NACA 2424 (naca2424-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: NACA 2424 (naca2424-il) Reynolds number: 1,000,000 Max Cl/Cd: 65.9 at α=7.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-naca2424-il-1000000.txt Download as CSV file: xf-naca2424-il-1000000.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 = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.1479 0.07195 0.06756 -0.0772 1.0000 0.0728
-19.500 -1.1504 0.06925 0.06479 -0.0775 1.0000 0.0736
-19.250 -1.1664 0.06510 0.06058 -0.0781 1.0000 0.0748
-19.000 -1.1793 0.06137 0.05680 -0.0785 1.0000 0.0759
-18.750 -1.1887 0.05811 0.05349 -0.0786 1.0000 0.0768
-18.500 -1.1949 0.05531 0.05064 -0.0784 1.0000 0.0779
-18.250 -1.2004 0.05266 0.04793 -0.0781 1.0000 0.0789
-18.000 -1.2033 0.05034 0.04555 -0.0776 1.0000 0.0798
-17.750 -1.2095 0.04784 0.04299 -0.0769 1.0000 0.0805
-17.500 -1.2204 0.04508 0.04018 -0.0759 1.0000 0.0816
-17.250 -1.2136 0.04247 0.03755 -0.0776 0.9991 0.0833
-17.000 -1.2010 0.04021 0.03525 -0.0795 0.9978 0.0846
-16.750 -1.1850 0.03835 0.03333 -0.0814 0.9962 0.0862
-16.500 -1.1691 0.03656 0.03150 -0.0831 0.9947 0.0879
-16.250 -1.1561 0.03449 0.02941 -0.0849 0.9932 0.0899
-16.000 -1.1390 0.03279 0.02768 -0.0867 0.9921 0.0916
-15.750 -1.1205 0.03142 0.02628 -0.0880 0.9908 0.0934
-15.500 -1.1049 0.03007 0.02488 -0.0883 0.9880 0.0946
-15.250 -1.0917 0.02836 0.02316 -0.0892 0.9855 0.0969
-15.000 -1.0728 0.02704 0.02183 -0.0903 0.9836 0.0993
-14.750 -1.0509 0.02592 0.02068 -0.0916 0.9821 0.1011
-14.500 -1.0263 0.02496 0.01969 -0.0931 0.9808 0.1032
-14.250 -1.0050 0.02374 0.01848 -0.0945 0.9797 0.1060
-14.000 -0.9798 0.02278 0.01752 -0.0960 0.9788 0.1088
-13.750 -0.9658 0.02189 0.01659 -0.0949 0.9738 0.1107
-13.500 -0.9467 0.02091 0.01560 -0.0951 0.9702 0.1132
-13.250 -0.9237 0.02000 0.01471 -0.0959 0.9679 0.1162
-13.000 -0.8966 0.01929 0.01398 -0.0971 0.9662 0.1193
-12.750 -0.8698 0.01849 0.01318 -0.0983 0.9648 0.1225
-12.500 -0.8590 0.01777 0.01246 -0.0963 0.9575 0.1249
-12.250 -0.8362 0.01710 0.01180 -0.0964 0.9538 0.1285
-12.000 -0.8110 0.01647 0.01116 -0.0968 0.9512 0.1321
-11.750 -0.7836 0.01578 0.01049 -0.0978 0.9491 0.1359
-11.500 -0.7682 0.01530 0.00999 -0.0961 0.9403 0.1392
-11.250 -0.7369 0.01474 0.00944 -0.0976 0.9367 0.1434
-11.000 -0.7022 0.01418 0.00890 -0.0998 0.9334 0.1484
-10.750 -0.6718 0.01382 0.00851 -0.1008 0.9264 0.1517
-10.500 -0.6392 0.01331 0.00802 -0.1026 0.9196 0.1568
-10.250 -0.6014 0.01295 0.00763 -0.1051 0.9130 0.1618
-10.000 -0.5744 0.01264 0.00731 -0.1055 0.9031 0.1661
-9.750 -0.5400 0.01230 0.00695 -0.1074 0.8948 0.1715
-9.500 -0.5180 0.01208 0.00670 -0.1066 0.8846 0.1755
-9.250 -0.4875 0.01181 0.00640 -0.1076 0.8745 0.1806
-9.000 -0.4668 0.01157 0.00616 -0.1065 0.8640 0.1853
-8.750 -0.4384 0.01140 0.00594 -0.1069 0.8536 0.1897
-8.500 -0.4168 0.01117 0.00570 -0.1060 0.8427 0.1947
-8.250 -0.3917 0.01098 0.00549 -0.1058 0.8312 0.2004
-8.000 -0.3678 0.01085 0.00532 -0.1051 0.8205 0.2047
-7.750 -0.3464 0.01065 0.00510 -0.1041 0.8085 0.2108
-7.500 -0.3273 0.01050 0.00493 -0.1025 0.7963 0.2163
-7.000 -0.2914 0.01024 0.00461 -0.0987 0.7716 0.2269
-6.750 -0.2752 0.01015 0.00447 -0.0963 0.7586 0.2321
-6.500 -0.2578 0.01008 0.00436 -0.0942 0.7465 0.2364
-6.250 -0.2439 0.00996 0.00422 -0.0914 0.7350 0.2433
-6.000 -0.2285 0.00987 0.00411 -0.0889 0.7234 0.2494
-5.750 -0.2130 0.00984 0.00402 -0.0863 0.7121 0.2538
-5.500 -0.2007 0.00971 0.00391 -0.0831 0.7007 0.2610
-5.250 -0.1879 0.00966 0.00382 -0.0799 0.6896 0.2668
-5.000 -0.1733 0.00962 0.00375 -0.0771 0.6788 0.2718
-4.750 -0.1664 0.00955 0.00366 -0.0727 0.6679 0.2791
-4.500 -0.1556 0.00948 0.00360 -0.0691 0.6582 0.2858
-4.250 -0.1470 0.00950 0.00355 -0.0649 0.6469 0.2902
-4.000 -0.1365 0.00940 0.00348 -0.0612 0.6378 0.2978
-3.750 -0.1278 0.00938 0.00343 -0.0571 0.6275 0.3044
-3.500 -0.1158 0.00938 0.00339 -0.0536 0.6183 0.3098
-3.250 -0.1071 0.00932 0.00335 -0.0495 0.6093 0.3171
-3.000 -0.1014 0.00932 0.00332 -0.0448 0.5998 0.3238
-2.750 -0.0888 0.00930 0.00329 -0.0414 0.5917 0.3300
-2.500 -0.0799 0.00927 0.00326 -0.0373 0.5829 0.3381
-2.250 -0.0670 0.00925 0.00324 -0.0341 0.5749 0.3459
-2.000 -0.0515 0.00924 0.00322 -0.0313 0.5672 0.3524
-1.750 -0.0417 0.00922 0.00320 -0.0275 0.5587 0.3622
-1.500 -0.0258 0.00921 0.00319 -0.0249 0.5515 0.3704
-1.250 -0.0094 0.00918 0.00318 -0.0223 0.5444 0.3791
-1.000 0.0042 0.00918 0.00317 -0.0193 0.5367 0.3889
-0.750 0.0217 0.00918 0.00318 -0.0170 0.5300 0.3981
-0.500 0.0383 0.00914 0.00317 -0.0146 0.5233 0.4095
-0.250 0.0537 0.00918 0.00319 -0.0119 0.5160 0.4183
0.000 0.0683 0.00916 0.00321 -0.0090 0.5093 0.4312
0.250 0.0875 0.00915 0.00323 -0.0072 0.5034 0.4430
0.500 0.1038 0.00914 0.00325 -0.0047 0.4968 0.4560
0.750 0.1193 0.00920 0.00329 -0.0021 0.4892 0.4671
1.000 0.1387 0.00915 0.00331 -0.0002 0.4841 0.4836
1.250 0.1559 0.00915 0.00335 0.0020 0.4778 0.4975
1.500 0.1719 0.00921 0.00341 0.0045 0.4710 0.5120
1.750 0.1894 0.00921 0.00347 0.0067 0.4651 0.5287
2.000 0.2091 0.00921 0.00352 0.0084 0.4595 0.5436
2.250 0.2272 0.00927 0.00359 0.0104 0.4530 0.5597
2.500 0.2427 0.00933 0.00369 0.0129 0.4461 0.5764
2.750 0.2635 0.00934 0.00375 0.0144 0.4407 0.5912
3.000 0.2825 0.00939 0.00384 0.0162 0.4345 0.6082
3.250 0.2995 0.00948 0.00395 0.0184 0.4277 0.6238
3.500 0.3212 0.00953 0.00404 0.0196 0.4224 0.6393
3.750 0.3418 0.00958 0.00415 0.0210 0.4162 0.6572
4.000 0.3599 0.00968 0.00429 0.0228 0.4093 0.6756
4.250 0.3813 0.00977 0.00442 0.0240 0.4034 0.6926
4.500 0.4046 0.00984 0.00454 0.0248 0.3976 0.7119
4.750 0.4266 0.00994 0.00470 0.0258 0.3908 0.7335
5.000 0.4499 0.01005 0.00487 0.0265 0.3843 0.7558
5.250 0.4798 0.01011 0.00503 0.0259 0.3783 0.7803
5.500 0.5093 0.01026 0.00523 0.0252 0.3708 0.8056
5.750 0.5392 0.01039 0.00543 0.0245 0.3640 0.8307
6.000 0.5713 0.01050 0.00562 0.0233 0.3576 0.8555
6.250 0.6042 0.01072 0.00587 0.0218 0.3495 0.8802
6.500 0.6492 0.01089 0.00612 0.0180 0.3428 0.9026
6.750 0.7019 0.01123 0.00647 0.0124 0.3337 0.9195
7.000 0.7513 0.01163 0.00686 0.0076 0.3258 0.9304
7.250 0.7948 0.01206 0.00727 0.0039 0.3173 0.9378
7.500 0.8244 0.01256 0.00773 0.0031 0.3097 0.9485
7.750 0.8426 0.01296 0.00813 0.0047 0.3037 0.9621
8.000 0.8723 0.01348 0.00860 0.0036 0.2955 0.9669
8.250 0.8979 0.01393 0.00903 0.0036 0.2886 0.9739
8.500 0.9232 0.01443 0.00950 0.0034 0.2816 0.9786
8.750 0.9552 0.01495 0.00998 0.0018 0.2740 0.9808
9.000 0.9872 0.01542 0.01043 0.0002 0.2668 0.9836
9.250 1.0156 0.01604 0.01100 -0.0009 0.2590 0.9869
9.500 1.0438 0.01655 0.01150 -0.0017 0.2526 0.9901
9.750 1.0711 0.01721 0.01211 -0.0027 0.2450 0.9923
10.000 1.1033 0.01767 0.01256 -0.0045 0.2388 0.9943
10.250 1.1323 0.01824 0.01310 -0.0059 0.2321 0.9965
10.500 1.1612 0.01883 0.01366 -0.0073 0.2257 0.9984
10.750 1.1904 0.01945 0.01426 -0.0088 0.2195 0.9999
11.250 1.2045 0.02075 0.01555 -0.0035 0.2099 1.0000
11.500 1.2113 0.02147 0.01625 -0.0010 0.2051 1.0000
11.750 1.2161 0.02234 0.01711 0.0017 0.2002 1.0000
12.000 1.2252 0.02307 0.01785 0.0038 0.1964 1.0000
12.250 1.2338 0.02387 0.01865 0.0058 0.1920 1.0000
12.500 1.2377 0.02497 0.01973 0.0082 0.1870 1.0000
12.750 1.2470 0.02582 0.02060 0.0100 0.1835 1.0000
13.000 1.2545 0.02681 0.02160 0.0119 0.1794 1.0000
13.250 1.2601 0.02796 0.02274 0.0138 0.1753 1.0000
13.500 1.2658 0.02917 0.02395 0.0156 0.1715 1.0000
13.750 1.2752 0.03017 0.02498 0.0170 0.1681 1.0000
14.000 1.2798 0.03154 0.02635 0.0186 0.1642 1.0000
14.250 1.2833 0.03303 0.02784 0.0202 0.1599 1.0000
14.500 1.2915 0.03424 0.02908 0.0214 0.1569 1.0000
14.750 1.2959 0.03576 0.03060 0.0228 0.1527 1.0000
15.000 1.2966 0.03762 0.03245 0.0242 0.1485 1.0000
15.250 1.3042 0.03898 0.03386 0.0251 0.1457 1.0000
15.500 1.3073 0.04073 0.03561 0.0262 0.1413 1.0000
15.750 1.3060 0.04289 0.03777 0.0274 0.1375 1.0000
16.000 1.3127 0.04441 0.03932 0.0282 0.1342 1.0000
16.250 1.3140 0.04645 0.04138 0.0290 0.1311 1.0000
16.500 1.3126 0.04875 0.04369 0.0299 0.1278 1.0000
16.750 1.3160 0.05067 0.04564 0.0305 0.1248 1.0000
17.000 1.3184 0.05269 0.04769 0.0311 0.1225 1.0000
17.250 1.3158 0.05522 0.05024 0.0316 0.1195 1.0000
17.500 1.3144 0.05769 0.05275 0.0321 0.1167 1.0000
17.750 1.3171 0.05979 0.05488 0.0325 0.1145 1.0000
18.000 1.3146 0.06242 0.05754 0.0328 0.1117 1.0000
18.250 1.3106 0.06522 0.06036 0.0331 0.1093 1.0000
18.500 1.3098 0.06777 0.06296 0.0332 0.1075 1.0000
18.750 1.3111 0.07012 0.06535 0.0333 0.1053 1.0000
19.000 1.3073 0.07304 0.06831 0.0333 0.1032 1.0000
19.250 1.3028 0.07604 0.07133 0.0333 0.1011 1.0000
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