0123 1.0000
16.250 1.2060 0.05045 0.04666 0.0480 0.0121 1.0000
16.500 1.1991 0.05450 0.05083 0.0464 0.0120 1.0000
16.750 1.1894 0.05915 0.05560 0.0443 0.0119 1.0000
17.000 1.1787 0.06413 0.06071 0.0419 0.0119 1.0000
17.250 1.1650 0.06980 0.06650 0.0390 0.0118 1.0000
17.500 1.1578 0.07468 0.07145 0.0363 0.0116 1.0000
17.750 1.1383 0.08156 0.07847 0.0327 0.0117 1.0000
18.000 1.1205 0.08839 0.08542 0.0291 0.0117 1.0000
18.250 1.0991 0.09597 0.09312 0.0251 0.0116 1.0000
18.500 1.0744 0.10439 0.10169 0.0206 0.0117 1.0000
18.750 1.0513 0.11268 0.11010 0.0162 0.0116 1.0000
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