FX LIII-142 K 25 AIRFOIL (fxl142k-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: FX LIII-142 K 25 AIRFOIL (fxl142k-il) Reynolds number: 500,000 Max Cl/Cd: 63.08 at α=7.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fxl142k-il-500000.txt Download as CSV file: xf-fxl142k-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: FX LIII-142 K 25 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.750 -1.0826 0.12303 0.11952 0.0109 1.0000 0.0086
-18.500 -1.1036 0.11499 0.11135 0.0067 1.0000 0.0087
-18.250 -1.1225 0.10753 0.10376 0.0029 1.0000 0.0087
-18.000 -1.1432 0.09997 0.09607 -0.0008 1.0000 0.0087
-17.750 -1.1633 0.09265 0.08861 -0.0044 1.0000 0.0089
-17.500 -1.1757 0.08683 0.08267 -0.0072 1.0000 0.0087
-17.250 -1.1923 0.08050 0.07620 -0.0101 1.0000 0.0090
-17.000 -1.2025 0.07530 0.07088 -0.0125 1.0000 0.0088
-16.750 -1.2153 0.06990 0.06535 -0.0148 1.0000 0.0094
-16.500 -1.2250 0.06509 0.06041 -0.0169 1.0000 0.0096
-16.250 -1.2314 0.06091 0.05611 -0.0185 1.0000 0.0098
-16.000 -1.2362 0.05714 0.05223 -0.0198 1.0000 0.0100
-15.750 -1.2477 0.05269 0.04767 -0.0212 1.0000 0.0105
-15.500 -1.2530 0.04915 0.04404 -0.0222 1.0000 0.0108
-15.250 -1.2587 0.04564 0.04046 -0.0231 1.0000 0.0119
-15.000 -1.2609 0.04261 0.03734 -0.0236 1.0000 0.0131
-14.750 -1.2659 0.03931 0.03401 -0.0242 1.0000 0.0156
-14.500 -1.2644 0.03677 0.03144 -0.0245 1.0000 0.0191
-14.250 -1.2547 0.03510 0.02978 -0.0247 1.0000 0.0230
-14.000 -1.2385 0.03406 0.02880 -0.0250 1.0000 0.0269
-13.750 -1.2171 0.03354 0.02820 -0.0252 1.0000 0.0294
-13.500 -1.2041 0.03224 0.02681 -0.0252 1.0000 0.0303
-13.250 -1.1985 0.03026 0.02483 -0.0253 1.0000 0.0324
-13.000 -1.1851 0.02907 0.02360 -0.0254 1.0000 0.0339
-12.750 -1.1730 0.02780 0.02226 -0.0252 1.0000 0.0350
-12.500 -1.1597 0.02672 0.02112 -0.0250 1.0000 0.0363
-12.250 -1.1444 0.02587 0.02020 -0.0246 1.0000 0.0376
-12.000 -1.1289 0.02510 0.01934 -0.0241 1.0000 0.0385
-11.750 -1.1165 0.02415 0.01831 -0.0232 1.0000 0.0393
-11.500 -1.1149 0.02258 0.01667 -0.0211 1.0000 0.0409
-11.250 -1.1082 0.02157 0.01564 -0.0189 1.0000 0.0425
-11.000 -1.0965 0.02092 0.01498 -0.0170 1.0000 0.0443
-10.750 -1.0821 0.02036 0.01439 -0.0153 1.0000 0.0458
-10.500 -1.0639 0.01990 0.01388 -0.0142 1.0000 0.0476
-10.250 -1.0463 0.01934 0.01326 -0.0129 1.0000 0.0486
-10.000 -1.0292 0.01872 0.01258 -0.0116 1.0000 0.0503
-9.750 -1.0150 0.01785 0.01171 -0.0099 1.0000 0.0530
-9.500 -0.9954 0.01734 0.01119 -0.0089 1.0000 0.0552
-9.250 -0.9748 0.01689 0.01071 -0.0079 1.0000 0.0571
-9.000 -0.9542 0.01642 0.01019 -0.0069 1.0000 0.0586
-8.750 -0.9331 0.01596 0.00968 -0.0059 1.0000 0.0598
-8.500 -0.9112 0.01556 0.00923 -0.0050 1.0000 0.0607
-8.250 -0.8941 0.01476 0.00839 -0.0035 1.0000 0.0637
-8.000 -0.8740 0.01418 0.00783 -0.0023 1.0000 0.0669
-7.750 -0.8525 0.01373 0.00736 -0.0014 1.0000 0.0704
-7.500 -0.8299 0.01337 0.00696 -0.0005 1.0000 0.0737
-7.250 -0.7986 0.01266 0.00637 -0.0018 0.9749 0.0845
-7.000 -0.7400 0.01195 0.00575 -0.0089 0.9283 0.1132
-6.750 -0.7083 0.01165 0.00535 -0.0099 0.8639 0.1312
-6.500 -0.6857 0.01146 0.00503 -0.0089 0.8277 0.1462
-6.250 -0.6630 0.01117 0.00472 -0.0080 0.8012 0.1616
-6.000 -0.6411 0.01080 0.00434 -0.0069 0.7653 0.1827
-5.750 -0.6196 0.01041 0.00399 -0.0059 0.7486 0.2191
-5.500 -0.5971 0.01003 0.00368 -0.0051 0.7352 0.2594
-5.250 -0.5744 0.00963 0.00343 -0.0043 0.7241 0.3071
-5.000 -0.5502 0.00931 0.00323 -0.0037 0.7134 0.3476
-4.750 -0.5246 0.00910 0.00307 -0.0033 0.7038 0.3786
-4.500 -0.4990 0.00893 0.00293 -0.0029 0.6953 0.4028
-4.250 -0.4725 0.00877 0.00282 -0.0025 0.6863 0.4259
-4.000 -0.4461 0.00867 0.00274 -0.0022 0.6791 0.4466
-3.750 -0.4187 0.00861 0.00270 -0.0020 0.6716 0.4641
-3.500 -0.3911 0.00860 0.00264 -0.0018 0.6651 0.4777
-3.250 -0.3633 0.00859 0.00259 -0.0016 0.6585 0.4902
-3.000 -0.3357 0.00860 0.00253 -0.0014 0.6525 0.5026
-2.750 -0.3083 0.00858 0.00251 -0.0012 0.6472 0.5132
-2.500 -0.2806 0.00857 0.00249 -0.0011 0.6419 0.5219
-2.250 -0.2526 0.00863 0.00248 -0.0009 0.6372 0.5304
-2.000 -0.2247 0.00865 0.00251 -0.0008 0.6325 0.5377
-1.750 -0.1966 0.00870 0.00253 -0.0007 0.6274 0.5471
-1.500 -0.1688 0.00875 0.00256 -0.0006 0.6227 0.5557
-1.250 -0.1407 0.00879 0.00257 -0.0005 0.6181 0.5630
-1.000 -0.1126 0.00876 0.00257 -0.0004 0.6129 0.5692
-0.750 -0.0844 0.00880 0.00256 -0.0003 0.6082 0.5757
-0.500 -0.0563 0.00876 0.00256 -0.0002 0.6035 0.5809
-0.250 -0.0281 0.00874 0.00255 -0.0001 0.5975 0.5860
0.000 0.0000 0.00876 0.00252 0.0000 0.5920 0.5919
0.250 0.0281 0.00874 0.00255 0.0001 0.5861 0.5976
0.500 0.0563 0.00876 0.00256 0.0002 0.5809 0.6034
0.750 0.0844 0.00880 0.00255 0.0003 0.5757 0.6082
1.000 0.1126 0.00876 0.00257 0.0004 0.5692 0.6129
1.250 0.1407 0.00879 0.00257 0.0005 0.5629 0.6181
1.500 0.1688 0.00875 0.00256 0.0006 0.5557 0.6228
1.750 0.1966 0.00870 0.00253 0.0007 0.5471 0.6275
2.000 0.2247 0.00865 0.00251 0.0008 0.5376 0.6325
2.250 0.2527 0.00862 0.00248 0.0009 0.5301 0.6372
2.500 0.2806 0.00857 0.00249 0.0011 0.5218 0.6419
2.750 0.3083 0.00858 0.00251 0.0012 0.5131 0.6472
3.000 0.3357 0.00860 0.00253 0.0014 0.5026 0.6525
3.250 0.3633 0.00859 0.00259 0.0016 0.4901 0.6584
3.500 0.3911 0.00860 0.00264 0.0018 0.4773 0.6650
3.750 0.4187 0.00861 0.00270 0.0020 0.4637 0.6715
4.000 0.4461 0.00867 0.00274 0.0022 0.4462 0.6791
4.500 0.4990 0.00893 0.00293 0.0029 0.4027 0.6953
4.750 0.5246 0.00910 0.00307 0.0033 0.3782 0.7038
5.000 0.5502 0.00931 0.00323 0.0037 0.3482 0.7134
5.250 0.5745 0.00962 0.00342 0.0043 0.3075 0.7240
5.500 0.5972 0.01003 0.00368 0.0051 0.2596 0.7353
5.750 0.6196 0.01042 0.00399 0.0059 0.2188 0.7486
6.000 0.6411 0.01081 0.00434 0.0069 0.1824 0.7653
6.250 0.6630 0.01118 0.00472 0.0080 0.1614 0.8012
6.500 0.6857 0.01146 0.00504 0.0089 0.1460 0.8277
6.750 0.7084 0.01165 0.00535 0.0099 0.1313 0.8639
7.000 0.7401 0.01195 0.00575 0.0089 0.1132 0.9283
7.250 0.7986 0.01266 0.00636 0.0018 0.0848 0.9749
7.500 0.8300 0.01336 0.00695 0.0005 0.0736 1.0000
7.750 0.8525 0.01373 0.00736 0.0014 0.0702 1.0000
8.000 0.8740 0.01418 0.00782 0.0023 0.0669 1.0000
8.250 0.8942 0.01475 0.00838 0.0035 0.0637 1.0000
8.500 0.9112 0.01556 0.00923 0.0050 0.0607 1.0000
8.750 0.9332 0.01595 0.00967 0.0059 0.0598 1.0000
9.000 0.9543 0.01641 0.01018 0.0069 0.0586 1.0000
9.250 0.9748 0.01690 0.01072 0.0079 0.0571 1.0000
9.500 0.9949 0.01739 0.01125 0.0089 0.0554 1.0000
9.750 1.0145 0.01790 0.01178 0.0100 0.0535 1.0000
10.000 1.0296 0.01869 0.01256 0.0115 0.0504 1.0000
10.250 1.0445 0.01948 0.01340 0.0131 0.0488 1.0000
10.500 1.0647 0.01985 0.01383 0.0141 0.0474 1.0000
10.750 1.0814 0.02042 0.01445 0.0154 0.0460 1.0000
11.000 1.0976 0.02087 0.01493 0.0168 0.0440 1.0000
11.250 1.1081 0.02159 0.01567 0.0189 0.0427 1.0000
11.500 1.1153 0.02258 0.01668 0.0211 0.0411 1.0000
11.750 1.1152 0.02428 0.01844 0.0233 0.0390 1.0000
12.000 1.1285 0.02517 0.01942 0.0241 0.0385 1.0000
12.250 1.1450 0.02587 0.02019 0.0245 0.0376 1.0000
12.500 1.1583 0.02688 0.02129 0.0250 0.0366 1.0000
12.750 1.1725 0.02789 0.02237 0.0252 0.0352 1.0000
13.000 1.1867 0.02898 0.02350 0.0252 0.0336 1.0000
13.250 1.1985 0.03033 0.02489 0.0252 0.0324 1.0000
13.500 1.2046 0.03225 0.02683 0.0252 0.0306 1.0000
13.750 1.2209 0.03325 0.02791 0.0250 0.0291 1.0000
14.000 1.2421 0.03380 0.02853 0.0248 0.0263 1.0000
14.250 1.2544 0.03522 0.02993 0.0245 0.0241 1.0000
14.500 1.2657 0.03674 0.03144 0.0243 0.0197 1.0000
14.750 1.2688 0.03912 0.03383 0.0240 0.0168 1.0000
15.000 1.2644 0.04236 0.03709 0.0235 0.0137 1.0000
15.250 1.2627 0.04535 0.04017 0.0229 0.0123 1.0000
15.500 1.2575 0.04879 0.04368 0.0221 0.0110 1.0000
15.750 1.2495 0.05267 0.04765 0.0210 0.0105 1.0000
16.000 1.2392 0.05696 0.05205 0.0196 0.0099 1.0000
16.250 1.2353 0.06062 0.05582 0.0183 0.0097 1.0000
16.500 1.2263 0.06516 0.06049 0.0165 0.0094 1.0000
16.750 1.2162 0.07005 0.06551 0.0144 0.0093 1.0000
17.000 1.2073 0.07488 0.07045 0.0123 0.0091 1.0000
17.250 1.1936 0.08063 0.07634 0.0097 0.0090 1.0000
17.500 1.1809 0.08635 0.08218 0.0070 0.0090 1.0000
17.750 1.1637 0.09296 0.08893 0.0039 0.0088 1.0000
18.000 1.1473 0.09964 0.09573 0.0006 0.0088 1.0000
18.250 1.1273 0.10708 0.10331 -0.0031 0.0087 1.0000
18.500 1.1068 0.11482 0.11118 -0.0070 0.0087 1.0000
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