NACA 2424 (naca2424-il) Xfoil prediction polar at RE=100,000 Ncrit=9
| Details | Polar file |
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Airfoil: NACA 2424 (naca2424-il) Reynolds number: 100,000 Max Cl/Cd: 36.82 at α=6.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-naca2424-il-100000.txt Download as CSV file: xf-naca2424-il-100000.csv |
XFOIL Version 6.96
Calculated polar for: NACA 2424
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.100 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-13.750 -0.7964 0.07244 0.06551 -0.0680 1.0000 0.1908
-13.500 -0.8535 0.06598 0.05894 -0.0663 1.0000 0.1923
-13.250 -0.8988 0.06163 0.05450 -0.0632 1.0000 0.1937
-13.000 -0.9552 0.05746 0.05017 -0.0584 1.0000 0.1948
-12.750 -0.9889 0.05514 0.04775 -0.0535 1.0000 0.1965
-12.500 -1.0261 0.05302 0.04551 -0.0477 1.0000 0.1980
-12.250 -1.0666 0.05114 0.04348 -0.0407 1.0000 0.1995
-12.000 -1.1075 0.04959 0.04177 -0.0327 1.0000 0.2007
-11.750 -1.1488 0.04839 0.04039 -0.0238 1.0000 0.2018
-11.500 -1.1879 0.04725 0.03904 -0.0148 1.0000 0.2033
-11.250 -1.2216 0.04595 0.03746 -0.0065 1.0000 0.2048
-11.000 -1.1894 0.04561 0.03742 -0.0075 1.0000 0.2087
-10.750 -1.1895 0.04512 0.03695 -0.0038 1.0000 0.2118
-10.500 -1.1694 0.04436 0.03597 -0.0044 0.9920 0.2172
-10.250 -1.1485 0.04332 0.03478 -0.0047 0.9830 0.2224
-10.000 -1.1049 0.04327 0.03489 -0.0081 0.9761 0.2282
-9.750 -1.0916 0.04244 0.03384 -0.0069 0.9666 0.2337
-9.500 -1.0710 0.04157 0.03290 -0.0066 0.9577 0.2390
-9.250 -1.0316 0.04145 0.03291 -0.0092 0.9508 0.2454
-9.000 -1.0243 0.04068 0.03194 -0.0065 0.9404 0.2509
-8.750 -0.9870 0.04008 0.03137 -0.0088 0.9339 0.2576
-8.500 -0.9682 0.03976 0.03110 -0.0076 0.9239 0.2631
-8.250 -0.9494 0.03910 0.03016 -0.0067 0.9161 0.2706
-8.000 -0.9253 0.03863 0.02984 -0.0065 0.9067 0.2762
-7.750 -0.8946 0.03832 0.02955 -0.0072 0.8987 0.2836
-7.500 -0.8846 0.03774 0.02867 -0.0045 0.8898 0.2905
-7.250 -0.8534 0.03740 0.02859 -0.0053 0.8808 0.2971
-7.000 -0.8190 0.03693 0.02803 -0.0066 0.8747 0.3063
-6.750 -0.8152 0.03652 0.02752 -0.0027 0.8632 0.3120
-6.500 -0.7790 0.03624 0.02741 -0.0042 0.8560 0.3203
-6.250 -0.7486 0.03564 0.02654 -0.0045 0.8510 0.3305
-6.000 -0.7406 0.03551 0.02661 -0.0014 0.8382 0.3360
-5.750 -0.7069 0.03511 0.02622 -0.0022 0.8318 0.3460
-5.500 -0.6630 0.03442 0.02552 -0.0048 0.8281 0.3568
-5.250 -0.6680 0.03458 0.02573 0.0006 0.8138 0.3623
-4.750 -0.5840 0.03332 0.02451 -0.0035 0.8055 0.3856
-4.500 -0.6017 0.03370 0.02482 0.0040 0.7899 0.3914
-4.250 -0.5589 0.03302 0.02421 0.0019 0.7857 0.4031
-4.000 -0.5548 0.03320 0.02439 0.0058 0.7745 0.4118
-3.750 -0.5314 0.03282 0.02400 0.0068 0.7669 0.4226
-3.500 -0.4884 0.03217 0.02340 0.0049 0.7633 0.4365
-3.250 -0.4941 0.03257 0.02377 0.0103 0.7505 0.4442
-3.000 -0.4616 0.03220 0.02351 0.0100 0.7443 0.4568
-2.750 -0.4175 0.03138 0.02274 0.0081 0.7412 0.4717
-2.500 -0.3937 0.03113 0.02247 0.0092 0.7350 0.4854
-1.750 -0.3535 0.03146 0.02300 0.0169 0.7079 0.5210
-1.500 -0.3407 0.03144 0.02293 0.0198 0.6995 0.5358
-1.250 -0.2908 0.03051 0.02216 0.0173 0.6969 0.5539
-1.000 -0.2377 0.02945 0.02119 0.0143 0.6948 0.5736
-0.750 -0.2794 0.03132 0.02305 0.0246 0.6776 0.5817
-0.500 -0.2310 0.03035 0.02220 0.0225 0.6749 0.6024
-0.250 -0.1782 0.02934 0.02129 0.0197 0.6727 0.6242
0.000 -0.1672 0.02961 0.02161 0.0227 0.6646 0.6414
0.250 -0.0350 0.02704 0.01914 0.0073 0.6693 0.6740
0.500 -0.1205 0.02944 0.02161 0.0254 0.6506 0.6820
0.750 -0.0502 0.02822 0.02046 0.0198 0.6488 0.7080
1.000 0.0412 0.02701 0.01929 0.0102 0.6470 0.7351
1.500 0.0521 0.02830 0.02080 0.0180 0.6276 0.7722
1.750 0.1897 0.02719 0.01964 0.0003 0.6252 0.7947
2.000 0.0951 0.02937 0.02201 0.0202 0.6105 0.8149
2.250 0.2582 0.02835 0.02091 -0.0016 0.6071 0.8287
2.500 0.4055 0.02784 0.02016 -0.0218 0.6016 0.8390
2.750 0.4419 0.02911 0.02156 -0.0235 0.5901 0.8472
3.000 0.5513 0.02916 0.02143 -0.0373 0.5813 0.8521
3.250 0.5801 0.02967 0.02193 -0.0372 0.5730 0.8655
3.500 0.6374 0.03030 0.02256 -0.0422 0.5625 0.8719
3.750 0.7218 0.03029 0.02233 -0.0518 0.5543 0.8789
4.000 0.7228 0.03112 0.02332 -0.0472 0.5445 0.8930
4.250 0.7989 0.03099 0.02300 -0.0555 0.5355 0.9006
4.750 0.8436 0.03188 0.02396 -0.0541 0.5179 0.9278
5.000 0.9185 0.03183 0.02375 -0.0626 0.5085 0.9330
5.250 0.9311 0.03239 0.02443 -0.0605 0.4990 0.9475
5.500 1.0118 0.03196 0.02374 -0.0700 0.4899 0.9530
5.750 1.0217 0.03260 0.02457 -0.0678 0.4802 0.9672
6.000 1.0730 0.03242 0.02427 -0.0723 0.4712 0.9773
6.250 1.1134 0.03258 0.02448 -0.0756 0.4616 0.9876
6.500 1.1616 0.03232 0.02417 -0.0800 0.4516 0.9972
6.750 1.1907 0.03234 0.02408 -0.0810 0.4442 1.0000
7.000 1.1622 0.03296 0.02485 -0.0722 0.4381 1.0000
7.250 1.1630 0.03307 0.02492 -0.0681 0.4317 1.0000
7.500 1.1952 0.03299 0.02464 -0.0691 0.4249 1.0000
7.750 1.1505 0.03378 0.02561 -0.0576 0.4199 1.0000
8.000 1.1216 0.03418 0.02606 -0.0484 0.4147 1.0000
8.250 1.1827 0.03383 0.02545 -0.0540 0.4067 1.0000
8.500 1.1392 0.03449 0.02621 -0.0425 0.4026 1.0000
8.750 1.0895 0.03534 0.02719 -0.0303 0.3980 1.0000
9.000 1.0832 0.03571 0.02753 -0.0250 0.3921 1.0000
9.250 1.1395 0.03534 0.02694 -0.0292 0.3846 1.0000
9.500 1.0800 0.03679 0.02857 -0.0162 0.3804 1.0000
9.750 1.0573 0.03784 0.02967 -0.0092 0.3745 1.0000
10.000 1.1464 0.03652 0.02800 -0.0174 0.3663 1.0000
10.250 1.0795 0.03865 0.03037 -0.0044 0.3621 1.0000
10.500 1.0449 0.04053 0.03236 0.0033 0.3562 1.0000
10.750 1.1247 0.03876 0.03028 -0.0025 0.3488 1.0000
11.000 1.0817 0.04105 0.03274 0.0060 0.3438 1.0000
11.250 1.0293 0.04427 0.03614 0.0142 0.3381 1.0000
11.500 1.0988 0.04220 0.03383 0.0107 0.3314 1.0000
11.750 1.0843 0.04404 0.03573 0.0150 0.3260 1.0000
12.000 0.8048 0.06653 0.05887 0.0300 0.3139 1.0000
12.250 1.0608 0.04753 0.03932 0.0222 0.3142 1.0000
12.500 1.0832 0.04783 0.03955 0.0229 0.3085 1.0000
12.750 0.7801 0.07637 0.06874 0.0328 0.2938 1.0000
13.000 0.9409 0.06119 0.05333 0.0332 0.2960 1.0000
13.250 1.0766 0.05265 0.04443 0.0297 0.2918 1.0000
14.000 1.0707 0.05818 0.05002 0.0350 0.2757 1.0000
14.250 0.4799 0.14015 0.13285 0.0200 0.2400 1.0000
14.500 0.4638 0.14613 0.13887 0.0183 0.2387 1.0000
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