FX 83-W-227 (fx83w227-il) Xfoil prediction polar at RE=200,000 Ncrit=9
| Details | Polar file |
|---|---|
|
Airfoil: FX 83-W-227 (fx83w227-il) Reynolds number: 200,000 Max Cl/Cd: 56.25 at α=8.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx83w227-il-200000.txt Download as CSV file: xf-fx83w227-il-200000.csv |
XFOIL Version 6.96
Calculated polar for: FX 83-W-227
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
------ -------- --------- --------- -------- -------- --------
-16.750 -0.7466 0.08217 0.07758 -0.0942 1.0000 0.0800
-16.500 -0.8187 0.07281 0.06795 -0.0963 1.0000 0.0797
-16.250 -0.8676 0.06741 0.06236 -0.0956 1.0000 0.0797
-16.000 -0.9100 0.06351 0.05830 -0.0935 1.0000 0.0798
-15.750 -0.9420 0.05948 0.05403 -0.0931 0.9986 0.0802
-15.500 -0.9592 0.05471 0.04889 -0.0966 0.9938 0.0811
-15.250 -0.9442 0.05210 0.04620 -0.0989 0.9900 0.0825
-15.000 -0.9163 0.05084 0.04498 -0.1013 0.9862 0.0840
-14.750 -0.8982 0.04897 0.04302 -0.1040 0.9827 0.0857
-14.500 -0.8884 0.04691 0.04080 -0.1055 0.9769 0.0872
-14.250 -0.8806 0.04454 0.03817 -0.1071 0.9717 0.0888
-14.000 -0.8787 0.04252 0.03586 -0.1074 0.9648 0.0900
-13.750 -0.8525 0.04067 0.03396 -0.1092 0.9606 0.0918
-13.500 -0.8185 0.03958 0.03291 -0.1118 0.9579 0.0938
-13.250 -0.7993 0.03839 0.03164 -0.1125 0.9521 0.0957
-13.000 -0.7823 0.03705 0.03015 -0.1131 0.9459 0.0978
-12.750 -0.7608 0.03558 0.02843 -0.1147 0.9426 0.0998
-12.500 -0.7373 0.03425 0.02705 -0.1151 0.9364 0.1019
-12.250 -0.7059 0.03331 0.02618 -0.1167 0.9319 0.1043
-12.000 -0.6747 0.03223 0.02504 -0.1188 0.9289 0.1072
-11.750 -0.6430 0.03098 0.02360 -0.1212 0.9268 0.1102
-11.500 -0.6247 0.03001 0.02253 -0.1205 0.9190 0.1124
-11.250 -0.5854 0.02899 0.02161 -0.1233 0.9160 0.1158
-11.000 -0.5509 0.02803 0.02058 -0.1258 0.9130 0.1198
-10.750 -0.5188 0.02702 0.01936 -0.1279 0.9102 0.1234
-10.500 -0.4883 0.02611 0.01858 -0.1288 0.9038 0.1273
-10.250 -0.4618 0.02539 0.01784 -0.1294 0.8977 0.1314
-10.000 -0.4306 0.02455 0.01683 -0.1311 0.8937 0.1362
-9.750 -0.4016 0.02374 0.01613 -0.1318 0.8876 0.1411
-9.500 -0.3805 0.02317 0.01553 -0.1313 0.8800 0.1459
-9.250 -0.3470 0.02234 0.01461 -0.1330 0.8756 0.1522
-9.000 -0.3339 0.02192 0.01425 -0.1309 0.8667 0.1572
-8.750 -0.3113 0.02140 0.01364 -0.1305 0.8601 0.1636
-8.500 -0.2816 0.02065 0.01293 -0.1316 0.8553 0.1713
-8.250 -0.2767 0.02044 0.01271 -0.1277 0.8453 0.1769
-8.000 -0.2526 0.01984 0.01209 -0.1276 0.8396 0.1856
-7.750 -0.2427 0.01957 0.01183 -0.1247 0.8319 0.1931
-7.500 -0.2289 0.01918 0.01143 -0.1224 0.8244 0.2019
-7.250 -0.2067 0.01871 0.01092 -0.1218 0.8192 0.2135
-7.000 -0.2069 0.01856 0.01086 -0.1169 0.8105 0.2217
-6.750 -0.1933 0.01827 0.01054 -0.1144 0.8040 0.2346
-6.500 -0.1739 0.01785 0.01013 -0.1132 0.7993 0.2507
-6.250 -0.1802 0.01780 0.01020 -0.1069 0.7904 0.2618
-6.000 -0.1670 0.01744 0.00990 -0.1044 0.7846 0.2811
-5.750 -0.1464 0.01705 0.00953 -0.1033 0.7802 0.3070
-5.500 -0.1500 0.01701 0.00962 -0.0974 0.7720 0.3264
-5.250 -0.1388 0.01669 0.00941 -0.0944 0.7662 0.3540
-5.000 -0.1186 0.01633 0.00913 -0.0931 0.7620 0.3879
-4.750 -0.1158 0.01627 0.00921 -0.0884 0.7551 0.4142
-4.500 -0.1043 0.01611 0.00914 -0.0852 0.7489 0.4445
-4.250 -0.0825 0.01588 0.00899 -0.0840 0.7445 0.4775
-4.000 -0.0630 0.01581 0.00898 -0.0823 0.7397 0.5064
-3.750 -0.0562 0.01588 0.00915 -0.0782 0.7327 0.5293
-3.500 -0.0342 0.01582 0.00911 -0.0769 0.7277 0.5538
-3.250 -0.0043 0.01578 0.00901 -0.0771 0.7239 0.5775
-3.000 0.0084 0.01592 0.00921 -0.0740 0.7179 0.5946
-2.750 0.0249 0.01600 0.00932 -0.0716 0.7119 0.6110
-2.500 0.0533 0.01600 0.00928 -0.0715 0.7074 0.6279
-2.250 0.0873 0.01602 0.00921 -0.0725 0.7038 0.6442
-2.000 0.0929 0.01623 0.00949 -0.0681 0.6970 0.6566
-1.750 0.1155 0.01630 0.00956 -0.0669 0.6915 0.6689
-1.500 0.1456 0.01628 0.00945 -0.0671 0.6873 0.6828
-1.250 0.1757 0.01641 0.00958 -0.0674 0.6830 0.6941
-1.000 0.1830 0.01655 0.00976 -0.0633 0.6764 0.7053
-0.750 0.2095 0.01662 0.00982 -0.0628 0.6714 0.7171
-0.500 0.2452 0.01664 0.00977 -0.0641 0.6674 0.7287
-0.250 0.2602 0.01679 0.00994 -0.0615 0.6619 0.7401
0.000 0.2761 0.01689 0.01008 -0.0590 0.6559 0.7493
0.250 0.3046 0.01690 0.01004 -0.0590 0.6513 0.7600
0.500 0.3438 0.01690 0.00995 -0.0611 0.6474 0.7689
0.750 0.3484 0.01705 0.01019 -0.0565 0.6408 0.7784
1.000 0.3666 0.01705 0.01017 -0.0546 0.6354 0.7877
1.250 0.4022 0.01705 0.01013 -0.0560 0.6311 0.7955
1.500 0.4268 0.01707 0.01006 -0.0555 0.6266 0.8055
1.750 0.4351 0.01719 0.01030 -0.0517 0.6201 0.8133
2.000 0.4576 0.01715 0.01022 -0.0506 0.6150 0.8230
2.250 0.4972 0.01714 0.01014 -0.0529 0.6109 0.8302
2.500 0.5089 0.01727 0.01033 -0.0498 0.6054 0.8399
2.750 0.5205 0.01730 0.01040 -0.0467 0.5994 0.8497
3.000 0.5544 0.01731 0.01037 -0.0479 0.5946 0.8579
3.250 0.5940 0.01734 0.01028 -0.0503 0.5907 0.8664
3.500 0.5947 0.01756 0.01066 -0.0452 0.5843 0.8768
3.750 0.6155 0.01761 0.01071 -0.0439 0.5789 0.8870
4.000 0.6633 0.01771 0.01074 -0.0479 0.5744 0.8925
4.250 0.6807 0.01789 0.01093 -0.0461 0.5693 0.9039
4.500 0.7053 0.01821 0.01133 -0.0458 0.5632 0.9112
4.750 0.7377 0.01832 0.01139 -0.0469 0.5583 0.9207
5.000 0.7966 0.01852 0.01147 -0.0533 0.5539 0.9232
5.250 0.8118 0.01898 0.01207 -0.0514 0.5474 0.9323
5.500 0.8445 0.01922 0.01231 -0.0528 0.5419 0.9402
5.750 0.9012 0.01943 0.01242 -0.0588 0.5373 0.9419
6.000 0.9334 0.01984 0.01288 -0.0603 0.5318 0.9485
6.250 0.9600 0.02014 0.01323 -0.0608 0.5257 0.9570
6.500 1.0082 0.02032 0.01336 -0.0652 0.5207 0.9608
6.750 1.0510 0.02061 0.01359 -0.0686 0.5160 0.9669
7.000 1.0747 0.02099 0.01409 -0.0689 0.5097 0.9758
7.250 1.1136 0.02117 0.01427 -0.0718 0.5043 0.9824
7.500 1.1695 0.02135 0.01434 -0.0777 0.4997 0.9842
7.750 1.1938 0.02176 0.01489 -0.0783 0.4936 0.9941
8.000 1.2316 0.02199 0.01515 -0.0813 0.4878 1.0000
8.250 1.2288 0.02190 0.01500 -0.0764 0.4840 1.0000
8.500 1.2374 0.02200 0.01503 -0.0735 0.4801 1.0000
8.750 1.1953 0.02230 0.01541 -0.0614 0.4759 1.0000
9.000 1.1904 0.02264 0.01577 -0.0561 0.4712 1.0000
9.250 1.2103 0.02276 0.01584 -0.0550 0.4667 1.0000
9.500 1.2467 0.02292 0.01591 -0.0568 0.4626 1.0000
9.750 1.2197 0.02368 0.01680 -0.0479 0.4578 1.0000
10.000 1.2215 0.02419 0.01734 -0.0441 0.4530 1.0000
10.250 1.2463 0.02433 0.01744 -0.0438 0.4486 1.0000
10.500 1.2790 0.02450 0.01755 -0.0449 0.4444 1.0000
10.750 1.2544 0.02558 0.01877 -0.0373 0.4393 1.0000
11.000 1.2600 0.02616 0.01939 -0.0343 0.4343 1.0000
11.250 1.2906 0.02614 0.01931 -0.0350 0.4298 1.0000
11.500 1.3042 0.02670 0.01989 -0.0333 0.4253 1.0000
11.750 1.2858 0.02799 0.02131 -0.0273 0.4198 1.0000
12.000 1.2995 0.02844 0.02176 -0.0258 0.4149 1.0000
12.250 1.3401 0.02817 0.02140 -0.0277 0.4105 1.0000
12.500 1.3219 0.02971 0.02308 -0.0223 0.4054 1.0000
12.750 1.3155 0.03093 0.02439 -0.0185 0.3998 1.0000
13.000 1.3427 0.03086 0.02427 -0.0186 0.3948 1.0000
13.250 1.3516 0.03162 0.02505 -0.0168 0.3895 1.0000
13.500 1.3310 0.03355 0.02711 -0.0120 0.3831 1.0000
13.750 1.3552 0.03341 0.02689 -0.0118 0.3768 1.0000
14.000 1.3512 0.03484 0.02839 -0.0090 0.3708 1.0000
14.250 1.3400 0.03668 0.03033 -0.0058 0.3644 1.0000
14.500 1.3659 0.03654 0.03012 -0.0057 0.3588 1.0000
14.750 1.3538 0.03869 0.03239 -0.0028 0.3527 1.0000
15.000 1.3476 0.04057 0.03435 -0.0005 0.3463 1.0000
15.250 1.3760 0.04027 0.03396 -0.0006 0.3410 1.0000
15.500 1.3559 0.04329 0.03713 0.0023 0.3348 1.0000
15.750 1.3533 0.04518 0.03908 0.0039 0.3284 1.0000
16.000 1.3881 0.04434 0.03813 0.0034 0.3229 1.0000
16.250 1.3512 0.04901 0.04303 0.0065 0.3158 1.0000
16.500 1.3590 0.05023 0.04425 0.0073 0.3093 1.0000
16.750 1.3615 0.05199 0.04605 0.0083 0.3030 1.0000
17.000 1.3462 0.05541 0.04958 0.0097 0.2955 1.0000
17.250 1.3702 0.05523 0.04929 0.0098 0.2890 1.0000
17.500 1.3389 0.06038 0.05464 0.0113 0.2809 1.0000
17.750 1.3581 0.06062 0.05478 0.0115 0.2737 1.0000
18.000 1.3304 0.06576 0.06011 0.0125 0.2655 1.0000
18.250 1.3438 0.06660 0.06086 0.0128 0.2578 1.0000
18.500 1.3186 0.07175 0.06617 0.0132 0.2489 1.0000
18.750 1.3283 0.07301 0.06734 0.0135 0.2404 1.0000
19.000 1.3050 0.07820 0.07267 0.0136 0.2310 1.0000
19.250 1.3028 0.08095 0.07539 0.0136 0.2221 1.0000
|
Polar data table (+)
Polar graphs
<< Back to FX 83-W-227 (fx83w227-il)