NACA 24112 (naca24112-jf) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 24112 (naca24112-jf) Reynolds number: 500,000 Max Cl/Cd: 83.02 at α=8° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-naca24112-jf-500000-n5.txt Download as CSV file: xf-naca24112-jf-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NACA 24112
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-14.500 -1.0685 0.05345 0.05024 -0.0341 1.0000 0.0138
-14.250 -1.0952 0.04715 0.04369 -0.0365 1.0000 0.0138
-14.000 -1.1094 0.04328 0.03962 -0.0364 1.0000 0.0139
-13.750 -1.1169 0.04049 0.03666 -0.0351 1.0000 0.0140
-13.500 -1.1200 0.03828 0.03430 -0.0332 1.0000 0.0141
-13.250 -1.1198 0.03645 0.03233 -0.0310 1.0000 0.0142
-13.000 -1.1172 0.03486 0.03061 -0.0285 1.0000 0.0143
-12.750 -1.1107 0.03336 0.02897 -0.0263 1.0000 0.0145
-12.500 -1.1007 0.03190 0.02737 -0.0246 1.0000 0.0147
-12.250 -1.0889 0.03048 0.02580 -0.0229 1.0000 0.0149
-12.000 -1.0756 0.02910 0.02426 -0.0214 1.0000 0.0151
-11.750 -1.0610 0.02777 0.02276 -0.0199 1.0000 0.0154
-11.500 -1.0451 0.02650 0.02131 -0.0185 1.0000 0.0157
-11.250 -1.0279 0.02531 0.01995 -0.0172 1.0000 0.0160
-11.000 -1.0093 0.02424 0.01870 -0.0160 1.0000 0.0163
-10.750 -0.9901 0.02323 0.01755 -0.0148 1.0000 0.0166
-10.500 -0.9703 0.02238 0.01664 -0.0137 1.0000 0.0169
-10.250 -0.9489 0.02171 0.01591 -0.0128 1.0000 0.0173
-10.000 -0.9271 0.02106 0.01521 -0.0119 1.0000 0.0176
-9.750 -0.9052 0.02039 0.01446 -0.0109 1.0000 0.0180
-9.500 -0.8831 0.01972 0.01370 -0.0100 1.0000 0.0184
-9.250 -0.8609 0.01905 0.01294 -0.0091 1.0000 0.0188
-9.000 -0.8386 0.01840 0.01219 -0.0081 1.0000 0.0193
-8.750 -0.8162 0.01779 0.01148 -0.0071 1.0000 0.0197
-8.500 -0.7944 0.01715 0.01079 -0.0060 1.0000 0.0201
-8.250 -0.7722 0.01665 0.01029 -0.0049 1.0000 0.0206
-8.000 -0.7499 0.01625 0.00987 -0.0039 1.0000 0.0212
-7.750 -0.7280 0.01586 0.00945 -0.0027 1.0000 0.0218
-7.500 -0.6943 0.01535 0.00888 -0.0040 0.9939 0.0227
-7.250 -0.6595 0.01484 0.00829 -0.0055 0.9833 0.0234
-7.000 -0.6271 0.01429 0.00772 -0.0066 0.9706 0.0242
-6.750 -0.5952 0.01387 0.00729 -0.0074 0.9555 0.0250
-6.500 -0.5652 0.01352 0.00690 -0.0078 0.9359 0.0260
-6.250 -0.5380 0.01321 0.00651 -0.0075 0.9116 0.0271
-6.000 -0.5132 0.01291 0.00611 -0.0066 0.8844 0.0281
-5.500 -0.4645 0.01243 0.00545 -0.0047 0.8276 0.0304
-5.250 -0.4395 0.01224 0.00513 -0.0039 0.7990 0.0317
-5.000 -0.4143 0.01206 0.00482 -0.0032 0.7712 0.0330
-4.750 -0.3888 0.01186 0.00454 -0.0025 0.7445 0.0347
-4.500 -0.3629 0.01173 0.00430 -0.0020 0.7176 0.0366
-4.250 -0.3367 0.01161 0.00404 -0.0015 0.6912 0.0383
-4.000 -0.3107 0.01143 0.00380 -0.0010 0.6675 0.0405
-3.750 -0.2842 0.01132 0.00360 -0.0006 0.6431 0.0432
-3.500 -0.2577 0.01122 0.00339 -0.0002 0.6192 0.0458
-3.250 -0.2311 0.01110 0.00321 0.0001 0.5964 0.0489
-3.000 -0.2042 0.01102 0.00304 0.0004 0.5752 0.0523
-2.750 -0.1775 0.01092 0.00289 0.0007 0.5537 0.0568
-2.500 -0.1504 0.01086 0.00275 0.0010 0.5329 0.0613
-2.250 -0.1234 0.01077 0.00262 0.0012 0.5139 0.0673
-2.000 -0.0962 0.01072 0.00250 0.0015 0.4962 0.0738
-1.750 -0.0691 0.01065 0.00240 0.0017 0.4783 0.0825
-1.500 -0.0420 0.01058 0.00231 0.0019 0.4618 0.0934
-1.250 -0.0148 0.01051 0.00223 0.0021 0.4475 0.1076
-1.000 0.0123 0.01043 0.00216 0.0023 0.4340 0.1283
-0.750 0.0389 0.01029 0.00208 0.0025 0.4207 0.1662
-0.500 0.0565 0.00898 0.00185 0.0039 0.4103 0.4883
-0.250 0.0780 0.00845 0.00180 0.0051 0.4007 0.6310
0.000 0.1007 0.00812 0.00181 0.0064 0.3912 0.7304
0.250 0.1252 0.00798 0.00186 0.0074 0.3821 0.7953
0.500 0.1509 0.00795 0.00193 0.0082 0.3730 0.8415
0.750 0.1777 0.00799 0.00202 0.0088 0.3658 0.8739
1.000 0.2054 0.00807 0.00211 0.0091 0.3579 0.8983
1.250 0.2338 0.00819 0.00221 0.0093 0.3508 0.9177
1.500 0.2631 0.00833 0.00233 0.0093 0.3437 0.9355
1.750 0.2938 0.00850 0.00245 0.0090 0.3373 0.9477
2.000 0.3224 0.00859 0.00251 0.0090 0.3312 0.9548
2.250 0.3539 0.00872 0.00258 0.0082 0.3243 0.9586
2.500 0.3862 0.00884 0.00267 0.0074 0.3189 0.9621
2.750 0.4170 0.00895 0.00275 0.0068 0.3129 0.9665
3.000 0.4466 0.00909 0.00284 0.0064 0.3067 0.9709
3.250 0.4806 0.00921 0.00294 0.0051 0.3015 0.9730
3.500 0.5146 0.00933 0.00303 0.0038 0.2954 0.9752
3.750 0.5475 0.00949 0.00314 0.0026 0.2894 0.9777
4.000 0.5791 0.00959 0.00325 0.0018 0.2842 0.9808
4.250 0.6106 0.00973 0.00336 0.0010 0.2782 0.9835
4.500 0.6445 0.00988 0.00348 -0.0004 0.2725 0.9850
4.750 0.6780 0.01000 0.00361 -0.0017 0.2668 0.9868
5.000 0.7105 0.01016 0.00374 -0.0028 0.2605 0.9889
5.250 0.7424 0.01031 0.00389 -0.0038 0.2552 0.9912
5.500 0.7736 0.01046 0.00404 -0.0047 0.2490 0.9934
5.750 0.8060 0.01065 0.00420 -0.0058 0.2428 0.9949
6.000 0.8387 0.01079 0.00437 -0.0070 0.2365 0.9964
6.250 0.8707 0.01099 0.00455 -0.0081 0.2296 0.9981
6.500 0.9026 0.01116 0.00473 -0.0092 0.2230 0.9996
6.750 0.9280 0.01137 0.00493 -0.0089 0.2159 1.0000
7.000 0.9510 0.01156 0.00512 -0.0081 0.2093 1.0000
7.250 0.9735 0.01178 0.00533 -0.0072 0.2015 1.0000
7.500 0.9961 0.01200 0.00556 -0.0063 0.1941 1.0000
7.750 1.0180 0.01229 0.00581 -0.0053 0.1854 1.0000
8.000 1.0403 0.01253 0.00606 -0.0044 0.1771 1.0000
8.250 1.0619 0.01283 0.00635 -0.0034 0.1684 1.0000
8.500 1.0833 0.01317 0.00666 -0.0024 0.1586 1.0000
8.750 1.1048 0.01349 0.00698 -0.0015 0.1493 1.0000
9.000 1.1257 0.01387 0.00734 -0.0004 0.1396 1.0000
9.250 1.1460 0.01430 0.00774 0.0007 0.1293 1.0000
9.500 1.1659 0.01477 0.00817 0.0018 0.1185 1.0000
9.750 1.1858 0.01524 0.00862 0.0029 0.1082 1.0000
10.000 1.2052 0.01575 0.00912 0.0041 0.0980 1.0000
10.250 1.2241 0.01632 0.00966 0.0052 0.0882 1.0000
10.500 1.2426 0.01693 0.01024 0.0064 0.0790 1.0000
10.750 1.2607 0.01758 0.01087 0.0076 0.0706 1.0000
11.250 1.2956 0.01893 0.01222 0.0099 0.0564 1.0000
11.500 1.3122 0.01963 0.01294 0.0112 0.0511 1.0000
12.000 1.3427 0.02115 0.01451 0.0139 0.0426 1.0000
12.250 1.3545 0.02202 0.01541 0.0156 0.0391 1.0000
12.500 1.3649 0.02283 0.01627 0.0176 0.0365 1.0000
12.750 1.3727 0.02386 0.01733 0.0195 0.0340 1.0000
13.000 1.3810 0.02495 0.01850 0.0211 0.0321 1.0000
13.250 1.3883 0.02622 0.01985 0.0224 0.0303 1.0000
13.500 1.3932 0.02784 0.02152 0.0234 0.0287 1.0000
13.750 1.3980 0.02963 0.02341 0.0240 0.0274 1.0000
14.000 1.4021 0.03169 0.02557 0.0241 0.0262 1.0000
14.250 1.4037 0.03422 0.02819 0.0237 0.0250 1.0000
14.500 1.4024 0.03731 0.03138 0.0229 0.0241 1.0000
14.750 1.3992 0.04083 0.03501 0.0216 0.0234 1.0000
15.000 1.3957 0.04454 0.03884 0.0202 0.0228 1.0000
15.250 1.3890 0.04875 0.04319 0.0185 0.0222 1.0000
15.500 1.3792 0.05343 0.04799 0.0166 0.0218 1.0000
15.750 1.3665 0.05851 0.05319 0.0146 0.0214 1.0000
16.000 1.3518 0.06388 0.05868 0.0126 0.0210 1.0000
16.250 1.3355 0.06946 0.06438 0.0104 0.0208 1.0000
16.500 1.3187 0.07519 0.07022 0.0082 0.0205 1.0000
16.750 1.3017 0.08107 0.07620 0.0059 0.0202 1.0000
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