FX 84-W-150 (fx84w150-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: FX 84-W-150 (fx84w150-il) Reynolds number: 1,000,000 Max Cl/Cd: 146.26 at α=6° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx84w150-il-1000000.txt Download as CSV file: xf-fx84w150-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: FX 84-W-150
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
------ -------- --------- --------- -------- -------- --------
-15.750 -0.7115 0.07661 0.07438 -0.0772 1.0000 0.0136
-15.500 -0.7944 0.05883 0.05632 -0.0889 1.0000 0.0133
-15.250 -0.8376 0.04724 0.04449 -0.0978 0.9949 0.0132
-15.000 -0.8341 0.03928 0.03627 -0.1101 0.9634 0.0133
-14.750 -0.8299 0.03532 0.03209 -0.1150 0.9363 0.0134
-14.500 -0.8406 0.03238 0.02892 -0.1152 0.9148 0.0135
-14.250 -0.8454 0.03028 0.02666 -0.1146 0.9006 0.0137
-14.000 -0.8489 0.02846 0.02470 -0.1135 0.8891 0.0137
-13.750 -0.8494 0.02701 0.02309 -0.1119 0.8793 0.0139
-13.500 -0.8500 0.02565 0.02160 -0.1099 0.8699 0.0141
-13.250 -0.8463 0.02467 0.02048 -0.1077 0.8620 0.0143
-13.000 -0.8416 0.02382 0.01953 -0.1052 0.8545 0.0144
-12.750 -0.8327 0.02302 0.01858 -0.1032 0.8482 0.0146
-12.500 -0.8177 0.02227 0.01772 -0.1020 0.8425 0.0147
-12.250 -0.8116 0.02077 0.01606 -0.1000 0.8362 0.0151
-12.000 -0.7972 0.01981 0.01499 -0.0987 0.8308 0.0154
-11.750 -0.7779 0.01914 0.01427 -0.0979 0.8257 0.0157
-11.500 -0.7569 0.01861 0.01367 -0.0973 0.8205 0.0161
-11.250 -0.7355 0.01810 0.01306 -0.0966 0.8155 0.0165
-11.000 -0.7132 0.01755 0.01245 -0.0962 0.8109 0.0169
-10.750 -0.6906 0.01701 0.01182 -0.0957 0.8061 0.0173
-10.500 -0.6669 0.01661 0.01131 -0.0952 0.8014 0.0177
-10.250 -0.6442 0.01602 0.01063 -0.0948 0.7970 0.0181
-10.000 -0.6226 0.01526 0.00983 -0.0942 0.7924 0.0189
-9.750 -0.5978 0.01489 0.00941 -0.0939 0.7878 0.0195
-9.500 -0.5729 0.01454 0.00899 -0.0937 0.7834 0.0201
-9.250 -0.5472 0.01416 0.00857 -0.0935 0.7794 0.0208
-9.000 -0.5213 0.01383 0.00816 -0.0934 0.7749 0.0214
-8.750 -0.4970 0.01330 0.00755 -0.0930 0.7705 0.0221
-8.500 -0.4718 0.01288 0.00709 -0.0928 0.7662 0.0232
-8.250 -0.4450 0.01260 0.00680 -0.0928 0.7624 0.0241
-8.000 -0.4180 0.01235 0.00650 -0.0927 0.7581 0.0251
-7.750 -0.3912 0.01209 0.00617 -0.0927 0.7538 0.0260
-7.500 -0.3657 0.01165 0.00570 -0.0925 0.7495 0.0276
-7.250 -0.3383 0.01140 0.00544 -0.0925 0.7454 0.0289
-7.000 -0.3109 0.01119 0.00519 -0.0925 0.7412 0.0301
-6.750 -0.2843 0.01087 0.00481 -0.0924 0.7370 0.0317
-6.500 -0.2571 0.01063 0.00456 -0.0924 0.7328 0.0336
-6.250 -0.2292 0.01045 0.00436 -0.0925 0.7285 0.0353
-6.000 -0.2018 0.01020 0.00407 -0.0926 0.7241 0.0371
-5.750 -0.1746 0.00998 0.00382 -0.0925 0.7195 0.0395
-5.500 -0.1465 0.00981 0.00364 -0.0927 0.7153 0.0417
-5.250 -0.1186 0.00959 0.00340 -0.0928 0.7109 0.0445
-5.000 -0.0908 0.00941 0.00322 -0.0928 0.7065 0.0478
-4.750 -0.0627 0.00932 0.00307 -0.0929 0.7021 0.0504
-4.500 -0.0348 0.00907 0.00287 -0.0931 0.6981 0.0559
-4.250 -0.0065 0.00893 0.00272 -0.0932 0.6938 0.0604
-4.000 0.0215 0.00877 0.00256 -0.0933 0.6896 0.0676
-3.750 0.0495 0.00863 0.00243 -0.0935 0.6853 0.0760
-3.500 0.0780 0.00847 0.00231 -0.0937 0.6812 0.0858
-3.250 0.1062 0.00833 0.00220 -0.0938 0.6767 0.0985
-3.000 0.1343 0.00821 0.00210 -0.0940 0.6724 0.1137
-2.750 0.1626 0.00806 0.00201 -0.0942 0.6684 0.1328
-2.500 0.1910 0.00791 0.00193 -0.0944 0.6641 0.1565
-2.250 0.2191 0.00775 0.00186 -0.0946 0.6595 0.1859
-2.000 0.2469 0.00760 0.00179 -0.0948 0.6550 0.2247
-1.750 0.2749 0.00736 0.00173 -0.0950 0.6511 0.2780
-1.500 0.3026 0.00706 0.00167 -0.0953 0.6465 0.3567
-1.250 0.3296 0.00672 0.00162 -0.0954 0.6418 0.4585
-1.000 0.3567 0.00644 0.00161 -0.0955 0.6372 0.5571
-0.750 0.3846 0.00624 0.00162 -0.0957 0.6325 0.6286
-0.500 0.4126 0.00617 0.00164 -0.0957 0.6276 0.6750
-0.250 0.4405 0.00616 0.00168 -0.0958 0.6229 0.7081
0.000 0.4691 0.00613 0.00171 -0.0960 0.6189 0.7334
0.250 0.4975 0.00613 0.00175 -0.0961 0.6141 0.7545
0.500 0.5256 0.00617 0.00178 -0.0961 0.6093 0.7717
0.750 0.5539 0.00620 0.00183 -0.0963 0.6049 0.7862
1.000 0.5824 0.00622 0.00188 -0.0964 0.6005 0.8007
1.500 0.6380 0.00634 0.00199 -0.0964 0.5910 0.8258
1.750 0.6661 0.00635 0.00204 -0.0965 0.5865 0.8380
2.000 0.6933 0.00640 0.00212 -0.0964 0.5814 0.8533
2.250 0.7200 0.00649 0.00219 -0.0961 0.5763 0.8666
2.500 0.7476 0.00652 0.00226 -0.0961 0.5714 0.8757
2.750 0.7749 0.00658 0.00232 -0.0961 0.5657 0.8838
3.000 0.8012 0.00667 0.00240 -0.0958 0.5601 0.8921
3.250 0.8287 0.00671 0.00246 -0.0958 0.5551 0.8996
3.500 0.8551 0.00677 0.00254 -0.0956 0.5496 0.9075
3.750 0.8808 0.00688 0.00263 -0.0953 0.5443 0.9155
4.000 0.9069 0.00692 0.00271 -0.0950 0.5394 0.9241
4.250 0.9319 0.00699 0.00279 -0.0944 0.5332 0.9329
4.500 0.9561 0.00709 0.00288 -0.0938 0.5267 0.9432
4.750 0.9795 0.00713 0.00296 -0.0929 0.5202 0.9546
5.000 1.0034 0.00724 0.00305 -0.0922 0.5135 0.9683
5.250 1.0350 0.00730 0.00315 -0.0932 0.5074 0.9806
5.500 1.0700 0.00743 0.00327 -0.0950 0.5004 0.9928
5.750 1.0996 0.00757 0.00340 -0.0958 0.4938 1.0000
6.000 1.1262 0.00770 0.00353 -0.0959 0.4863 1.0000
6.250 1.1516 0.00788 0.00368 -0.0957 0.4751 1.0000
6.500 1.1752 0.00812 0.00386 -0.0952 0.4586 1.0000
6.750 1.1984 0.00837 0.00406 -0.0947 0.4438 1.0000
7.000 1.2209 0.00864 0.00427 -0.0940 0.4295 1.0000
7.250 1.2429 0.00892 0.00450 -0.0932 0.4165 1.0000
7.500 1.2638 0.00922 0.00476 -0.0923 0.4024 1.0000
7.750 1.2836 0.00953 0.00503 -0.0911 0.3878 1.0000
8.000 1.3004 0.00989 0.00533 -0.0894 0.3707 1.0000
8.250 1.3133 0.01031 0.00568 -0.0870 0.3530 1.0000
8.500 1.3243 0.01081 0.00611 -0.0843 0.3333 1.0000
8.750 1.3328 0.01145 0.00664 -0.0815 0.3115 1.0000
9.000 1.3384 0.01226 0.00732 -0.0783 0.2835 1.0000
9.250 1.3443 0.01312 0.00806 -0.0753 0.2587 1.0000
9.500 1.3481 0.01414 0.00896 -0.0722 0.2325 1.0000
9.750 1.3503 0.01532 0.00998 -0.0691 0.2059 1.0000
10.000 1.3540 0.01649 0.01104 -0.0663 0.1820 1.0000
10.250 1.3553 0.01786 0.01228 -0.0635 0.1566 1.0000
10.500 1.3561 0.01934 0.01363 -0.0607 0.1331 1.0000
10.750 1.3561 0.02094 0.01510 -0.0581 0.1104 1.0000
11.000 1.3588 0.02246 0.01654 -0.0559 0.0932 1.0000
11.250 1.3619 0.02402 0.01803 -0.0539 0.0784 1.0000
11.500 1.3660 0.02557 0.01952 -0.0521 0.0668 1.0000
11.750 1.3718 0.02705 0.02098 -0.0506 0.0586 1.0000
12.000 1.3772 0.02861 0.02252 -0.0491 0.0513 1.0000
12.250 1.3820 0.03028 0.02416 -0.0477 0.0448 1.0000
12.500 1.3904 0.03172 0.02563 -0.0467 0.0410 1.0000
12.750 1.3957 0.03347 0.02737 -0.0455 0.0370 1.0000
13.000 1.4042 0.03499 0.02893 -0.0446 0.0344 1.0000
13.250 1.4090 0.03688 0.03082 -0.0436 0.0316 1.0000
13.500 1.4175 0.03849 0.03248 -0.0429 0.0301 1.0000
13.750 1.4247 0.04025 0.03427 -0.0422 0.0285 1.0000
14.000 1.4293 0.04228 0.03633 -0.0414 0.0267 1.0000
14.250 1.4348 0.04430 0.03840 -0.0408 0.0255 1.0000
14.500 1.4427 0.04612 0.04027 -0.0404 0.0246 1.0000
14.750 1.4486 0.04819 0.04238 -0.0399 0.0236 1.0000
15.000 1.4529 0.05045 0.04468 -0.0395 0.0226 1.0000
15.250 1.4527 0.05325 0.04754 -0.0391 0.0214 1.0000
15.500 1.4600 0.05529 0.04965 -0.0390 0.0209 1.0000
15.750 1.4663 0.05748 0.05190 -0.0388 0.0203 1.0000
16.000 1.4710 0.05988 0.05436 -0.0388 0.0196 1.0000
16.250 1.4745 0.06247 0.05700 -0.0388 0.0190 1.0000
16.500 1.4757 0.06537 0.05994 -0.0389 0.0183 1.0000
16.750 1.4704 0.06918 0.06383 -0.0391 0.0176 1.0000
17.000 1.4764 0.07160 0.06632 -0.0394 0.0173 1.0000
17.250 1.4815 0.07416 0.06896 -0.0397 0.0168 1.0000
17.500 1.4840 0.07710 0.07197 -0.0401 0.0163 1.0000
17.750 1.4859 0.08017 0.07510 -0.0406 0.0159 1.0000
18.000 1.4870 0.08338 0.07838 -0.0413 0.0155 1.0000
18.250 1.4862 0.08693 0.08199 -0.0420 0.0151 1.0000
18.500 1.4806 0.09120 0.08633 -0.0430 0.0146 1.0000
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