EPPLER EA 6(-1)-012 AIRFOIL (ea61012-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: EPPLER EA 6(-1)-012 AIRFOIL (ea61012-il) Reynolds number: 1,000,000 Max Cl/Cd: 70.66 at α=11.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-ea61012-il-1000000-n5.txt Download as CSV file: xf-ea61012-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: EPPLER EA 6(-1)-012 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.250 -1.4341 0.06704 0.06330 -0.0290 1.0000 0.0129
-19.000 -1.4497 0.06133 0.05746 -0.0319 1.0000 0.0132
-18.750 -1.4613 0.05651 0.05253 -0.0340 1.0000 0.0134
-18.500 -1.4701 0.05235 0.04826 -0.0355 1.0000 0.0139
-18.250 -1.4764 0.04872 0.04454 -0.0366 1.0000 0.0143
-18.000 -1.4806 0.04557 0.04129 -0.0372 1.0000 0.0148
-17.750 -1.4820 0.04282 0.03845 -0.0376 1.0000 0.0152
-17.500 -1.4822 0.04030 0.03584 -0.0378 1.0000 0.0158
-17.250 -1.4805 0.03806 0.03352 -0.0377 1.0000 0.0162
-17.000 -1.4783 0.03591 0.03132 -0.0375 1.0000 0.0169
-16.750 -1.4750 0.03397 0.02932 -0.0371 1.0000 0.0178
-16.500 -1.4693 0.03227 0.02757 -0.0366 1.0000 0.0186
-16.250 -1.4624 0.03075 0.02598 -0.0360 1.0000 0.0193
-16.000 -1.4542 0.02938 0.02455 -0.0353 1.0000 0.0201
-15.750 -1.4452 0.02810 0.02320 -0.0345 1.0000 0.0205
-15.500 -1.4359 0.02688 0.02195 -0.0336 1.0000 0.0216
-15.250 -1.4249 0.02582 0.02087 -0.0327 1.0000 0.0227
-15.000 -1.4131 0.02486 0.01988 -0.0318 1.0000 0.0237
-14.750 -1.4009 0.02395 0.01893 -0.0308 1.0000 0.0244
-14.500 -1.3883 0.02311 0.01803 -0.0298 1.0000 0.0251
-14.250 -1.3754 0.02234 0.01720 -0.0286 1.0000 0.0256
-14.000 -1.3622 0.02162 0.01642 -0.0273 1.0000 0.0260
-13.750 -1.3492 0.02095 0.01570 -0.0259 1.0000 0.0265
-13.500 -1.3372 0.02025 0.01496 -0.0241 1.0000 0.0271
-13.250 -1.3231 0.01972 0.01442 -0.0224 1.0000 0.0281
-13.000 -1.3082 0.01926 0.01395 -0.0207 1.0000 0.0289
-12.750 -1.2930 0.01883 0.01349 -0.0190 1.0000 0.0296
-12.500 -1.2754 0.01843 0.01306 -0.0176 1.0000 0.0303
-12.250 -1.2563 0.01801 0.01261 -0.0165 1.0000 0.0310
-12.000 -1.2361 0.01763 0.01220 -0.0155 1.0000 0.0316
-11.750 -1.2155 0.01725 0.01179 -0.0146 1.0000 0.0322
-11.500 -1.1876 0.01685 0.01134 -0.0151 0.9608 0.0327
-11.250 -1.1519 0.01663 0.01088 -0.0172 0.8725 0.0332
-11.000 -1.1315 0.01641 0.01053 -0.0160 0.8496 0.0334
-10.750 -1.1107 0.01607 0.01011 -0.0150 0.8384 0.0340
-10.500 -1.0905 0.01562 0.00960 -0.0139 0.8300 0.0353
-10.250 -1.0679 0.01530 0.00925 -0.0132 0.8235 0.0362
-10.000 -1.0452 0.01498 0.00888 -0.0124 0.8175 0.0368
-9.750 -1.0216 0.01470 0.00857 -0.0118 0.8126 0.0375
-9.500 -0.9977 0.01442 0.00825 -0.0113 0.8079 0.0382
-9.250 -0.9737 0.01413 0.00792 -0.0107 0.8037 0.0388
-8.750 -0.9251 0.01356 0.00727 -0.0096 0.7966 0.0398
-8.500 -0.9003 0.01328 0.00695 -0.0092 0.7930 0.0403
-8.250 -0.8755 0.01300 0.00663 -0.0087 0.7894 0.0407
-8.000 -0.8503 0.01276 0.00635 -0.0083 0.7859 0.0412
-7.750 -0.8249 0.01252 0.00607 -0.0079 0.7826 0.0415
-7.500 -0.7990 0.01230 0.00583 -0.0076 0.7791 0.0418
-7.250 -0.7729 0.01210 0.00560 -0.0073 0.7755 0.0421
-7.000 -0.7481 0.01176 0.00522 -0.0068 0.7721 0.0430
-6.500 -0.6966 0.01123 0.00466 -0.0060 0.7660 0.0450
-6.250 -0.6703 0.01101 0.00443 -0.0058 0.7626 0.0459
-6.000 -0.6438 0.01080 0.00422 -0.0055 0.7591 0.0468
-5.750 -0.6171 0.01062 0.00401 -0.0052 0.7558 0.0476
-5.500 -0.5904 0.01044 0.00382 -0.0050 0.7527 0.0485
-5.250 -0.5633 0.01026 0.00363 -0.0048 0.7493 0.0492
-5.000 -0.5361 0.01010 0.00346 -0.0047 0.7454 0.0499
-4.750 -0.5089 0.00995 0.00329 -0.0045 0.7415 0.0505
-4.500 -0.4818 0.00981 0.00313 -0.0043 0.7380 0.0513
-4.250 -0.4546 0.00961 0.00294 -0.0041 0.7341 0.0532
-4.000 -0.4274 0.00944 0.00278 -0.0039 0.7290 0.0549
-3.750 -0.4001 0.00929 0.00263 -0.0037 0.7238 0.0565
-3.500 -0.3725 0.00915 0.00249 -0.0036 0.7189 0.0582
-3.250 -0.3448 0.00903 0.00237 -0.0035 0.7134 0.0597
-3.000 -0.3174 0.00889 0.00223 -0.0033 0.7083 0.0630
-2.750 -0.2898 0.00875 0.00212 -0.0032 0.7038 0.0670
-2.500 -0.2622 0.00860 0.00200 -0.0031 0.6985 0.0737
-2.250 -0.2350 0.00842 0.00188 -0.0029 0.6932 0.0884
-2.000 -0.2085 0.00813 0.00174 -0.0026 0.6878 0.1245
-1.750 -0.1822 0.00782 0.00161 -0.0024 0.6824 0.1718
-1.500 -0.1559 0.00755 0.00148 -0.0021 0.6746 0.2164
-1.250 -0.1297 0.00722 0.00136 -0.0018 0.6667 0.2730
-1.000 -0.1040 0.00688 0.00124 -0.0015 0.6586 0.3433
-0.750 -0.0776 0.00659 0.00115 -0.0012 0.6482 0.4010
-0.500 -0.0529 0.00618 0.00101 -0.0007 0.6330 0.4868
-0.250 -0.0273 0.00596 0.00098 -0.0002 0.6134 0.5643
0.000 0.0000 0.00594 0.00098 0.0000 0.5934 0.5935
0.250 0.0273 0.00596 0.00098 0.0002 0.5641 0.6128
0.500 0.0530 0.00616 0.00101 0.0007 0.4916 0.6338
0.750 0.0776 0.00659 0.00115 0.0012 0.4009 0.6484
1.000 0.1040 0.00688 0.00124 0.0015 0.3433 0.6585
1.250 0.1296 0.00723 0.00136 0.0018 0.2720 0.6663
1.750 0.1822 0.00781 0.00160 0.0024 0.1730 0.6824
2.000 0.2086 0.00812 0.00173 0.0026 0.1261 0.6879
2.250 0.2350 0.00842 0.00188 0.0029 0.0886 0.6932
2.500 0.2622 0.00860 0.00200 0.0031 0.0738 0.6985
2.750 0.2898 0.00875 0.00212 0.0032 0.0670 0.7039
3.000 0.3174 0.00889 0.00223 0.0033 0.0630 0.7083
3.250 0.3448 0.00903 0.00237 0.0035 0.0597 0.7134
3.500 0.3726 0.00915 0.00249 0.0036 0.0582 0.7189
3.750 0.4001 0.00929 0.00263 0.0037 0.0565 0.7238
4.000 0.4274 0.00944 0.00278 0.0039 0.0549 0.7291
4.250 0.4547 0.00961 0.00294 0.0041 0.0533 0.7340
4.500 0.4818 0.00981 0.00313 0.0043 0.0513 0.7379
4.750 0.5089 0.00995 0.00329 0.0045 0.0506 0.7415
5.000 0.5361 0.01010 0.00346 0.0047 0.0500 0.7454
5.250 0.5633 0.01026 0.00363 0.0048 0.0492 0.7493
5.500 0.5904 0.01044 0.00382 0.0050 0.0485 0.7527
5.750 0.6172 0.01062 0.00402 0.0052 0.0476 0.7558
6.000 0.6438 0.01080 0.00422 0.0055 0.0468 0.7591
6.250 0.6703 0.01101 0.00443 0.0058 0.0459 0.7626
6.500 0.6967 0.01123 0.00466 0.0060 0.0450 0.7660
7.000 0.7482 0.01176 0.00522 0.0068 0.0431 0.7721
7.250 0.7729 0.01211 0.00560 0.0073 0.0421 0.7755
7.500 0.7990 0.01230 0.00583 0.0076 0.0418 0.7791
7.750 0.8249 0.01252 0.00607 0.0079 0.0415 0.7826
8.000 0.8504 0.01276 0.00635 0.0083 0.0412 0.7859
8.250 0.8755 0.01301 0.00664 0.0087 0.0408 0.7894
8.500 0.9004 0.01327 0.00695 0.0092 0.0403 0.7930
8.750 0.9252 0.01355 0.00726 0.0096 0.0398 0.7966
9.250 0.9739 0.01412 0.00791 0.0107 0.0387 0.8037
9.500 0.9977 0.01442 0.00825 0.0113 0.0382 0.8079
9.750 1.0218 0.01469 0.00856 0.0118 0.0375 0.8126
10.000 1.0453 0.01498 0.00888 0.0124 0.0368 0.8175
10.250 1.0681 0.01528 0.00923 0.0131 0.0361 0.8235
10.500 1.0907 0.01561 0.00958 0.0139 0.0352 0.8300
10.750 1.1107 0.01607 0.01011 0.0150 0.0339 0.8384
11.000 1.1315 0.01641 0.01053 0.0160 0.0334 0.8496
11.250 1.1519 0.01663 0.01089 0.0172 0.0332 0.8723
11.500 1.1872 0.01686 0.01136 0.0152 0.0327 0.9601
11.750 1.2160 0.01721 0.01175 0.0145 0.0321 1.0000
12.000 1.2365 0.01760 0.01217 0.0154 0.0315 1.0000
12.250 1.2564 0.01801 0.01261 0.0165 0.0309 1.0000
12.500 1.2759 0.01840 0.01303 0.0175 0.0302 1.0000
12.750 1.2933 0.01883 0.01349 0.0189 0.0296 1.0000
13.000 1.3088 0.01925 0.01393 0.0206 0.0288 1.0000
13.250 1.3235 0.01971 0.01441 0.0224 0.0281 1.0000
13.500 1.3374 0.02026 0.01497 0.0241 0.0272 1.0000
13.750 1.3494 0.02096 0.01571 0.0258 0.0263 1.0000
14.000 1.3627 0.02162 0.01642 0.0272 0.0260 1.0000
14.250 1.3759 0.02233 0.01719 0.0285 0.0256 1.0000
14.500 1.3887 0.02311 0.01803 0.0297 0.0251 1.0000
14.750 1.4016 0.02394 0.01891 0.0307 0.0244 1.0000
15.000 1.4137 0.02485 0.01988 0.0317 0.0237 1.0000
15.250 1.4257 0.02580 0.02086 0.0326 0.0227 1.0000
15.500 1.4365 0.02688 0.02197 0.0335 0.0220 1.0000
15.750 1.4464 0.02806 0.02317 0.0343 0.0209 1.0000
16.000 1.4553 0.02935 0.02451 0.0351 0.0200 1.0000
16.250 1.4636 0.03072 0.02595 0.0358 0.0194 1.0000
16.500 1.4707 0.03224 0.02753 0.0364 0.0186 1.0000
16.750 1.4762 0.03394 0.02929 0.0369 0.0178 1.0000
17.000 1.4800 0.03585 0.03126 0.0373 0.0169 1.0000
17.250 1.4822 0.03799 0.03345 0.0375 0.0163 1.0000
17.500 1.4840 0.04024 0.03579 0.0376 0.0157 1.0000
17.750 1.4844 0.04269 0.03833 0.0374 0.0153 1.0000
18.000 1.4824 0.04551 0.04123 0.0370 0.0147 1.0000
18.250 1.4787 0.04862 0.04443 0.0364 0.0143 1.0000
18.500 1.4717 0.05233 0.04823 0.0353 0.0138 1.0000
18.750 1.4636 0.05640 0.05242 0.0338 0.0135 1.0000
19.000 1.4521 0.06119 0.05732 0.0317 0.0132 1.0000
19.250 1.4383 0.06664 0.06290 0.0290 0.0130 1.0000
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