FX 66-H-60 (fx66h60-il) Xfoil prediction polar at RE=200,000 Ncrit=9
| Details | Polar file |
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Airfoil: FX 66-H-60 (fx66h60-il) Reynolds number: 200,000 Max Cl/Cd: 51.35 at α=5.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx66h60-il-200000.txt Download as CSV file: xf-fx66h60-il-200000.csv |
XFOIL Version 6.96
Calculated polar for: FX 66-H-60
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.200 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-8.250 -0.6093 0.10255 0.09933 0.0266 1.0000 0.0238
-8.000 -0.6090 0.09892 0.09574 0.0235 1.0000 0.0239
-7.750 -0.6096 0.09536 0.09220 0.0203 1.0000 0.0240
-7.500 -0.6050 0.09155 0.08836 0.0175 1.0000 0.0240
-7.250 -0.5980 0.08777 0.08454 0.0150 1.0000 0.0242
-7.000 -0.5897 0.08393 0.08064 0.0130 1.0000 0.0242
-6.750 -0.5799 0.08008 0.07671 0.0114 1.0000 0.0243
-6.500 -0.5689 0.07618 0.07265 0.0102 1.0000 0.0244
-6.250 -0.5640 0.06968 0.06610 0.0089 1.0000 0.0248
-6.000 -0.5593 0.06377 0.06021 0.0086 1.0000 0.0257
-5.750 -0.5486 0.05990 0.05632 0.0086 1.0000 0.0267
-5.500 -0.5347 0.05632 0.05266 0.0084 1.0000 0.0278
-5.250 -0.5184 0.05280 0.04902 0.0080 1.0000 0.0293
-5.000 -0.4999 0.04932 0.04539 0.0078 1.0000 0.0311
-4.750 -0.4788 0.04603 0.04188 0.0079 1.0000 0.0336
-4.500 -0.4468 0.04576 0.04104 0.0091 1.0000 0.0368
-4.250 -0.4332 0.03936 0.03449 0.0091 1.0000 0.0382
-4.000 -0.4156 0.03588 0.03103 0.0093 1.0000 0.0406
-3.750 -0.3934 0.03339 0.02836 0.0100 1.0000 0.0449
-3.500 -0.3685 0.03081 0.02530 0.0112 1.0000 0.0521
-3.250 -0.3455 0.02908 0.02324 0.0120 1.0000 0.0648
-3.000 -0.3231 0.02687 0.02089 0.0125 1.0000 0.0785
-2.750 -0.2998 0.02473 0.01863 0.0131 1.0000 0.0924
-2.500 -0.2764 0.02257 0.01645 0.0135 1.0000 0.1081
-2.000 -0.2087 0.01729 0.01008 0.0179 1.0000 0.0357
-1.750 -0.1815 0.01526 0.00791 0.0187 1.0000 0.0333
-1.500 -0.1546 0.01382 0.00640 0.0196 1.0000 0.0330
-1.250 -0.1055 0.01247 0.00489 0.0156 0.8848 0.0382
-1.000 -0.0732 0.01182 0.00390 0.0153 0.7654 0.0457
-0.750 0.0404 0.00888 0.00329 0.0005 0.6622 1.0000
-0.500 0.0623 0.00904 0.00307 0.0018 0.6134 1.0000
-0.250 0.0848 0.00919 0.00286 0.0029 0.5757 1.0000
0.000 0.1078 0.00931 0.00272 0.0039 0.5440 1.0000
0.250 0.1311 0.00944 0.00262 0.0048 0.5175 1.0000
0.500 0.1546 0.00957 0.00254 0.0056 0.4955 1.0000
0.750 0.1784 0.00968 0.00250 0.0064 0.4750 1.0000
1.000 0.2022 0.00982 0.00247 0.0071 0.4576 1.0000
1.250 0.2260 0.00995 0.00247 0.0079 0.4417 1.0000
1.500 0.2499 0.01010 0.00251 0.0086 0.4273 1.0000
1.750 0.2738 0.01025 0.00256 0.0094 0.4141 1.0000
2.000 0.2976 0.01042 0.00264 0.0102 0.4021 1.0000
2.250 0.3215 0.01057 0.00274 0.0109 0.3903 1.0000
2.500 0.3454 0.01075 0.00291 0.0116 0.3796 1.0000
2.750 0.3692 0.01095 0.00308 0.0124 0.3701 1.0000
3.000 0.3929 0.01119 0.00324 0.0132 0.3615 1.0000
3.250 0.4168 0.01136 0.00346 0.0139 0.3521 1.0000
3.500 0.4407 0.01161 0.00371 0.0147 0.3441 1.0000
3.750 0.4646 0.01186 0.00401 0.0154 0.3369 1.0000
4.000 0.4885 0.01212 0.00434 0.0162 0.3294 1.0000
4.250 0.5124 0.01240 0.00462 0.0169 0.3226 1.0000
4.500 0.5365 0.01269 0.00503 0.0176 0.3156 1.0000
4.750 0.5606 0.01301 0.00539 0.0183 0.3098 1.0000
5.000 0.5848 0.01335 0.00588 0.0190 0.3032 1.0000
5.250 0.6086 0.01350 0.00614 0.0198 0.2926 1.0000
5.500 0.6316 0.01311 0.00581 0.0207 0.2689 1.0000
5.750 0.6557 0.01277 0.00562 0.0214 0.2372 1.0000
6.000 0.6719 0.01509 0.00697 0.0225 0.0359 1.0000
6.250 0.6926 0.01657 0.00870 0.0235 0.0257 1.0000
6.500 0.7137 0.01786 0.01018 0.0246 0.0232 1.0000
6.750 0.7339 0.01939 0.01183 0.0258 0.0218 1.0000
7.000 0.7541 0.02106 0.01367 0.0270 0.0212 1.0000
7.250 0.7748 0.02303 0.01577 0.0283 0.0213 1.0000
7.500 0.7959 0.02538 0.01831 0.0295 0.0218 1.0000
7.750 0.8162 0.02831 0.02154 0.0307 0.0229 1.0000
8.000 0.8333 0.03243 0.02601 0.0317 0.0244 1.0000
8.250 0.8502 0.03689 0.03073 0.0325 0.0257 1.0000
8.500 0.8627 0.04099 0.03524 0.0330 0.0256 1.0000
17.250 0.6614 0.20132 0.19816 -0.0463 0.0252 1.0000
17.500 0.6649 0.20465 0.20150 -0.0483 0.0252 1.0000
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