WORTMANN FX 73-170 (fx73170-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: WORTMANN FX 73-170 (fx73170-il) Reynolds number: 1,000,000 Max Cl/Cd: 151.52 at α=6.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx73170-il-1000000.txt Download as CSV file: xf-fx73170-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 73-170
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
------ -------- --------- --------- -------- -------- --------
-12.250 -0.1270 0.09603 0.09299 -0.1180 0.7490 0.0149
-12.000 -0.3834 0.03800 0.03409 -0.1523 0.7493 0.0091
-11.750 -0.3786 0.03574 0.03171 -0.1538 0.7481 0.0090
-11.500 -0.4008 0.03051 0.02614 -0.1553 0.7468 0.0092
-11.250 -0.3820 0.02995 0.02553 -0.1559 0.7454 0.0089
-11.000 -0.3972 0.02543 0.02063 -0.1556 0.7437 0.0092
-10.750 -0.3880 0.02386 0.01890 -0.1551 0.7420 0.0092
-10.500 -0.3792 0.02252 0.01746 -0.1542 0.7403 0.0094
-10.250 -0.3677 0.02214 0.01705 -0.1527 0.7388 0.0097
-10.000 -0.3554 0.02093 0.01568 -0.1514 0.7372 0.0098
-9.750 -0.3384 0.02020 0.01486 -0.1507 0.7356 0.0100
-9.500 -0.3202 0.01929 0.01382 -0.1501 0.7338 0.0102
-9.250 -0.3017 0.01865 0.01310 -0.1492 0.7327 0.0104
-9.000 -0.2836 0.01779 0.01215 -0.1482 0.7316 0.0107
-8.750 -0.2643 0.01706 0.01134 -0.1474 0.7304 0.0110
-8.500 -0.2444 0.01640 0.01061 -0.1466 0.7289 0.0111
-8.250 -0.2226 0.01600 0.01015 -0.1460 0.7274 0.0114
-8.000 -0.2021 0.01536 0.00944 -0.1452 0.7260 0.0115
-7.750 -0.1815 0.01475 0.00875 -0.1444 0.7247 0.0118
-7.500 -0.1638 0.01392 0.00787 -0.1432 0.7233 0.0121
-7.250 -0.1429 0.01341 0.00734 -0.1425 0.7221 0.0128
-7.000 -0.1198 0.01308 0.00697 -0.1421 0.7207 0.0131
-6.750 -0.0964 0.01274 0.00659 -0.1418 0.7191 0.0137
-6.500 -0.0716 0.01253 0.00635 -0.1416 0.7177 0.0144
-6.250 -0.0479 0.01223 0.00602 -0.1412 0.7167 0.0149
-6.000 -0.0273 0.01165 0.00542 -0.1404 0.7154 0.0160
-5.750 -0.0033 0.01134 0.00510 -0.1400 0.7141 0.0170
-5.500 0.0218 0.01110 0.00485 -0.1398 0.7128 0.0181
-5.250 0.0467 0.01082 0.00454 -0.1396 0.7115 0.0193
-5.000 0.0714 0.01052 0.00422 -0.1394 0.7102 0.0215
-4.750 0.0977 0.01034 0.00402 -0.1393 0.7090 0.0234
-4.500 0.1231 0.01008 0.00377 -0.1392 0.7077 0.0277
-4.250 0.1489 0.00985 0.00355 -0.1391 0.7064 0.0349
-4.000 0.1741 0.00957 0.00334 -0.1390 0.7050 0.0572
-3.750 0.1990 0.00928 0.00320 -0.1389 0.7031 0.1037
-3.500 0.2208 0.00876 0.00300 -0.1383 0.7022 0.1913
-3.250 0.2402 0.00807 0.00276 -0.1374 0.7011 0.3222
-3.000 0.2558 0.00721 0.00248 -0.1357 0.6998 0.4974
-2.750 0.2799 0.00708 0.00256 -0.1351 0.6985 0.5792
-2.500 0.3078 0.00712 0.00259 -0.1352 0.6972 0.5983
-2.250 0.3358 0.00720 0.00265 -0.1353 0.6958 0.6123
-2.000 0.3640 0.00728 0.00271 -0.1354 0.6944 0.6222
-1.750 0.3924 0.00740 0.00280 -0.1356 0.6931 0.6309
-1.500 0.4207 0.00751 0.00291 -0.1357 0.6919 0.6387
-1.250 0.4493 0.00766 0.00304 -0.1360 0.6907 0.6452
-1.000 0.4781 0.00781 0.00312 -0.1363 0.6893 0.6491
-0.750 0.5066 0.00787 0.00320 -0.1366 0.6877 0.6532
-0.500 0.5339 0.00792 0.00327 -0.1366 0.6867 0.6564
-0.250 0.5612 0.00795 0.00331 -0.1367 0.6854 0.6589
0.000 0.5887 0.00798 0.00333 -0.1368 0.6840 0.6609
0.250 0.6164 0.00800 0.00334 -0.1370 0.6827 0.6624
0.500 0.6441 0.00802 0.00334 -0.1372 0.6812 0.6635
0.750 0.6720 0.00803 0.00333 -0.1374 0.6798 0.6644
1.000 0.7001 0.00804 0.00332 -0.1377 0.6783 0.6650
1.250 0.7279 0.00801 0.00329 -0.1379 0.6770 0.6661
1.500 0.7558 0.00801 0.00329 -0.1382 0.6757 0.6674
1.750 0.7846 0.00807 0.00333 -0.1386 0.6740 0.6684
2.000 0.8120 0.00812 0.00340 -0.1388 0.6725 0.6693
2.250 0.8381 0.00812 0.00343 -0.1387 0.6711 0.6702
2.500 0.8645 0.00813 0.00347 -0.1386 0.6695 0.6711
2.750 0.8912 0.00814 0.00352 -0.1386 0.6678 0.6720
3.000 0.9182 0.00816 0.00355 -0.1387 0.6661 0.6730
3.250 0.9453 0.00816 0.00356 -0.1388 0.6641 0.6741
3.500 0.9725 0.00815 0.00356 -0.1388 0.6619 0.6752
3.750 1.0006 0.00820 0.00359 -0.1392 0.6593 0.6763
4.000 1.0251 0.00820 0.00363 -0.1387 0.6564 0.6772
4.250 1.0491 0.00818 0.00365 -0.1381 0.6533 0.6782
4.500 1.0739 0.00815 0.00364 -0.1376 0.6498 0.6791
4.750 1.0991 0.00813 0.00361 -0.1372 0.6454 0.6799
5.000 1.1233 0.00816 0.00366 -0.1367 0.6418 0.6807
5.250 1.1447 0.00812 0.00368 -0.1356 0.6368 0.6817
5.500 1.1681 0.00810 0.00369 -0.1349 0.6327 0.6829
5.750 1.1884 0.00810 0.00371 -0.1335 0.6255 0.6841
6.000 1.2068 0.00810 0.00373 -0.1317 0.6168 0.6854
6.250 1.2247 0.00814 0.00380 -0.1298 0.6070 0.6867
6.500 1.2408 0.00823 0.00388 -0.1276 0.5995 0.6878
6.750 1.2561 0.00829 0.00399 -0.1252 0.5899 0.6890
7.000 1.2711 0.00843 0.00414 -0.1228 0.5810 0.6902
7.250 1.2819 0.00866 0.00435 -0.1195 0.5655 0.6915
7.500 1.2925 0.00894 0.00461 -0.1163 0.5513 0.6927
7.750 1.2926 0.00947 0.00505 -0.1112 0.5266 0.6940
8.000 1.2890 0.01024 0.00571 -0.1058 0.4976 0.6953
8.250 1.2793 0.01151 0.00682 -0.1001 0.4629 0.6964
8.500 1.2677 0.01345 0.00857 -0.0953 0.4205 0.6976
8.750 1.2595 0.01580 0.01072 -0.0920 0.3743 0.6993
9.000 1.2548 0.01809 0.01281 -0.0894 0.3308 0.7007
9.250 1.2524 0.02024 0.01478 -0.0871 0.2914 0.7023
9.500 1.2534 0.02217 0.01655 -0.0851 0.2571 0.7037
9.750 1.2534 0.02415 0.01835 -0.0830 0.2227 0.7052
10.000 1.2550 0.02605 0.02008 -0.0812 0.1904 0.7066
10.250 1.2600 0.02779 0.02170 -0.0798 0.1635 0.7081
10.500 1.2653 0.02951 0.02329 -0.0784 0.1372 0.7094
10.750 1.2701 0.03129 0.02494 -0.0769 0.1126 0.7108
11.000 1.2764 0.03298 0.02651 -0.0756 0.0919 0.7120
11.250 1.2859 0.03456 0.02802 -0.0749 0.0765 0.7134
11.500 1.2967 0.03618 0.02959 -0.0744 0.0617 0.7153
11.750 1.3087 0.03769 0.03106 -0.0740 0.0523 0.7171
12.000 1.3203 0.03921 0.03257 -0.0735 0.0449 0.7189
12.250 1.3319 0.04068 0.03404 -0.0730 0.0399 0.7207
12.500 1.3454 0.04201 0.03540 -0.0726 0.0362 0.7226
12.750 1.3571 0.04352 0.03693 -0.0722 0.0330 0.7245
13.000 1.3679 0.04507 0.03849 -0.0716 0.0301 0.7265
13.250 1.3820 0.04633 0.03981 -0.0712 0.0286 0.7283
13.500 1.3950 0.04800 0.04149 -0.0713 0.0263 0.7308
13.750 1.4049 0.04978 0.04333 -0.0709 0.0241 0.7332
14.000 1.4198 0.05111 0.04472 -0.0709 0.0230 0.7359
14.250 1.4309 0.05275 0.04641 -0.0705 0.0217 0.7390
14.500 1.4391 0.05459 0.04828 -0.0700 0.0202 0.7420
14.750 1.4482 0.05639 0.05014 -0.0695 0.0189 0.7448
15.000 1.4607 0.05808 0.05191 -0.0695 0.0181 0.7486
15.250 1.4709 0.05987 0.05375 -0.0693 0.0169 0.7526
15.500 1.4791 0.06179 0.05570 -0.0689 0.0158 0.7567
15.750 1.4851 0.06401 0.05800 -0.0685 0.0148 0.7611
16.000 1.4963 0.06583 0.05992 -0.0686 0.0141 0.7670
16.250 1.5052 0.06784 0.06198 -0.0684 0.0131 0.7737
16.500 1.5104 0.07034 0.06456 -0.0684 0.0122 0.7818
16.750 1.5155 0.07291 0.06723 -0.0683 0.0116 0.7928
17.000 1.5261 0.07518 0.06965 -0.0690 0.0111 0.8130
17.250 1.5460 0.07802 0.07281 -0.0721 0.0103 0.9031
17.500 1.5599 0.08135 0.07622 -0.0741 0.0097 1.0000
17.750 1.5577 0.08457 0.07950 -0.0737 0.0091 1.0000
18.000 1.5612 0.08714 0.08215 -0.0735 0.0087 1.0000
18.250 1.5638 0.08984 0.08492 -0.0733 0.0084 1.0000
18.500 1.5650 0.09275 0.08791 -0.0733 0.0081 1.0000
18.750 1.5676 0.09545 0.09067 -0.0732 0.0076 1.0000
19.000 1.5665 0.09868 0.09397 -0.0733 0.0073 1.0000
19.250 1.5627 0.10233 0.09770 -0.0735 0.0071 1.0000
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