WORTMANN FX 77-W-343 AIRFOIL (fx77w343-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 77-W-343 AIRFOIL (fx77w343-il) Reynolds number: 1,000,000 Max Cl/Cd: 87.56 at α=7.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx77w343-il-1000000-n5.txt Download as CSV file: xf-fx77w343-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 77-W-343 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.250 -1.0558 0.09283 0.08556 -0.0151 0.4402 0.0156
-19.000 -1.0513 0.09008 0.08275 -0.0158 0.4392 0.0156
-18.750 -1.0440 0.08767 0.08030 -0.0164 0.4381 0.0157
-18.500 -1.0379 0.08511 0.07769 -0.0169 0.4370 0.0158
-18.250 -1.0302 0.08279 0.07531 -0.0174 0.4358 0.0159
-18.000 -1.0213 0.08061 0.07308 -0.0178 0.4347 0.0160
-17.750 -1.0140 0.07824 0.07067 -0.0183 0.4334 0.0161
-17.500 -1.0047 0.07616 0.06854 -0.0186 0.4321 0.0162
-17.250 -0.9943 0.07420 0.06655 -0.0189 0.4307 0.0163
-17.000 -0.9846 0.07215 0.06445 -0.0192 0.4294 0.0164
-16.750 -0.9748 0.07012 0.06238 -0.0195 0.4280 0.0165
-16.500 -0.9635 0.06829 0.06052 -0.0197 0.4271 0.0166
-16.250 -0.9527 0.06640 0.05860 -0.0199 0.4268 0.0167
-16.000 -0.9415 0.06457 0.05674 -0.0201 0.4263 0.0168
-15.750 -0.9289 0.06292 0.05507 -0.0202 0.4258 0.0169
-15.500 -0.9166 0.06124 0.05335 -0.0204 0.4252 0.0170
-15.250 -0.9046 0.05951 0.05160 -0.0205 0.4245 0.0171
-15.000 -0.8906 0.05803 0.05009 -0.0206 0.4237 0.0172
-14.750 -0.8763 0.05659 0.04863 -0.0206 0.4229 0.0173
-14.500 -0.8621 0.05514 0.04716 -0.0207 0.4219 0.0174
-14.250 -0.8487 0.05362 0.04561 -0.0207 0.4209 0.0175
-14.000 -0.8341 0.05225 0.04421 -0.0208 0.4198 0.0176
-13.750 -0.8186 0.05098 0.04292 -0.0208 0.4185 0.0178
-13.500 -0.8030 0.04971 0.04162 -0.0208 0.4172 0.0179
-13.250 -0.7879 0.04839 0.04027 -0.0208 0.4158 0.0180
-13.000 -0.7727 0.04709 0.03894 -0.0208 0.4145 0.0181
-12.750 -0.7562 0.04595 0.03777 -0.0208 0.4131 0.0182
-12.500 -0.7397 0.04482 0.03661 -0.0208 0.4118 0.0183
-12.250 -0.7234 0.04366 0.03543 -0.0208 0.4106 0.0184
-12.000 -0.7074 0.04249 0.03423 -0.0207 0.4093 0.0185
-11.750 -0.6903 0.04144 0.03317 -0.0207 0.4087 0.0186
-11.500 -0.6729 0.04041 0.03213 -0.0206 0.4083 0.0188
-11.250 -0.6556 0.03940 0.03111 -0.0205 0.4078 0.0191
-11.000 -0.6389 0.03835 0.03006 -0.0204 0.4074 0.0193
-10.750 -0.6229 0.03726 0.02896 -0.0203 0.4068 0.0196
-10.500 -0.6061 0.03627 0.02795 -0.0201 0.4063 0.0199
-10.250 -0.5888 0.03533 0.02701 -0.0199 0.4057 0.0203
-10.000 -0.5715 0.03441 0.02609 -0.0197 0.4050 0.0207
-9.750 -0.5547 0.03349 0.02517 -0.0194 0.4044 0.0212
-9.250 -0.5265 0.03141 0.02316 -0.0184 0.4032 0.0299
-9.000 -0.5084 0.03062 0.02236 -0.0182 0.4025 0.0310
-8.750 -0.4903 0.02985 0.02158 -0.0179 0.4019 0.0317
-8.500 -0.4731 0.02901 0.02074 -0.0176 0.4012 0.0324
-8.250 -0.4568 0.02814 0.01986 -0.0171 0.4006 0.0333
-8.000 -0.4399 0.02732 0.01903 -0.0167 0.4000 0.0341
-7.750 -0.4225 0.02655 0.01825 -0.0163 0.3993 0.0347
-7.500 -0.4055 0.02576 0.01744 -0.0158 0.3987 0.0354
-7.250 -0.3911 0.02490 0.01657 -0.0149 0.3981 0.0358
-7.000 -0.3918 0.02388 0.01554 -0.0118 0.3976 0.0363
-6.750 -0.3758 0.02307 0.01471 -0.0114 0.3970 0.0370
-6.500 -0.3541 0.02234 0.01397 -0.0119 0.3964 0.0376
-6.250 -0.3286 0.02172 0.01335 -0.0129 0.3957 0.0380
-6.000 -0.3007 0.02116 0.01278 -0.0143 0.3950 0.0384
-5.750 -0.2711 0.02065 0.01226 -0.0160 0.3942 0.0388
-5.500 -0.2401 0.02020 0.01180 -0.0178 0.3935 0.0392
-5.250 -0.2080 0.01978 0.01137 -0.0197 0.3927 0.0396
-5.000 -0.1751 0.01939 0.01097 -0.0218 0.3920 0.0400
-4.750 -0.1413 0.01900 0.01058 -0.0241 0.3913 0.0406
-4.500 -0.1071 0.01863 0.01022 -0.0263 0.3911 0.0412
-4.250 -0.0730 0.01833 0.00993 -0.0284 0.3909 0.0420
-4.000 -0.0391 0.01808 0.00969 -0.0303 0.3906 0.0430
-3.750 -0.0051 0.01782 0.00946 -0.0323 0.3901 0.0452
-3.500 0.0294 0.01752 0.00923 -0.0344 0.3895 0.0601
-3.250 0.0636 0.01735 0.00907 -0.0362 0.3887 0.0632
-3.000 0.0979 0.01719 0.00893 -0.0381 0.3879 0.0655
-2.750 0.1321 0.01707 0.00881 -0.0398 0.3872 0.0667
-2.500 0.1665 0.01693 0.00868 -0.0417 0.3866 0.0682
-2.250 0.2009 0.01680 0.00857 -0.0435 0.3859 0.0705
-2.000 0.2353 0.01669 0.00847 -0.0454 0.3853 0.0726
-1.750 0.2701 0.01653 0.00837 -0.0473 0.3847 0.0796
-1.500 0.3050 0.01637 0.00826 -0.0494 0.3842 0.1000
-1.250 0.3394 0.01629 0.00820 -0.0512 0.3836 0.1046
-1.000 0.3750 0.01607 0.00808 -0.0534 0.3830 0.1266
-0.750 0.4102 0.01591 0.00798 -0.0556 0.3824 0.1522
-0.500 0.4470 0.01556 0.00781 -0.0583 0.3818 0.2019
-0.250 0.4840 0.01523 0.00764 -0.0611 0.3811 0.2527
0.000 0.5210 0.01490 0.00749 -0.0638 0.3805 0.3053
0.250 0.5589 0.01448 0.00730 -0.0669 0.3798 0.3674
0.500 0.5966 0.01408 0.00714 -0.0699 0.3791 0.4374
0.750 0.6316 0.01400 0.00713 -0.0719 0.3783 0.4573
1.000 0.6668 0.01389 0.00713 -0.0740 0.3774 0.4922
1.250 0.7009 0.01391 0.00718 -0.0758 0.3764 0.5060
1.500 0.7358 0.01385 0.00728 -0.0778 0.3752 0.5442
1.750 0.7689 0.01397 0.00741 -0.0793 0.3741 0.5574
2.000 0.8026 0.01402 0.00750 -0.0809 0.3738 0.5667
2.250 0.8360 0.01409 0.00758 -0.0824 0.3734 0.5728
2.500 0.8694 0.01416 0.00767 -0.0840 0.3729 0.5774
2.750 0.9027 0.01425 0.00780 -0.0855 0.3724 0.5829
3.000 0.9357 0.01435 0.00794 -0.0869 0.3718 0.5895
3.250 0.9685 0.01448 0.00809 -0.0883 0.3711 0.5955
3.500 1.0012 0.01461 0.00825 -0.0897 0.3703 0.6011
3.750 1.0339 0.01473 0.00837 -0.0912 0.3695 0.6047
4.000 1.0664 0.01484 0.00848 -0.0926 0.3686 0.6075
4.250 1.0989 0.01496 0.00859 -0.0940 0.3675 0.6098
4.500 1.1312 0.01509 0.00873 -0.0954 0.3664 0.6124
4.750 1.1632 0.01523 0.00890 -0.0967 0.3652 0.6152
5.000 1.1950 0.01539 0.00906 -0.0980 0.3640 0.6179
5.250 1.2266 0.01555 0.00922 -0.0993 0.3628 0.6203
5.500 1.2580 0.01571 0.00938 -0.1006 0.3614 0.6223
5.750 1.2891 0.01589 0.00954 -0.1018 0.3598 0.6241
6.000 1.3197 0.01609 0.00973 -0.1030 0.3578 0.6253
6.250 1.3509 0.01623 0.00988 -0.1043 0.3568 0.6263
6.500 1.3821 0.01637 0.01003 -0.1056 0.3556 0.6270
6.750 1.4130 0.01652 0.01019 -0.1068 0.3538 0.6276
7.000 1.4435 0.01667 0.01035 -0.1080 0.3508 0.6281
7.250 1.4733 0.01687 0.01052 -0.1091 0.3463 0.6285
7.500 1.5013 0.01716 0.01076 -0.1100 0.3410 0.6289
7.750 1.5288 0.01746 0.01104 -0.1108 0.3366 0.6295
8.000 1.5547 0.01782 0.01138 -0.1114 0.3320 0.6305
8.250 1.5794 0.01823 0.01178 -0.1119 0.3288 0.6315
8.500 1.6035 0.01864 0.01220 -0.1122 0.3264 0.6324
8.750 1.6275 0.01902 0.01261 -0.1125 0.3251 0.6332
9.000 1.6496 0.01946 0.01308 -0.1125 0.3237 0.6340
9.250 1.6684 0.02002 0.01367 -0.1120 0.3223 0.6347
9.500 1.6695 0.02104 0.01475 -0.1087 0.3211 0.6353
9.750 1.6754 0.02243 0.01620 -0.1071 0.3198 0.6360
10.000 1.6833 0.02401 0.01783 -0.1063 0.3184 0.6366
10.250 1.6903 0.02583 0.01970 -0.1058 0.3168 0.6372
10.500 1.6948 0.02797 0.02189 -0.1054 0.3152 0.6378
10.750 1.6970 0.03032 0.02430 -0.1049 0.3136 0.6383
11.000 1.6936 0.03321 0.02726 -0.1042 0.3117 0.6389
11.250 1.6957 0.03563 0.02975 -0.1038 0.3107 0.6395
11.500 1.6978 0.03808 0.03227 -0.1035 0.3097 0.6401
11.750 1.6951 0.04096 0.03524 -0.1030 0.3084 0.6408
12.000 1.6867 0.04436 0.03873 -0.1023 0.3066 0.6414
12.250 1.6656 0.04904 0.04350 -0.1011 0.3044 0.6419
12.500 1.6376 0.05442 0.04899 -0.0998 0.3018 0.6423
12.750 1.5836 0.06261 0.05731 -0.0977 0.2981 0.6425
13.000 1.5401 0.06989 0.06468 -0.0962 0.2947 0.6428
13.250 1.5133 0.07565 0.07053 -0.0955 0.2905 0.6432
13.500 1.4252 0.08810 0.08306 -0.0932 0.2774 0.6431
13.750 1.4030 0.09358 0.08853 -0.0929 0.2707 0.6435
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