WORTMANN FX 73-170 A (fx73170a-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
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Airfoil: WORTMANN FX 73-170 A (fx73170a-il) Reynolds number: 1,000,000 Max Cl/Cd: 151.72 at α=7.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx73170a-il-1000000.txt Download as CSV file: xf-fx73170a-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: FX 73-170 A
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
------ -------- --------- --------- -------- -------- --------
-11.250 0.0011 0.09199 0.08884 -0.1272 0.7144 0.0114
-11.000 0.0033 0.08854 0.08539 -0.1287 0.7125 0.0119
-10.750 0.0094 0.08440 0.08123 -0.1320 0.7103 0.0118
-10.500 0.0196 0.08185 0.07867 -0.1341 0.7085 0.0120
-10.250 0.0239 0.07816 0.07501 -0.1366 0.7069 0.0121
-10.000 0.0264 0.07370 0.07056 -0.1399 0.7052 0.0120
-9.750 0.0332 0.07086 0.06773 -0.1420 0.7030 0.0125
-9.500 0.0348 0.06626 0.06314 -0.1459 0.7011 0.0125
-9.250 0.0364 0.06147 0.05836 -0.1505 0.6992 0.0130
-9.000 0.0240 0.05295 0.04982 -0.1608 0.6970 0.0127
-8.750 0.0049 0.04718 0.04393 -0.1644 0.6945 0.0125
-8.500 -0.0142 0.04388 0.04056 -0.1621 0.6925 0.0125
-8.250 -0.0232 0.04095 0.03754 -0.1600 0.6907 0.0128
-8.000 -0.0290 0.03790 0.03435 -0.1576 0.6887 0.0133
-7.750 -0.1300 0.01944 0.01431 -0.1409 0.6868 0.0094
-7.500 -0.1034 0.02013 0.01510 -0.1411 0.6849 0.0100
-7.250 -0.0899 0.01826 0.01291 -0.1390 0.6828 0.0103
-7.000 -0.0717 0.01696 0.01138 -0.1377 0.6805 0.0104
-6.750 -0.0514 0.01583 0.01005 -0.1366 0.6786 0.0105
-6.500 -0.0302 0.01482 0.00890 -0.1357 0.6772 0.0106
-6.250 -0.0062 0.01447 0.00846 -0.1352 0.6755 0.0111
-6.000 0.0169 0.01386 0.00776 -0.1345 0.6737 0.0112
-5.750 0.0400 0.01324 0.00705 -0.1339 0.6720 0.0113
-5.500 0.0607 0.01237 0.00610 -0.1328 0.6703 0.0116
-5.250 0.0828 0.01188 0.00558 -0.1320 0.6686 0.0123
-5.000 0.1072 0.01165 0.00531 -0.1316 0.6667 0.0130
-4.750 0.1310 0.01134 0.00494 -0.1311 0.6644 0.0135
-4.500 0.1547 0.01104 0.00462 -0.1305 0.6631 0.0141
-4.250 0.1795 0.01084 0.00439 -0.1301 0.6616 0.0146
-4.000 0.2006 0.01034 0.00386 -0.1290 0.6600 0.0159
-3.750 0.2253 0.01014 0.00365 -0.1286 0.6585 0.0168
-3.500 0.2504 0.00997 0.00346 -0.1282 0.6569 0.0183
-3.250 0.2746 0.00975 0.00322 -0.1277 0.6553 0.0209
-3.000 0.3001 0.00963 0.00308 -0.1275 0.6538 0.0232
-2.750 0.3249 0.00945 0.00289 -0.1270 0.6521 0.0288
-2.500 0.3498 0.00929 0.00276 -0.1267 0.6502 0.0419
-2.250 0.3740 0.00911 0.00266 -0.1262 0.6488 0.0684
-2.000 0.3956 0.00878 0.00257 -0.1253 0.6475 0.1362
-1.500 0.4260 0.00758 0.00238 -0.1212 0.6444 0.4604
-1.250 0.4381 0.00704 0.00234 -0.1182 0.6429 0.6261
-1.000 0.4564 0.00686 0.00241 -0.1163 0.6414 0.7150
-0.750 0.4800 0.00689 0.00248 -0.1154 0.6400 0.7538
-0.500 0.5056 0.00695 0.00252 -0.1151 0.6386 0.7696
-0.250 0.5315 0.00704 0.00259 -0.1148 0.6370 0.7828
0.000 0.5574 0.00719 0.00272 -0.1145 0.6351 0.7981
0.250 0.5813 0.00726 0.00282 -0.1137 0.6339 0.8103
0.500 0.6056 0.00733 0.00288 -0.1131 0.6326 0.8182
0.750 0.6312 0.00736 0.00294 -0.1128 0.6313 0.8246
1.000 0.6566 0.00743 0.00300 -0.1125 0.6299 0.8309
1.250 0.6821 0.00748 0.00304 -0.1122 0.6285 0.8347
1.500 0.7088 0.00750 0.00305 -0.1122 0.6271 0.8376
1.750 0.7358 0.00753 0.00307 -0.1123 0.6257 0.8400
2.000 0.7624 0.00757 0.00310 -0.1124 0.6242 0.8426
2.250 0.7897 0.00763 0.00315 -0.1126 0.6227 0.8451
2.500 0.8179 0.00774 0.00322 -0.1130 0.6211 0.8475
2.750 0.8448 0.00784 0.00331 -0.1132 0.6197 0.8498
3.000 0.8701 0.00786 0.00336 -0.1130 0.6186 0.8523
3.250 0.8958 0.00789 0.00342 -0.1128 0.6173 0.8547
3.500 0.9214 0.00793 0.00348 -0.1127 0.6158 0.8573
3.750 0.9472 0.00797 0.00356 -0.1126 0.6143 0.8599
4.000 0.9732 0.00803 0.00362 -0.1126 0.6128 0.8626
4.250 0.9990 0.00809 0.00368 -0.1126 0.6113 0.8649
4.500 1.0258 0.00813 0.00375 -0.1127 0.6097 0.8673
4.750 1.0542 0.00820 0.00383 -0.1133 0.6082 0.8695
5.000 1.0843 0.00833 0.00394 -0.1142 0.6060 0.8716
5.250 1.1083 0.00837 0.00404 -0.1139 0.6040 0.8743
5.500 1.1312 0.00840 0.00412 -0.1132 0.6016 0.8769
5.750 1.1556 0.00844 0.00420 -0.1130 0.5991 0.8794
6.000 1.1804 0.00847 0.00425 -0.1128 0.5963 0.8819
6.250 1.2091 0.00852 0.00432 -0.1135 0.5932 0.8846
6.500 1.2380 0.00862 0.00444 -0.1142 0.5900 0.8870
6.750 1.2599 0.00865 0.00456 -0.1135 0.5866 0.8903
7.000 1.2857 0.00872 0.00468 -0.1137 0.5832 0.8934
7.500 1.3413 0.00893 0.00497 -0.1150 0.5721 0.9001
7.750 1.3715 0.00904 0.00515 -0.1163 0.5667 0.9035
8.000 1.3996 0.00923 0.00537 -0.1172 0.5586 0.9074
8.500 1.4594 0.00967 0.00592 -0.1200 0.5398 0.9160
8.750 1.4874 0.00999 0.00627 -0.1212 0.5298 0.9222
9.000 1.5108 0.01045 0.00677 -0.1216 0.5142 0.9323
9.250 1.5301 0.01137 0.00767 -0.1221 0.4871 0.9582
9.500 1.5339 0.01300 0.00920 -0.1199 0.4567 1.0000
9.750 1.5068 0.01612 0.01207 -0.1136 0.4081 1.0000
10.000 1.4950 0.01857 0.01439 -0.1097 0.3794 1.0000
10.250 1.4734 0.02172 0.01736 -0.1047 0.3432 1.0000
10.500 1.4744 0.02349 0.01910 -0.1024 0.3281 1.0000
10.750 1.4488 0.02711 0.02250 -0.0975 0.2865 1.0000
11.000 1.4341 0.03017 0.02538 -0.0940 0.2543 1.0000
11.250 1.4331 0.03229 0.02743 -0.0919 0.2360 1.0000
11.500 1.4239 0.03510 0.03009 -0.0891 0.2069 1.0000
11.750 1.4147 0.03799 0.03282 -0.0865 0.1766 1.0000
12.250 1.4094 0.04288 0.03747 -0.0826 0.1310 1.0000
12.500 1.4049 0.04555 0.04002 -0.0807 0.1076 1.0000
12.750 1.4074 0.04765 0.04204 -0.0794 0.0922 1.0000
13.000 1.4064 0.05012 0.04441 -0.0778 0.0751 1.0000
13.250 1.4091 0.05228 0.04650 -0.0766 0.0616 1.0000
13.500 1.4118 0.05449 0.04867 -0.0755 0.0510 1.0000
13.750 1.4149 0.05666 0.05078 -0.0744 0.0410 1.0000
14.000 1.4203 0.05866 0.05278 -0.0735 0.0357 1.0000
14.250 1.4271 0.06057 0.05471 -0.0728 0.0319 1.0000
14.500 1.4337 0.06248 0.05663 -0.0721 0.0287 1.0000
14.750 1.4408 0.06440 0.05856 -0.0715 0.0260 1.0000
15.000 1.4476 0.06634 0.06055 -0.0709 0.0241 1.0000
15.250 1.4536 0.06835 0.06257 -0.0703 0.0220 1.0000
15.500 1.4602 0.07034 0.06461 -0.0697 0.0208 1.0000
15.750 1.4676 0.07229 0.06660 -0.0693 0.0191 1.0000
16.000 1.4726 0.07447 0.06880 -0.0688 0.0169 1.0000
16.250 1.4793 0.07650 0.07088 -0.0684 0.0155 1.0000
16.500 1.4849 0.07869 0.07310 -0.0680 0.0140 1.0000
16.750 1.4889 0.08100 0.07544 -0.0676 0.0118 1.0000
17.000 1.4907 0.08362 0.07807 -0.0671 0.0099 1.0000
17.250 1.4947 0.08603 0.08053 -0.0668 0.0088 1.0000
17.500 1.4966 0.08868 0.08322 -0.0665 0.0079 1.0000
17.750 1.4961 0.09169 0.08629 -0.0661 0.0072 1.0000
18.000 1.5021 0.09389 0.08856 -0.0661 0.0067 1.0000
18.250 1.5030 0.09677 0.09151 -0.0659 0.0062 1.0000
18.500 1.5041 0.09961 0.09441 -0.0659 0.0060 1.0000
18.750 1.5013 0.10299 0.09785 -0.0658 0.0055 1.0000
19.000 1.5007 0.10612 0.10107 -0.0659 0.0052 1.0000
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