WORTMANN FX 73-170 A (fx73170a-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 73-170 A (fx73170a-il) Reynolds number: 200,000 Max Cl/Cd: 51.19 at α=6° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx73170a-il-200000-n5.txt Download as CSV file: xf-fx73170a-il-200000-n5.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 73-170 A
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-13.500 -0.0115 0.12572 0.12055 -0.1227 0.7669 0.0248
-13.250 -0.0107 0.12255 0.11737 -0.1252 0.7651 0.0250
-13.000 -0.0055 0.11944 0.11424 -0.1272 0.7632 0.0251
-12.750 -0.0016 0.11606 0.11089 -0.1290 0.7608 0.0252
-12.500 0.0020 0.11261 0.10746 -0.1309 0.7586 0.0252
-12.000 0.0115 0.10587 0.10074 -0.1340 0.7538 0.0253
-11.750 0.0186 0.10252 0.09738 -0.1348 0.7518 0.0254
-11.500 0.0300 0.09982 0.09463 -0.1346 0.7498 0.0259
-11.250 0.0347 0.09670 0.09150 -0.1362 0.7479 0.0259
-11.000 0.0372 0.09332 0.08815 -0.1379 0.7456 0.0258
-10.750 0.0973 0.07454 0.06967 -0.1292 0.7336 0.0193
-10.500 0.0986 0.07117 0.06632 -0.1299 0.7317 0.0187
-10.000 0.0303 0.07466 0.06956 -0.1443 0.7372 0.0157
-9.750 0.0350 0.07242 0.06732 -0.1451 0.7353 0.0155
-9.500 0.0427 0.07079 0.06566 -0.1457 0.7335 0.0149
-9.250 0.0348 0.06601 0.06094 -0.1481 0.7311 0.0149
-9.000 0.0224 0.06042 0.05542 -0.1518 0.7282 0.0146
-8.750 0.0019 0.05500 0.04997 -0.1543 0.7253 0.0146
-8.500 -0.0158 0.05162 0.04654 -0.1536 0.7227 0.0143
-8.250 -0.0361 0.04872 0.04353 -0.1508 0.7204 0.0142
-8.000 -0.0472 0.04558 0.04019 -0.1486 0.7186 0.0137
-7.750 -0.0587 0.04193 0.03632 -0.1458 0.7164 0.0137
-7.500 -0.0646 0.03856 0.03270 -0.1429 0.7139 0.0136
-7.250 -0.0654 0.03536 0.02919 -0.1401 0.7115 0.0135
-7.000 -0.0605 0.03261 0.02607 -0.1376 0.7093 0.0137
-6.750 -0.0514 0.03004 0.02311 -0.1354 0.7073 0.0137
-6.500 -0.0376 0.02793 0.02059 -0.1337 0.7054 0.0146
-6.250 -0.0209 0.02583 0.01791 -0.1320 0.7038 0.0157
-6.000 -0.0007 0.02437 0.01616 -0.1310 0.7022 0.0159
-5.750 0.0186 0.02372 0.01549 -0.1301 0.6998 0.0167
-5.500 0.0395 0.02274 0.01436 -0.1292 0.6976 0.0171
-5.250 0.0617 0.02183 0.01330 -0.1284 0.6955 0.0177
-5.000 0.0846 0.02094 0.01226 -0.1277 0.6937 0.0185
-4.750 0.1079 0.02017 0.01137 -0.1270 0.6921 0.0190
-4.500 0.1312 0.01944 0.01050 -0.1263 0.6905 0.0201
-4.250 0.1546 0.01891 0.00996 -0.1259 0.6890 0.0219
-4.000 0.1793 0.01852 0.00949 -0.1256 0.6877 0.0243
-3.750 0.1979 0.01813 0.00912 -0.1242 0.6852 0.0264
-3.500 0.2179 0.01782 0.00880 -0.1231 0.6829 0.0287
-3.250 0.2391 0.01753 0.00846 -0.1221 0.6810 0.0326
-3.000 0.2613 0.01726 0.00818 -0.1213 0.6792 0.0392
-2.750 0.2839 0.01696 0.00786 -0.1206 0.6776 0.0473
-2.500 0.3070 0.01665 0.00758 -0.1200 0.6761 0.0662
-2.250 0.3289 0.01619 0.00734 -0.1194 0.6747 0.1246
-2.000 0.3455 0.01533 0.00713 -0.1180 0.6735 0.3066
-1.750 0.3537 0.01453 0.00716 -0.1147 0.6715 0.5301
-1.500 0.3628 0.01444 0.00771 -0.1107 0.6689 0.6928
-1.250 0.3812 0.01469 0.00801 -0.1086 0.6668 0.7517
-1.000 0.3997 0.01497 0.00830 -0.1064 0.6649 0.7920
-0.750 0.4168 0.01527 0.00861 -0.1037 0.6632 0.8271
-0.500 0.4361 0.01544 0.00874 -0.1016 0.6618 0.8489
-0.250 0.4602 0.01551 0.00874 -0.1008 0.6605 0.8593
0.000 0.4864 0.01553 0.00865 -0.1007 0.6593 0.8659
0.250 0.5148 0.01553 0.00855 -0.1009 0.6582 0.8706
0.500 0.5288 0.01578 0.00881 -0.0987 0.6555 0.8769
0.750 0.5443 0.01603 0.00907 -0.0967 0.6530 0.8820
1.000 0.5635 0.01622 0.00923 -0.0955 0.6509 0.8869
1.250 0.5842 0.01636 0.00934 -0.0945 0.6490 0.8922
1.500 0.6081 0.01645 0.00939 -0.0941 0.6475 0.8966
1.750 0.6347 0.01649 0.00939 -0.0942 0.6461 0.9009
2.000 0.6628 0.01652 0.00936 -0.0946 0.6449 0.9052
2.250 0.6917 0.01654 0.00933 -0.0951 0.6438 0.9095
2.500 0.7204 0.01665 0.00943 -0.0957 0.6427 0.9132
2.750 0.7171 0.01747 0.01037 -0.0909 0.6383 0.9222
3.000 0.7372 0.01786 0.01080 -0.0903 0.6356 0.9279
3.250 0.7644 0.01806 0.01100 -0.0909 0.6336 0.9329
3.500 0.7928 0.01820 0.01115 -0.0916 0.6321 0.9383
3.750 0.8270 0.01833 0.01128 -0.0934 0.6310 0.9425
4.000 0.8621 0.01844 0.01139 -0.0955 0.6300 0.9467
4.250 0.8987 0.01850 0.01147 -0.0977 0.6291 0.9513
4.750 0.9326 0.02061 0.01379 -0.0977 0.6206 1.0000
5.000 0.9497 0.02101 0.01420 -0.0966 0.6181 1.0000
5.250 0.9769 0.02108 0.01430 -0.0970 0.6166 1.0000
5.500 1.0063 0.02111 0.01434 -0.0977 0.6154 1.0000
5.750 1.0386 0.02105 0.01429 -0.0989 0.6144 1.0000
6.000 1.0730 0.02096 0.01423 -0.1004 0.6136 1.0000
6.500 1.0483 0.02451 0.01789 -0.0910 0.6004 1.0000
6.750 1.0832 0.02415 0.01758 -0.0922 0.5995 1.0000
7.000 1.1195 0.02375 0.01722 -0.0936 0.5988 1.0000
7.500 1.0948 0.02852 0.02214 -0.0862 0.5822 1.0000
7.750 1.1420 0.02714 0.02080 -0.0884 0.5833 1.0000
8.250 1.1409 0.03078 0.02458 -0.0839 0.5678 1.0000
8.500 1.1898 0.02910 0.02297 -0.0860 0.5691 1.0000
9.000 1.1972 0.03221 0.02623 -0.0825 0.5539 1.0000
9.500 1.2147 0.03468 0.02886 -0.0800 0.5390 1.0000
9.750 1.2080 0.03720 0.03146 -0.0777 0.5270 1.0000
10.750 1.2490 0.04197 0.03653 -0.0737 0.4858 1.0000
11.000 1.2695 0.04219 0.03681 -0.0733 0.4720 1.0000
11.250 1.3046 0.04081 0.03538 -0.0737 0.4489 1.0000
11.500 1.3392 0.03929 0.03359 -0.0736 0.4098 1.0000
11.750 1.3476 0.04034 0.03443 -0.0720 0.3754 1.0000
12.000 1.3462 0.04243 0.03633 -0.0701 0.3447 1.0000
12.500 1.3345 0.04783 0.04141 -0.0660 0.2859 1.0000
12.750 1.3279 0.05076 0.04420 -0.0643 0.2582 1.0000
13.000 1.3247 0.05348 0.04684 -0.0628 0.2350 1.0000
13.250 1.3185 0.05657 0.04980 -0.0613 0.2081 1.0000
13.500 1.3142 0.05953 0.05265 -0.0601 0.1856 1.0000
13.750 1.3113 0.06240 0.05542 -0.0590 0.1630 1.0000
14.000 1.3073 0.06545 0.05837 -0.0579 0.1415 1.0000
14.250 1.3062 0.06825 0.06112 -0.0570 0.1215 1.0000
14.500 1.3053 0.07108 0.06389 -0.0562 0.1049 1.0000
14.750 1.3030 0.07407 0.06680 -0.0555 0.0885 1.0000
15.000 1.3034 0.07684 0.06954 -0.0549 0.0765 1.0000
15.500 1.3048 0.08242 0.07511 -0.0540 0.0566 1.0000
15.750 1.3063 0.08516 0.07787 -0.0536 0.0496 1.0000
16.000 1.3057 0.08820 0.08093 -0.0533 0.0435 1.0000
16.250 1.3085 0.09084 0.08362 -0.0532 0.0385 1.0000
16.500 1.3084 0.09389 0.08672 -0.0530 0.0359 1.0000
16.750 1.3121 0.09651 0.08944 -0.0530 0.0327 1.0000
17.000 1.3134 0.09944 0.09242 -0.0531 0.0296 1.0000
17.250 1.3135 0.10256 0.09560 -0.0532 0.0272 1.0000
17.500 1.3160 0.10539 0.09856 -0.0534 0.0253 1.0000
17.750 1.3169 0.10845 0.10169 -0.0537 0.0232 1.0000
18.000 1.3155 0.11185 0.10515 -0.0541 0.0215 1.0000
18.250 1.3170 0.11488 0.10832 -0.0545 0.0202 1.0000
18.500 1.3183 0.11798 0.11153 -0.0551 0.0182 1.0000
18.750 1.3164 0.12157 0.11518 -0.0558 0.0170 1.0000
19.000 1.3170 0.12483 0.11856 -0.0566 0.0157 1.0000
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