NACA 2414 (n2414-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: NACA 2414 (n2414-il) Reynolds number: 1,000,000 Max Cl/Cd: 103.69 at α=5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-n2414-il-1000000.txt Download as CSV file: xf-n2414-il-1000000.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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.250 -1.1298 0.08491 0.08162 -0.0429 1.0000 0.0199
-18.000 -1.1553 0.07749 0.07409 -0.0469 1.0000 0.0199
-17.750 -1.1815 0.07006 0.06653 -0.0510 1.0000 0.0199
-17.500 -1.2057 0.06285 0.05919 -0.0551 1.0000 0.0200
-17.250 -1.2260 0.05617 0.05238 -0.0590 1.0000 0.0200
-17.000 -1.2413 0.05018 0.04627 -0.0627 1.0000 0.0201
-16.750 -1.2517 0.04505 0.04101 -0.0660 1.0000 0.0202
-16.500 -1.2577 0.04071 0.03656 -0.0687 1.0000 0.0204
-16.250 -1.2599 0.03715 0.03289 -0.0707 1.0000 0.0206
-16.000 -1.2595 0.03419 0.02983 -0.0721 1.0000 0.0208
-15.750 -1.2572 0.03174 0.02728 -0.0728 1.0000 0.0210
-15.500 -1.2531 0.02972 0.02516 -0.0729 1.0000 0.0212
-15.250 -1.2475 0.02806 0.02341 -0.0724 1.0000 0.0215
-15.000 -1.2401 0.02672 0.02199 -0.0715 1.0000 0.0217
-14.750 -1.2315 0.02560 0.02079 -0.0702 1.0000 0.0220
-14.500 -1.2211 0.02473 0.01984 -0.0687 1.0000 0.0222
-14.250 -1.2229 0.02346 0.01850 -0.0654 1.0000 0.0226
-14.000 -1.2227 0.02251 0.01749 -0.0617 1.0000 0.0229
-13.750 -1.2157 0.02176 0.01670 -0.0588 1.0000 0.0233
-13.500 -1.2065 0.02114 0.01604 -0.0561 1.0000 0.0237
-13.250 -1.1965 0.02060 0.01546 -0.0533 1.0000 0.0241
-13.000 -1.1862 0.02009 0.01490 -0.0505 1.0000 0.0245
-12.750 -1.1752 0.01961 0.01438 -0.0478 1.0000 0.0249
-12.500 -1.1634 0.01916 0.01387 -0.0452 1.0000 0.0253
-12.250 -1.1503 0.01876 0.01342 -0.0427 1.0000 0.0257
-12.000 -1.1298 0.01801 0.01262 -0.0420 0.9993 0.0263
-11.750 -1.1006 0.01731 0.01189 -0.0430 0.9979 0.0272
-11.500 -1.0696 0.01680 0.01136 -0.0441 0.9965 0.0281
-11.250 -1.0377 0.01637 0.01089 -0.0453 0.9952 0.0290
-11.000 -1.0047 0.01601 0.01048 -0.0467 0.9942 0.0298
-10.750 -0.9748 0.01528 0.00974 -0.0477 0.9927 0.0312
-10.500 -0.9448 0.01484 0.00929 -0.0485 0.9904 0.0324
-10.250 -0.9130 0.01447 0.00888 -0.0495 0.9885 0.0336
-10.000 -0.8807 0.01403 0.00841 -0.0507 0.9868 0.0348
-9.750 -0.8481 0.01354 0.00792 -0.0521 0.9853 0.0365
-9.500 -0.8139 0.01319 0.00756 -0.0536 0.9842 0.0382
-9.250 -0.7794 0.01282 0.00716 -0.0552 0.9833 0.0399
-9.000 -0.7448 0.01239 0.00675 -0.0568 0.9824 0.0422
-8.750 -0.7166 0.01211 0.00645 -0.0569 0.9782 0.0440
-8.500 -0.6857 0.01172 0.00606 -0.0577 0.9749 0.0464
-8.250 -0.6538 0.01138 0.00573 -0.0586 0.9719 0.0491
-8.000 -0.6238 0.01110 0.00543 -0.0590 0.9682 0.0515
-7.750 -0.5983 0.01077 0.00513 -0.0586 0.9618 0.0550
-7.500 -0.5699 0.01055 0.00488 -0.0586 0.9570 0.0579
-7.250 -0.5442 0.01023 0.00459 -0.0581 0.9509 0.0622
-7.000 -0.5176 0.01003 0.00437 -0.0577 0.9444 0.0658
-6.750 -0.4910 0.00974 0.00411 -0.0574 0.9385 0.0714
-6.500 -0.4648 0.00953 0.00390 -0.0570 0.9308 0.0765
-6.250 -0.4379 0.00930 0.00368 -0.0567 0.9241 0.0826
-6.000 -0.4114 0.00908 0.00348 -0.0563 0.9160 0.0895
-5.750 -0.3843 0.00890 0.00329 -0.0560 0.9082 0.0964
-5.500 -0.3574 0.00869 0.00311 -0.0558 0.8996 0.1052
-5.250 -0.3303 0.00850 0.00293 -0.0555 0.8909 0.1145
-5.000 -0.3031 0.00832 0.00278 -0.0553 0.8815 0.1248
-4.750 -0.2758 0.00817 0.00262 -0.0550 0.8722 0.1358
-4.500 -0.2483 0.00801 0.00248 -0.0548 0.8617 0.1477
-4.250 -0.2210 0.00785 0.00235 -0.0546 0.8514 0.1620
-4.000 -0.1937 0.00770 0.00223 -0.0544 0.8403 0.1770
-3.750 -0.1661 0.00756 0.00212 -0.0543 0.8288 0.1932
-3.500 -0.1387 0.00744 0.00201 -0.0541 0.8170 0.2105
-3.250 -0.1112 0.00733 0.00192 -0.0539 0.8043 0.2281
-3.000 -0.0837 0.00721 0.00183 -0.0537 0.7913 0.2472
-2.750 -0.0562 0.00711 0.00175 -0.0536 0.7780 0.2670
-2.500 -0.0288 0.00702 0.00168 -0.0534 0.7642 0.2883
-2.250 -0.0015 0.00694 0.00162 -0.0532 0.7497 0.3106
-1.750 0.0536 0.00677 0.00152 -0.0528 0.7200 0.3593
-1.500 0.0810 0.00670 0.00148 -0.0527 0.7051 0.3869
-1.250 0.1081 0.00661 0.00145 -0.0525 0.6899 0.4184
-1.000 0.1351 0.00652 0.00143 -0.0522 0.6746 0.4569
-0.750 0.1620 0.00644 0.00142 -0.0520 0.6591 0.4984
-0.500 0.1889 0.00637 0.00142 -0.0517 0.6435 0.5383
-0.250 0.2161 0.00631 0.00142 -0.0515 0.6282 0.5765
0.000 0.2432 0.00625 0.00144 -0.0512 0.6131 0.6137
0.250 0.2702 0.00622 0.00147 -0.0510 0.5983 0.6508
0.500 0.2972 0.00620 0.00150 -0.0507 0.5840 0.6851
0.750 0.3240 0.00619 0.00154 -0.0503 0.5698 0.7191
1.000 0.3507 0.00618 0.00158 -0.0500 0.5559 0.7535
1.250 0.3775 0.00616 0.00164 -0.0496 0.5428 0.7869
1.500 0.4040 0.00617 0.00171 -0.0491 0.5303 0.8186
1.750 0.4303 0.00620 0.00178 -0.0486 0.5179 0.8493
2.000 0.4563 0.00624 0.00186 -0.0480 0.5052 0.8781
2.250 0.4823 0.00630 0.00195 -0.0473 0.4931 0.9041
2.500 0.5081 0.00639 0.00204 -0.0467 0.4812 0.9262
2.750 0.5347 0.00650 0.00214 -0.0462 0.4691 0.9447
3.000 0.5634 0.00661 0.00223 -0.0461 0.4573 0.9595
3.250 0.5934 0.00675 0.00232 -0.0465 0.4448 0.9709
3.500 0.6256 0.00692 0.00243 -0.0473 0.4312 0.9796
4.000 0.6973 0.00727 0.00266 -0.0508 0.3996 0.9885
4.250 0.7327 0.00747 0.00278 -0.0525 0.3830 0.9926
4.500 0.7713 0.00769 0.00291 -0.0549 0.3636 0.9952
4.750 0.8116 0.00792 0.00306 -0.0577 0.3427 0.9983
5.000 0.8451 0.00815 0.00321 -0.0590 0.3225 1.0000
5.250 0.8660 0.00836 0.00334 -0.0577 0.3049 1.0000
5.500 0.8866 0.00860 0.00349 -0.0563 0.2862 1.0000
5.750 0.9070 0.00887 0.00367 -0.0548 0.2669 1.0000
6.000 0.9274 0.00916 0.00386 -0.0534 0.2477 1.0000
6.250 0.9481 0.00944 0.00405 -0.0520 0.2288 1.0000
6.500 0.9688 0.00975 0.00427 -0.0506 0.2104 1.0000
6.750 0.9896 0.01006 0.00450 -0.0493 0.1931 1.0000
7.000 1.0106 0.01041 0.00475 -0.0481 0.1757 1.0000
7.250 1.0316 0.01078 0.00503 -0.0468 0.1586 1.0000
7.500 1.0532 0.01116 0.00532 -0.0457 0.1434 1.0000
7.750 1.0749 0.01154 0.00563 -0.0447 0.1294 1.0000
8.000 1.0966 0.01192 0.00594 -0.0437 0.1166 1.0000
8.250 1.1184 0.01231 0.00627 -0.0427 0.1053 1.0000
8.500 1.1401 0.01270 0.00661 -0.0417 0.0954 1.0000
8.750 1.1616 0.01310 0.00696 -0.0407 0.0864 1.0000
9.000 1.1828 0.01351 0.00733 -0.0396 0.0786 1.0000
9.250 1.2032 0.01396 0.00773 -0.0385 0.0715 1.0000
9.500 1.2244 0.01435 0.00811 -0.0375 0.0663 1.0000
9.750 1.2446 0.01478 0.00852 -0.0363 0.0614 1.0000
10.000 1.2640 0.01524 0.00896 -0.0350 0.0569 1.0000
10.250 1.2830 0.01565 0.00937 -0.0336 0.0535 1.0000
10.500 1.2998 0.01612 0.00984 -0.0319 0.0503 1.0000
10.750 1.3165 0.01661 0.01033 -0.0302 0.0475 1.0000
11.000 1.3335 0.01709 0.01082 -0.0286 0.0451 1.0000
11.250 1.3477 0.01774 0.01146 -0.0266 0.0424 1.0000
11.500 1.3654 0.01820 0.01197 -0.0253 0.0407 1.0000
11.750 1.3809 0.01881 0.01258 -0.0237 0.0388 1.0000
12.000 1.3935 0.01959 0.01338 -0.0218 0.0369 1.0000
12.250 1.4099 0.02017 0.01400 -0.0204 0.0357 1.0000
12.500 1.4244 0.02088 0.01474 -0.0189 0.0343 1.0000
12.750 1.4365 0.02176 0.01564 -0.0173 0.0330 1.0000
13.000 1.4478 0.02272 0.01664 -0.0156 0.0318 1.0000
13.250 1.4617 0.02354 0.01751 -0.0144 0.0309 1.0000
13.500 1.4738 0.02450 0.01852 -0.0130 0.0298 1.0000
13.750 1.4837 0.02567 0.01971 -0.0116 0.0288 1.0000
14.000 1.4897 0.02717 0.02125 -0.0101 0.0277 1.0000
14.250 1.5016 0.02828 0.02243 -0.0091 0.0271 1.0000
14.500 1.5116 0.02957 0.02378 -0.0081 0.0263 1.0000
14.750 1.5197 0.03106 0.02533 -0.0071 0.0256 1.0000
15.000 1.5256 0.03282 0.02713 -0.0062 0.0250 1.0000
15.250 1.5271 0.03503 0.02940 -0.0053 0.0243 1.0000
15.500 1.5299 0.03723 0.03168 -0.0046 0.0237 1.0000
15.750 1.5359 0.03918 0.03371 -0.0042 0.0233 1.0000
16.000 1.5399 0.04137 0.03598 -0.0039 0.0228 1.0000
16.250 1.5426 0.04378 0.03847 -0.0037 0.0224 1.0000
16.500 1.5437 0.04646 0.04122 -0.0037 0.0220 1.0000
16.750 1.5428 0.04943 0.04426 -0.0038 0.0216 1.0000
17.000 1.5388 0.05286 0.04777 -0.0041 0.0212 1.0000
17.250 1.5312 0.05684 0.05183 -0.0047 0.0209 1.0000
17.500 1.5180 0.06166 0.05676 -0.0057 0.0205 1.0000
17.750 1.5153 0.06519 0.06038 -0.0064 0.0203 1.0000
18.000 1.5119 0.06888 0.06417 -0.0073 0.0200 1.0000
18.250 1.5058 0.07299 0.06838 -0.0084 0.0198 1.0000
18.500 1.4989 0.07728 0.07278 -0.0096 0.0196 1.0000
18.750 1.4897 0.08192 0.07751 -0.0110 0.0193 1.0000
19.000 1.4802 0.08669 0.08238 -0.0125 0.0191 1.0000
19.250 1.4697 0.09170 0.08748 -0.0143 0.0189 1.0000
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