WORTMANN FX 77-W-343 AIRFOIL (fx77w343-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: WORTMANN FX 77-W-343 AIRFOIL (fx77w343-il) Reynolds number: 500,000 Max Cl/Cd: 45.17 at α=7.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx77w343-il-500000.txt Download as CSV file: xf-fx77w343-il-500000.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 = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.250 -0.9600 0.10342 0.09602 -0.0149 0.4982 0.0364
-19.000 -0.9546 0.10070 0.09325 -0.0158 0.4953 0.0368
-18.750 -0.9496 0.09791 0.09040 -0.0167 0.4925 0.0372
-18.500 -0.9422 0.09544 0.08786 -0.0175 0.4897 0.0377
-18.250 -0.9348 0.09298 0.08532 -0.0183 0.4867 0.0382
-18.000 -0.9279 0.09046 0.08274 -0.0190 0.4849 0.0387
-17.750 -0.9188 0.08823 0.08045 -0.0196 0.4833 0.0392
-17.500 -0.9094 0.08603 0.07818 -0.0201 0.4816 0.0396
-17.250 -0.9030 0.08353 0.07564 -0.0206 0.4799 0.0400
-17.000 -0.8986 0.08088 0.07297 -0.0211 0.4782 0.0405
-16.750 -0.8936 0.07828 0.07034 -0.0215 0.4765 0.0410
-16.500 -0.8862 0.07599 0.06799 -0.0219 0.4747 0.0415
-16.250 -0.8774 0.07386 0.06581 -0.0222 0.4729 0.0420
-16.000 -0.8687 0.07172 0.06361 -0.0226 0.4711 0.0426
-15.750 -0.8583 0.06976 0.06158 -0.0229 0.4692 0.0431
-15.500 -0.8466 0.06796 0.05970 -0.0232 0.4669 0.0436
-15.250 -0.8372 0.06595 0.05765 -0.0234 0.4657 0.0440
-15.000 -0.8283 0.06393 0.05562 -0.0235 0.4647 0.0447
-14.750 -0.8183 0.06205 0.05372 -0.0236 0.4637 0.0453
-14.500 -0.8076 0.06023 0.05188 -0.0237 0.4625 0.0459
-14.250 -0.7951 0.05863 0.05025 -0.0238 0.4613 0.0465
-14.000 -0.7819 0.05711 0.04872 -0.0239 0.4601 0.0473
-13.750 -0.7685 0.05562 0.04720 -0.0239 0.4589 0.0480
-13.500 -0.7554 0.05411 0.04568 -0.0240 0.4577 0.0489
-13.250 -0.7408 0.05278 0.04435 -0.0240 0.4565 0.0500
-13.000 -0.7252 0.05155 0.04310 -0.0241 0.4553 0.0512
-12.750 -0.7092 0.05034 0.04189 -0.0242 0.4541 0.0526
-12.500 -0.6928 0.04917 0.04071 -0.0243 0.4529 0.0543
-12.250 -0.6762 0.04805 0.03954 -0.0244 0.4517 0.0562
-12.000 -0.6590 0.04701 0.03847 -0.0244 0.4503 0.0578
-11.750 -0.6412 0.04605 0.03747 -0.0245 0.4486 0.0598
-11.500 -0.6216 0.04526 0.03662 -0.0248 0.4466 0.0616
-11.250 -0.6075 0.04400 0.03536 -0.0246 0.4461 0.0630
-11.000 -0.5912 0.04292 0.03426 -0.0245 0.4455 0.0646
-10.750 -0.5730 0.04199 0.03332 -0.0245 0.4449 0.0662
-10.500 -0.5584 0.04085 0.03217 -0.0243 0.4442 0.0678
-10.250 -0.5448 0.03966 0.03098 -0.0240 0.4436 0.0696
-10.000 -0.5299 0.03858 0.02989 -0.0237 0.4430 0.0714
-9.750 -0.5158 0.03749 0.02881 -0.0233 0.4423 0.0733
-9.500 -0.5019 0.03644 0.02777 -0.0229 0.4417 0.0755
-9.250 -0.4884 0.03541 0.02677 -0.0224 0.4410 0.0785
-9.000 -0.4763 0.03433 0.02574 -0.0217 0.4403 0.0825
-8.750 -0.4645 0.03324 0.02471 -0.0210 0.4397 0.0928
-8.500 -0.4488 0.03240 0.02387 -0.0205 0.4390 0.0993
-8.250 -0.4337 0.03154 0.02300 -0.0200 0.4383 0.1038
-8.000 -0.4214 0.03053 0.02200 -0.0192 0.4377 0.1084
-7.750 -0.4120 0.02939 0.02090 -0.0181 0.4371 0.1143
-7.500 -0.4090 0.02801 0.01963 -0.0162 0.4365 0.1274
-7.250 -0.4095 0.02697 0.01859 -0.0134 0.4360 0.1410
-7.000 -0.4070 0.02596 0.01758 -0.0111 0.4354 0.1482
-6.750 -0.3938 0.02481 0.01649 -0.0111 0.4346 0.1598
-6.500 -0.3749 0.02340 0.01522 -0.0127 0.4337 0.1922
-6.250 -0.3467 0.02241 0.01430 -0.0153 0.4329 0.2105
-6.000 -0.3140 0.02111 0.01317 -0.0194 0.4322 0.2531
-5.750 -0.2794 0.02000 0.01228 -0.0234 0.4313 0.3057
-5.500 -0.2422 0.01900 0.01154 -0.0277 0.4304 0.3642
-5.250 -0.2042 0.01835 0.01117 -0.0315 0.4291 0.4259
-5.000 -0.1691 0.01846 0.01140 -0.0339 0.4277 0.4544
-4.750 -0.1336 0.01840 0.01148 -0.0362 0.4271 0.4870
-4.500 -0.0987 0.01834 0.01147 -0.0380 0.4267 0.5039
-4.000 -0.0299 0.01844 0.01174 -0.0413 0.4258 0.5342
-3.750 0.0043 0.01856 0.01189 -0.0428 0.4253 0.5481
-3.500 0.0387 0.01866 0.01194 -0.0444 0.4247 0.5567
-3.250 0.0722 0.01883 0.01215 -0.0457 0.4241 0.5633
-3.000 0.1062 0.01897 0.01229 -0.0472 0.4233 0.5709
-2.750 0.1399 0.01913 0.01244 -0.0487 0.4225 0.5770
-2.500 0.1727 0.01942 0.01277 -0.0498 0.4216 0.5822
-2.250 0.2059 0.01968 0.01304 -0.0510 0.4208 0.5877
-2.000 0.2399 0.01987 0.01318 -0.0526 0.4200 0.5934
-1.750 0.2723 0.02020 0.01354 -0.0537 0.4192 0.5966
-1.500 0.3050 0.02050 0.01384 -0.0548 0.4184 0.5998
-1.250 0.3380 0.02077 0.01409 -0.0561 0.4176 0.6036
-1.000 0.3717 0.02098 0.01425 -0.0577 0.4167 0.6078
-0.750 0.4057 0.02114 0.01435 -0.0593 0.4159 0.6113
-0.500 0.4376 0.02138 0.01460 -0.0602 0.4150 0.6133
-0.250 0.4694 0.02166 0.01488 -0.0612 0.4141 0.6156
0.000 0.5014 0.02195 0.01516 -0.0621 0.4133 0.6184
0.250 0.5338 0.02224 0.01542 -0.0633 0.4124 0.6214
0.500 0.5665 0.02257 0.01570 -0.0646 0.4114 0.6247
0.750 0.5991 0.02309 0.01616 -0.0662 0.4102 0.6278
1.000 0.6295 0.02384 0.01692 -0.0675 0.4089 0.6300
1.250 0.6606 0.02394 0.01707 -0.0684 0.4084 0.6317
1.500 0.6913 0.02414 0.01732 -0.0693 0.4078 0.6333
1.750 0.7217 0.02442 0.01765 -0.0701 0.4072 0.6352
2.000 0.7517 0.02475 0.01802 -0.0709 0.4064 0.6374
2.250 0.7818 0.02508 0.01839 -0.0717 0.4055 0.6401
2.500 0.8122 0.02538 0.01872 -0.0726 0.4046 0.6429
2.750 0.8433 0.02563 0.01897 -0.0739 0.4036 0.6455
3.000 0.8749 0.02589 0.01923 -0.0753 0.4026 0.6479
3.250 0.9058 0.02601 0.01936 -0.0766 0.4015 0.6501
3.500 0.9347 0.02618 0.01958 -0.0773 0.4006 0.6520
3.750 0.9635 0.02642 0.01985 -0.0779 0.3996 0.6536
4.000 0.9929 0.02662 0.02007 -0.0787 0.3987 0.6551
4.250 1.0230 0.02676 0.02021 -0.0797 0.3978 0.6565
4.500 1.0537 0.02686 0.02030 -0.0809 0.3970 0.6577
4.750 1.0846 0.02695 0.02038 -0.0821 0.3962 0.6589
5.000 1.1157 0.02703 0.02043 -0.0834 0.3954 0.6602
5.250 1.1470 0.02714 0.02050 -0.0848 0.3945 0.6615
5.500 1.1775 0.02738 0.02071 -0.0861 0.3934 0.6631
5.750 1.2022 0.02841 0.02177 -0.0869 0.3913 0.6647
6.000 1.2301 0.02855 0.02193 -0.0879 0.3907 0.6662
6.250 1.2569 0.02876 0.02218 -0.0888 0.3900 0.6674
6.500 1.2826 0.02903 0.02249 -0.0895 0.3890 0.6684
6.750 1.3063 0.02938 0.02287 -0.0899 0.3879 0.6692
7.000 1.3287 0.02957 0.02312 -0.0902 0.3866 0.6705
7.250 1.3493 0.02987 0.02347 -0.0901 0.3854 0.6716
7.500 1.3677 0.03031 0.02397 -0.0897 0.3843 0.6727
7.750 1.3849 0.03076 0.02447 -0.0891 0.3833 0.6737
8.000 1.4012 0.03120 0.02494 -0.0884 0.3822 0.6747
8.250 1.4053 0.03181 0.02559 -0.0857 0.3811 0.6756
8.500 1.4166 0.03244 0.02625 -0.0845 0.3801 0.6767
8.750 1.4345 0.03299 0.02681 -0.0843 0.3791 0.6781
9.000 1.4566 0.03337 0.02719 -0.0846 0.3781 0.6795
9.250 1.4803 0.03370 0.02749 -0.0852 0.3771 0.6808
9.500 1.5036 0.03414 0.02791 -0.0857 0.3756 0.6822
9.750 1.4964 0.03664 0.03050 -0.0839 0.3736 0.6834
10.000 0.7309 0.12178 0.11693 -0.0652 0.3141 0.6775
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