FX 73-K-170/22 (fx73k170-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: FX 73-K-170/22 (fx73k170-il) Reynolds number: 1,000,000 Max Cl/Cd: 137.97 at α=5.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx73k170-il-1000000-n5.txt Download as CSV file: xf-fx73k170-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: FX 73-K-170/22
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
------ -------- --------- --------- -------- -------- --------
-14.500 -0.4783 0.06855 0.06536 -0.1119 0.7711 0.0046
-14.250 -0.4446 0.07006 0.06691 -0.1116 0.7696 0.0050
-14.000 -0.4922 0.05558 0.05214 -0.1230 0.7683 0.0049
-13.750 -0.5064 0.04899 0.04538 -0.1288 0.7669 0.0049
-13.500 -0.5244 0.04266 0.03884 -0.1341 0.7652 0.0047
-13.250 -0.5215 0.03949 0.03553 -0.1371 0.7633 0.0049
-13.000 -0.5139 0.03699 0.03291 -0.1395 0.7620 0.0049
-12.750 -0.5148 0.03359 0.02932 -0.1422 0.7599 0.0049
-12.500 -0.5168 0.03011 0.02561 -0.1445 0.7581 0.0048
-12.250 -0.5035 0.02858 0.02398 -0.1458 0.7565 0.0049
-12.000 -0.4898 0.02715 0.02247 -0.1469 0.7547 0.0050
-11.750 -0.4784 0.02544 0.02064 -0.1478 0.7531 0.0050
-11.500 -0.4706 0.02343 0.01846 -0.1484 0.7512 0.0050
-11.250 -0.4510 0.02275 0.01772 -0.1490 0.7493 0.0051
-11.000 -0.4402 0.02128 0.01611 -0.1489 0.7471 0.0051
-10.750 -0.4242 0.02048 0.01524 -0.1489 0.7455 0.0051
-10.500 -0.4124 0.01961 0.01426 -0.1479 0.7434 0.0052
-10.250 -0.3987 0.01892 0.01349 -0.1468 0.7418 0.0052
-10.000 -0.3838 0.01805 0.01254 -0.1458 0.7403 0.0052
-9.750 -0.3673 0.01727 0.01167 -0.1449 0.7386 0.0052
-9.500 -0.3498 0.01655 0.01087 -0.1441 0.7367 0.0052
-9.250 -0.3326 0.01578 0.01002 -0.1431 0.7347 0.0053
-9.000 -0.3149 0.01503 0.00920 -0.1422 0.7326 0.0055
-8.750 -0.2936 0.01457 0.00868 -0.1417 0.7306 0.0057
-8.500 -0.2728 0.01405 0.00809 -0.1411 0.7287 0.0058
-8.250 -0.2503 0.01362 0.00761 -0.1406 0.7271 0.0059
-8.000 -0.2273 0.01320 0.00716 -0.1403 0.7254 0.0060
-7.750 -0.2039 0.01280 0.00673 -0.1399 0.7236 0.0061
-7.500 -0.1804 0.01240 0.00629 -0.1396 0.7215 0.0063
-7.250 -0.1563 0.01205 0.00590 -0.1393 0.7194 0.0064
-7.000 -0.1320 0.01171 0.00551 -0.1390 0.7171 0.0067
-6.750 -0.1074 0.01141 0.00516 -0.1388 0.7150 0.0069
-6.500 -0.0825 0.01113 0.00483 -0.1386 0.7128 0.0072
-6.250 -0.0568 0.01088 0.00455 -0.1385 0.7110 0.0075
-6.000 -0.0313 0.01057 0.00423 -0.1384 0.7089 0.0079
-5.750 -0.0055 0.01033 0.00397 -0.1383 0.7066 0.0085
-5.500 0.0206 0.01011 0.00373 -0.1382 0.7042 0.0092
-5.250 0.0468 0.00993 0.00351 -0.1382 0.7017 0.0100
-5.000 0.0729 0.00974 0.00330 -0.1381 0.6992 0.0112
-4.750 0.0993 0.00955 0.00310 -0.1381 0.6969 0.0133
-4.500 0.1259 0.00936 0.00293 -0.1381 0.6945 0.0180
-4.250 0.1523 0.00915 0.00276 -0.1381 0.6920 0.0278
-4.000 0.1783 0.00893 0.00260 -0.1380 0.6891 0.0435
-3.750 0.2042 0.00873 0.00244 -0.1380 0.6863 0.0614
-3.500 0.2299 0.00852 0.00230 -0.1378 0.6836 0.0876
-3.250 0.2553 0.00821 0.00215 -0.1377 0.6811 0.1349
-3.000 0.2780 0.00768 0.00196 -0.1373 0.6783 0.2371
-2.750 0.3008 0.00722 0.00179 -0.1368 0.6752 0.3320
-2.500 0.3244 0.00690 0.00167 -0.1363 0.6720 0.4036
-2.250 0.3490 0.00672 0.00159 -0.1359 0.6688 0.4556
-2.000 0.3740 0.00653 0.00159 -0.1355 0.6659 0.5200
-1.750 0.4009 0.00651 0.00161 -0.1355 0.6629 0.5426
-1.500 0.4281 0.00652 0.00162 -0.1355 0.6599 0.5600
-1.250 0.4553 0.00655 0.00162 -0.1355 0.6567 0.5672
-1.000 0.4823 0.00658 0.00163 -0.1354 0.6539 0.5739
-0.750 0.5102 0.00661 0.00164 -0.1356 0.6511 0.5809
-0.500 0.5375 0.00663 0.00166 -0.1356 0.6480 0.5853
-0.250 0.5647 0.00667 0.00168 -0.1356 0.6449 0.5896
0.000 0.5916 0.00672 0.00170 -0.1355 0.6418 0.5940
0.250 0.6186 0.00678 0.00172 -0.1355 0.6391 0.5974
0.500 0.6459 0.00679 0.00175 -0.1356 0.6365 0.6003
0.750 0.6729 0.00683 0.00179 -0.1356 0.6330 0.6034
1.000 0.6996 0.00687 0.00183 -0.1355 0.6297 0.6064
1.250 0.7257 0.00694 0.00187 -0.1353 0.6262 0.6092
1.500 0.7523 0.00700 0.00191 -0.1352 0.6229 0.6116
1.750 0.7792 0.00704 0.00195 -0.1352 0.6195 0.6135
2.000 0.8054 0.00708 0.00201 -0.1351 0.6159 0.6155
2.250 0.8309 0.00714 0.00207 -0.1348 0.6123 0.6177
2.500 0.8563 0.00721 0.00213 -0.1345 0.6085 0.6197
2.750 0.8827 0.00725 0.00220 -0.1344 0.6052 0.6218
3.000 0.9083 0.00732 0.00227 -0.1342 0.6011 0.6238
3.250 0.9332 0.00740 0.00235 -0.1338 0.5972 0.6259
3.500 0.9579 0.00748 0.00243 -0.1333 0.5935 0.6279
3.750 0.9836 0.00754 0.00251 -0.1331 0.5896 0.6294
4.000 1.0079 0.00761 0.00261 -0.1326 0.5850 0.6316
4.250 1.0307 0.00772 0.00271 -0.1318 0.5804 0.6336
4.500 1.0547 0.00779 0.00282 -0.1312 0.5749 0.6357
4.750 1.0774 0.00789 0.00293 -0.1304 0.5689 0.6377
5.000 1.0984 0.00802 0.00306 -0.1293 0.5625 0.6396
5.250 1.1203 0.00812 0.00318 -0.1283 0.5559 0.6417
5.500 1.1362 0.00827 0.00331 -0.1260 0.5466 0.6438
5.750 1.1535 0.00842 0.00346 -0.1241 0.5372 0.6457
6.000 1.1712 0.00860 0.00365 -0.1223 0.5278 0.6476
6.250 1.1839 0.00890 0.00392 -0.1196 0.5119 0.6497
6.500 1.1996 0.00917 0.00418 -0.1175 0.5027 0.6517
6.750 1.2094 0.00960 0.00456 -0.1144 0.4836 0.6542
7.000 1.2106 0.01035 0.00519 -0.1100 0.4550 0.6567
7.250 1.2139 0.01122 0.00594 -0.1064 0.4281 0.6590
7.750 1.2252 0.01336 0.00786 -0.1011 0.3728 0.6633
8.000 1.2248 0.01499 0.00931 -0.0981 0.3326 0.6658
8.250 1.2266 0.01660 0.01074 -0.0956 0.2951 0.6683
8.500 1.2338 0.01795 0.01197 -0.0938 0.2671 0.6715
8.750 1.2433 0.01918 0.01312 -0.0924 0.2458 0.6739
9.000 1.2505 0.02056 0.01439 -0.0907 0.2205 0.6766
9.250 1.2606 0.02184 0.01560 -0.0896 0.1999 0.6791
9.500 1.2610 0.02374 0.01732 -0.0874 0.1641 0.6819
9.750 1.2733 0.02492 0.01847 -0.0865 0.1507 0.6849
10.000 1.2816 0.02637 0.01984 -0.0853 0.1321 0.6882
10.250 1.2829 0.02832 0.02164 -0.0833 0.1035 0.6912
10.500 1.2942 0.02967 0.02296 -0.0825 0.0899 0.6943
10.750 1.3002 0.03147 0.02468 -0.0814 0.0709 0.6980
11.000 1.3020 0.03358 0.02666 -0.0798 0.0478 0.7019
11.250 1.3148 0.03491 0.02801 -0.0793 0.0420 0.7067
11.500 1.3247 0.03653 0.02960 -0.0786 0.0328 0.7106
11.750 1.3365 0.03806 0.03115 -0.0782 0.0278 0.7162
12.000 1.3486 0.03952 0.03263 -0.0777 0.0240 0.7221
12.250 1.3615 0.04103 0.03418 -0.0775 0.0212 0.7281
12.500 1.3746 0.04254 0.03574 -0.0773 0.0191 0.7356
12.750 1.3881 0.04406 0.03732 -0.0772 0.0179 0.7435
13.000 1.4022 0.04564 0.03897 -0.0774 0.0166 0.7536
13.250 1.4163 0.04734 0.04073 -0.0777 0.0142 0.7665
13.500 1.4305 0.04918 0.04266 -0.0783 0.0129 0.7849
13.750 1.4488 0.05101 0.04463 -0.0796 0.0115 0.8171
14.000 1.4841 0.05348 0.04740 -0.0852 0.0094 0.9381
14.250 1.4956 0.05556 0.04952 -0.0850 0.0084 1.0000
14.500 1.5016 0.05761 0.05159 -0.0842 0.0069 1.0000
14.750 1.5091 0.05952 0.05356 -0.0836 0.0067 1.0000
15.000 1.5145 0.06166 0.05573 -0.0829 0.0057 1.0000
15.250 1.5207 0.06376 0.05789 -0.0823 0.0054 1.0000
15.500 1.5255 0.06603 0.06021 -0.0817 0.0047 1.0000
15.750 1.5302 0.06833 0.06256 -0.0811 0.0043 1.0000
16.000 1.5339 0.07078 0.06506 -0.0806 0.0039 1.0000
16.250 1.5379 0.07321 0.06754 -0.0801 0.0037 1.0000
16.500 1.5407 0.07577 0.07018 -0.0797 0.0035 1.0000
16.750 1.5452 0.07819 0.07266 -0.0794 0.0033 1.0000
17.000 1.5474 0.08091 0.07545 -0.0790 0.0032 1.0000
17.250 1.5507 0.08353 0.07814 -0.0789 0.0031 1.0000
17.500 1.5522 0.08637 0.08105 -0.0787 0.0029 1.0000
17.750 1.5531 0.08935 0.08410 -0.0786 0.0028 1.0000
18.000 1.5556 0.09208 0.08690 -0.0785 0.0028 1.0000
18.250 1.5528 0.09556 0.09046 -0.0785 0.0025 1.0000
18.500 1.5528 0.09870 0.09367 -0.0787 0.0025 1.0000
18.750 1.5506 0.10219 0.09725 -0.0789 0.0024 1.0000
19.000 1.5488 0.10566 0.10080 -0.0792 0.0024 1.0000
19.250 1.5456 0.10934 0.10457 -0.0797 0.0023 1.0000
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