NACA 2414 (n2414-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 2414 (n2414-il) Reynolds number: 1,000,000 Max Cl/Cd: 90.04 at α=5.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-n2414-il-1000000-n5.txt Download as CSV file: xf-n2414-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NACA 2414
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
------ -------- --------- --------- -------- -------- --------
-18.500 -1.1513 0.08637 0.08297 -0.0417 1.0000 0.0159
-18.250 -1.2034 0.07478 0.07120 -0.0481 1.0000 0.0158
-18.000 -1.2484 0.06428 0.06051 -0.0541 1.0000 0.0157
-17.750 -1.2803 0.05571 0.05176 -0.0592 1.0000 0.0157
-17.500 -1.3010 0.04887 0.04476 -0.0636 1.0000 0.0158
-17.250 -1.3131 0.04353 0.03927 -0.0670 1.0000 0.0158
-17.000 -1.3192 0.03930 0.03491 -0.0696 1.0000 0.0159
-16.750 -1.3211 0.03592 0.03142 -0.0714 1.0000 0.0160
-16.500 -1.3213 0.03305 0.02844 -0.0725 1.0000 0.0161
-16.250 -1.3213 0.03053 0.02582 -0.0729 1.0000 0.0163
-16.000 -1.3186 0.02855 0.02375 -0.0726 1.0000 0.0165
-15.750 -1.3135 0.02697 0.02209 -0.0719 1.0000 0.0168
-15.500 -1.3068 0.02568 0.02074 -0.0707 1.0000 0.0170
-15.250 -1.2990 0.02460 0.01960 -0.0692 1.0000 0.0173
-15.000 -1.2907 0.02368 0.01863 -0.0672 1.0000 0.0176
-14.750 -1.2830 0.02291 0.01779 -0.0648 1.0000 0.0178
-14.500 -1.2746 0.02223 0.01706 -0.0622 1.0000 0.0181
-14.250 -1.2633 0.02160 0.01637 -0.0600 1.0000 0.0184
-14.000 -1.2520 0.02102 0.01574 -0.0576 1.0000 0.0186
-13.750 -1.2402 0.02049 0.01515 -0.0552 1.0000 0.0188
-13.500 -1.2287 0.01998 0.01459 -0.0527 1.0000 0.0191
-13.250 -1.2118 0.01934 0.01392 -0.0513 0.9994 0.0195
-13.000 -1.1853 0.01870 0.01325 -0.0518 0.9979 0.0200
-12.750 -1.1579 0.01812 0.01264 -0.0523 0.9962 0.0205
-12.500 -1.1297 0.01758 0.01206 -0.0530 0.9948 0.0211
-12.250 -1.1005 0.01708 0.01151 -0.0538 0.9936 0.0217
-12.000 -1.0732 0.01663 0.01101 -0.0541 0.9916 0.0222
-11.750 -1.0457 0.01611 0.01047 -0.0546 0.9893 0.0229
-11.500 -1.0168 0.01563 0.00998 -0.0552 0.9873 0.0238
-11.250 -0.9871 0.01519 0.00952 -0.0560 0.9855 0.0246
-11.000 -0.9570 0.01479 0.00908 -0.0567 0.9837 0.0254
-10.750 -0.9275 0.01440 0.00865 -0.0574 0.9815 0.0261
-10.500 -0.9016 0.01399 0.00824 -0.0572 0.9769 0.0271
-10.250 -0.8735 0.01362 0.00785 -0.0575 0.9732 0.0281
-10.000 -0.8441 0.01328 0.00749 -0.0580 0.9701 0.0292
-9.750 -0.8182 0.01297 0.00715 -0.0577 0.9650 0.0301
-9.500 -0.7916 0.01262 0.00680 -0.0576 0.9598 0.0316
-9.250 -0.7639 0.01232 0.00647 -0.0577 0.9554 0.0330
-9.000 -0.7381 0.01206 0.00619 -0.0573 0.9488 0.0342
-8.750 -0.7118 0.01175 0.00587 -0.0570 0.9423 0.0358
-8.500 -0.6856 0.01149 0.00559 -0.0567 0.9353 0.0375
-8.250 -0.6592 0.01126 0.00533 -0.0563 0.9266 0.0390
-8.000 -0.6331 0.01099 0.00505 -0.0560 0.9179 0.0412
-7.750 -0.6067 0.01077 0.00480 -0.0556 0.9085 0.0436
-7.500 -0.5800 0.01055 0.00456 -0.0554 0.8994 0.0459
-7.250 -0.5534 0.01034 0.00432 -0.0551 0.8902 0.0486
-7.000 -0.5263 0.01015 0.00411 -0.0549 0.8808 0.0512
-6.750 -0.4996 0.00994 0.00389 -0.0546 0.8712 0.0550
-6.500 -0.4725 0.00977 0.00369 -0.0544 0.8608 0.0585
-6.250 -0.4455 0.00958 0.00349 -0.0542 0.8506 0.0631
-6.000 -0.4183 0.00943 0.00331 -0.0539 0.8394 0.0672
-5.750 -0.3910 0.00926 0.00314 -0.0538 0.8282 0.0725
-5.500 -0.3639 0.00911 0.00297 -0.0536 0.8169 0.0779
-5.250 -0.3365 0.00899 0.00282 -0.0534 0.8045 0.0833
-5.000 -0.3091 0.00884 0.00267 -0.0532 0.7921 0.0905
-4.750 -0.2817 0.00872 0.00253 -0.0530 0.7797 0.0973
-4.500 -0.2544 0.00861 0.00240 -0.0529 0.7664 0.1049
-4.250 -0.2269 0.00849 0.00227 -0.0527 0.7527 0.1140
-4.000 -0.1993 0.00839 0.00216 -0.0526 0.7395 0.1235
-3.750 -0.1718 0.00830 0.00206 -0.0524 0.7258 0.1340
-3.500 -0.1445 0.00820 0.00196 -0.0523 0.7115 0.1468
-3.000 -0.0895 0.00802 0.00179 -0.0520 0.6823 0.1733
-2.750 -0.0619 0.00795 0.00172 -0.0519 0.6675 0.1869
-2.500 -0.0342 0.00789 0.00166 -0.0517 0.6533 0.2016
-2.250 -0.0067 0.00783 0.00161 -0.0516 0.6386 0.2174
-2.000 0.0208 0.00778 0.00156 -0.0515 0.6241 0.2350
-1.750 0.0485 0.00773 0.00152 -0.0514 0.6095 0.2522
-1.500 0.0763 0.00768 0.00149 -0.0513 0.5957 0.2705
-1.250 0.1040 0.00764 0.00146 -0.0512 0.5822 0.2892
-1.000 0.1316 0.00761 0.00145 -0.0511 0.5687 0.3098
-0.500 0.1871 0.00755 0.00143 -0.0510 0.5419 0.3529
-0.250 0.2147 0.00751 0.00143 -0.0509 0.5296 0.3775
0.000 0.2422 0.00748 0.00144 -0.0508 0.5171 0.4054
0.250 0.2696 0.00742 0.00145 -0.0506 0.5047 0.4399
0.500 0.2971 0.00736 0.00147 -0.0505 0.4936 0.4756
0.750 0.3245 0.00733 0.00150 -0.0504 0.4826 0.5113
1.000 0.3520 0.00729 0.00154 -0.0503 0.4717 0.5459
1.250 0.3795 0.00727 0.00158 -0.0502 0.4615 0.5780
1.500 0.4068 0.00728 0.00163 -0.0500 0.4504 0.6090
1.750 0.4343 0.00726 0.00169 -0.0499 0.4399 0.6410
2.000 0.4615 0.00727 0.00175 -0.0497 0.4283 0.6721
2.250 0.4883 0.00730 0.00183 -0.0494 0.4153 0.7038
2.500 0.5154 0.00731 0.00190 -0.0492 0.4026 0.7353
2.750 0.5421 0.00734 0.00199 -0.0489 0.3900 0.7675
3.000 0.5683 0.00739 0.00209 -0.0484 0.3764 0.8003
3.250 0.5943 0.00746 0.00220 -0.0479 0.3613 0.8313
3.500 0.6197 0.00755 0.00233 -0.0473 0.3456 0.8621
3.750 0.6447 0.00768 0.00246 -0.0466 0.3278 0.8900
4.000 0.6696 0.00784 0.00261 -0.0459 0.3098 0.9157
4.500 0.7222 0.00825 0.00293 -0.0451 0.2738 0.9565
4.750 0.7531 0.00854 0.00313 -0.0458 0.2522 0.9735
5.000 0.7854 0.00885 0.00333 -0.0468 0.2321 0.9844
5.250 0.8170 0.00913 0.00353 -0.0478 0.2139 0.9904
5.500 0.8478 0.00943 0.00374 -0.0486 0.1959 0.9942
5.750 0.8797 0.00977 0.00397 -0.0497 0.1766 0.9968
6.000 0.9105 0.01014 0.00423 -0.0506 0.1574 0.9997
6.250 0.9324 0.01045 0.00446 -0.0495 0.1424 1.0000
6.500 0.9533 0.01075 0.00469 -0.0482 0.1297 1.0000
6.750 0.9748 0.01104 0.00492 -0.0470 0.1187 1.0000
7.000 0.9969 0.01133 0.00517 -0.0459 0.1088 1.0000
7.250 1.0190 0.01166 0.00543 -0.0449 0.0990 1.0000
7.500 1.0412 0.01199 0.00571 -0.0440 0.0902 1.0000
7.750 1.0636 0.01232 0.00600 -0.0430 0.0825 1.0000
8.000 1.0863 0.01264 0.00629 -0.0422 0.0758 1.0000
8.250 1.1086 0.01299 0.00660 -0.0413 0.0697 1.0000
8.500 1.1307 0.01334 0.00693 -0.0404 0.0641 1.0000
8.750 1.1529 0.01368 0.00725 -0.0395 0.0594 1.0000
9.000 1.1744 0.01407 0.00761 -0.0385 0.0548 1.0000
9.250 1.1961 0.01442 0.00795 -0.0375 0.0511 1.0000
9.500 1.2171 0.01481 0.00833 -0.0365 0.0478 1.0000
9.750 1.2379 0.01519 0.00870 -0.0354 0.0448 1.0000
10.000 1.2576 0.01561 0.00912 -0.0342 0.0421 1.0000
10.250 1.2764 0.01599 0.00950 -0.0327 0.0399 1.0000
10.500 1.2938 0.01643 0.00994 -0.0311 0.0378 1.0000
10.750 1.3114 0.01687 0.01040 -0.0296 0.0362 1.0000
11.000 1.3289 0.01733 0.01087 -0.0281 0.0345 1.0000
11.250 1.3453 0.01786 0.01141 -0.0265 0.0328 1.0000
11.500 1.3619 0.01839 0.01196 -0.0250 0.0314 1.0000
11.750 1.3783 0.01894 0.01254 -0.0235 0.0300 1.0000
12.000 1.3935 0.01957 0.01319 -0.0220 0.0287 1.0000
12.250 1.4083 0.02025 0.01388 -0.0204 0.0276 1.0000
12.500 1.4236 0.02091 0.01458 -0.0191 0.0267 1.0000
12.750 1.4379 0.02165 0.01535 -0.0176 0.0258 1.0000
13.000 1.4510 0.02248 0.01621 -0.0162 0.0249 1.0000
13.250 1.4631 0.02341 0.01717 -0.0147 0.0240 1.0000
13.500 1.4762 0.02430 0.01812 -0.0135 0.0234 1.0000
13.750 1.4884 0.02528 0.01914 -0.0122 0.0227 1.0000
14.000 1.4995 0.02639 0.02029 -0.0110 0.0219 1.0000
14.250 1.5094 0.02762 0.02156 -0.0098 0.0212 1.0000
14.500 1.5179 0.02900 0.02298 -0.0087 0.0206 1.0000
14.750 1.5274 0.03035 0.02440 -0.0077 0.0201 1.0000
15.000 1.5361 0.03182 0.02593 -0.0069 0.0196 1.0000
15.250 1.5437 0.03343 0.02760 -0.0061 0.0192 1.0000
15.500 1.5501 0.03520 0.02943 -0.0054 0.0187 1.0000
15.750 1.5552 0.03716 0.03145 -0.0048 0.0183 1.0000
16.000 1.5590 0.03932 0.03367 -0.0043 0.0178 1.0000
16.250 1.5610 0.04171 0.03612 -0.0039 0.0174 1.0000
16.500 1.5637 0.04411 0.03861 -0.0038 0.0172 1.0000
16.750 1.5661 0.04663 0.04121 -0.0037 0.0169 1.0000
17.000 1.5671 0.04937 0.04404 -0.0038 0.0166 1.0000
17.250 1.5666 0.05235 0.04710 -0.0041 0.0164 1.0000
17.500 1.5649 0.05557 0.05039 -0.0045 0.0161 1.0000
17.750 1.5620 0.05900 0.05391 -0.0051 0.0158 1.0000
18.000 1.5577 0.06265 0.05765 -0.0058 0.0156 1.0000
18.250 1.5517 0.06659 0.06168 -0.0067 0.0154 1.0000
18.500 1.5442 0.07083 0.06601 -0.0077 0.0151 1.0000
18.750 1.5353 0.07534 0.07061 -0.0090 0.0149 1.0000
19.000 1.5245 0.08014 0.07550 -0.0104 0.0147 1.0000
19.250 1.5127 0.08519 0.08065 -0.0120 0.0146 1.0000
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