WORTMANN FX 73-170 (fx73170-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 73-170 (fx73170-il) Reynolds number: 1,000,000 Max Cl/Cd: 147.35 at α=5.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx73170-il-1000000-n5.txt Download as CSV file: xf-fx73170-il-1000000-n5.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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-15.250 -0.5449 0.06863 0.06522 -0.1140 0.7411 0.0055
-15.000 -0.5322 0.06581 0.06236 -0.1169 0.7397 0.0055
-14.750 -0.5931 0.04989 0.04606 -0.1296 0.7388 0.0055
-14.500 -0.5938 0.04608 0.04215 -0.1329 0.7379 0.0056
-14.250 -0.6117 0.04052 0.03635 -0.1366 0.7368 0.0055
-14.000 -0.6037 0.03838 0.03415 -0.1384 0.7353 0.0056
-13.750 -0.6029 0.03549 0.03111 -0.1403 0.7338 0.0056
-13.500 -0.6067 0.03224 0.02765 -0.1418 0.7322 0.0055
-13.250 -0.5975 0.03040 0.02572 -0.1429 0.7304 0.0057
-13.000 -0.5846 0.02896 0.02420 -0.1439 0.7290 0.0057
-12.750 -0.5716 0.02756 0.02268 -0.1446 0.7276 0.0056
-12.500 -0.5630 0.02573 0.02071 -0.1452 0.7261 0.0059
-12.250 -0.5454 0.02481 0.01972 -0.1457 0.7246 0.0059
-12.000 -0.5262 0.02408 0.01893 -0.1463 0.7232 0.0060
-11.750 -0.5147 0.02266 0.01740 -0.1463 0.7221 0.0061
-11.500 -0.5021 0.02141 0.01603 -0.1461 0.7209 0.0059
-11.250 -0.4843 0.02069 0.01527 -0.1460 0.7194 0.0063
-11.000 -0.4707 0.01969 0.01418 -0.1455 0.7178 0.0061
-10.750 -0.4560 0.01892 0.01335 -0.1448 0.7162 0.0064
-10.500 -0.4447 0.01816 0.01250 -0.1434 0.7146 0.0065
-10.250 -0.4277 0.01762 0.01189 -0.1426 0.7132 0.0067
-10.000 -0.4111 0.01693 0.01111 -0.1416 0.7119 0.0068
-9.750 -0.3925 0.01637 0.01048 -0.1409 0.7105 0.0068
-9.500 -0.3723 0.01590 0.00994 -0.1403 0.7091 0.0071
-9.250 -0.3514 0.01546 0.00943 -0.1398 0.7078 0.0072
-9.000 -0.3293 0.01508 0.00901 -0.1394 0.7067 0.0074
-8.750 -0.3089 0.01453 0.00840 -0.1387 0.7053 0.0074
-8.500 -0.2886 0.01395 0.00778 -0.1381 0.7040 0.0076
-8.250 -0.2665 0.01351 0.00730 -0.1377 0.7026 0.0078
-8.000 -0.2435 0.01312 0.00689 -0.1373 0.7013 0.0081
-7.750 -0.2195 0.01282 0.00656 -0.1371 0.7000 0.0084
-7.500 -0.1952 0.01252 0.00622 -0.1369 0.6987 0.0088
-7.250 -0.1708 0.01222 0.00589 -0.1367 0.6975 0.0090
-7.000 -0.1462 0.01193 0.00556 -0.1365 0.6962 0.0093
-6.750 -0.1213 0.01166 0.00525 -0.1364 0.6948 0.0096
-6.500 -0.0959 0.01144 0.00498 -0.1363 0.6934 0.0100
-6.250 -0.0706 0.01115 0.00468 -0.1362 0.6922 0.0103
-6.000 -0.0452 0.01086 0.00438 -0.1362 0.6910 0.0111
-5.750 -0.0189 0.01067 0.00419 -0.1363 0.6898 0.0120
-5.500 0.0076 0.01047 0.00397 -0.1363 0.6886 0.0130
-5.250 0.0339 0.01025 0.00375 -0.1364 0.6874 0.0139
-5.000 0.0604 0.01005 0.00355 -0.1364 0.6862 0.0150
-4.750 0.0872 0.00989 0.00336 -0.1365 0.6848 0.0163
-4.500 0.1139 0.00971 0.00318 -0.1366 0.6835 0.0186
-4.250 0.1406 0.00955 0.00302 -0.1367 0.6821 0.0221
-4.000 0.1673 0.00938 0.00287 -0.1368 0.6807 0.0283
-3.750 0.1940 0.00921 0.00273 -0.1369 0.6793 0.0381
-3.500 0.2208 0.00907 0.00261 -0.1370 0.6780 0.0510
-3.250 0.2473 0.00884 0.00248 -0.1371 0.6770 0.0763
-3.000 0.2731 0.00854 0.00234 -0.1371 0.6759 0.1226
-2.750 0.2986 0.00823 0.00221 -0.1371 0.6746 0.1809
-2.500 0.3228 0.00779 0.00206 -0.1369 0.6732 0.2689
-2.250 0.3458 0.00730 0.00189 -0.1366 0.6718 0.3759
-2.000 0.3641 0.00660 0.00178 -0.1352 0.6702 0.5656
-1.750 0.3919 0.00662 0.00181 -0.1354 0.6688 0.5861
-1.500 0.4199 0.00668 0.00187 -0.1355 0.6675 0.6043
-1.250 0.4482 0.00674 0.00189 -0.1357 0.6662 0.6136
-1.000 0.4761 0.00680 0.00195 -0.1359 0.6649 0.6211
-0.750 0.5043 0.00688 0.00199 -0.1361 0.6635 0.6263
-0.500 0.5325 0.00693 0.00202 -0.1363 0.6622 0.6299
-0.250 0.5605 0.00694 0.00203 -0.1365 0.6609 0.6322
0.000 0.5885 0.00695 0.00205 -0.1368 0.6595 0.6339
0.250 0.6165 0.00697 0.00207 -0.1370 0.6581 0.6349
0.500 0.6445 0.00699 0.00209 -0.1372 0.6567 0.6359
0.750 0.6723 0.00701 0.00210 -0.1374 0.6551 0.6368
1.000 0.7000 0.00703 0.00212 -0.1376 0.6535 0.6377
1.250 0.7276 0.00706 0.00214 -0.1377 0.6520 0.6386
1.500 0.7552 0.00710 0.00217 -0.1379 0.6504 0.6395
1.750 0.7827 0.00715 0.00220 -0.1381 0.6488 0.6405
2.000 0.8103 0.00718 0.00225 -0.1382 0.6474 0.6416
2.250 0.8377 0.00721 0.00230 -0.1384 0.6459 0.6426
2.500 0.8651 0.00724 0.00235 -0.1385 0.6443 0.6434
2.750 0.8923 0.00727 0.00240 -0.1386 0.6423 0.6443
3.000 0.9193 0.00731 0.00246 -0.1387 0.6403 0.6450
3.250 0.9460 0.00735 0.00251 -0.1387 0.6381 0.6457
3.500 0.9722 0.00740 0.00255 -0.1386 0.6353 0.6464
3.750 0.9982 0.00744 0.00261 -0.1384 0.6321 0.6472
4.000 1.0237 0.00746 0.00267 -0.1381 0.6271 0.6482
4.250 1.0488 0.00750 0.00273 -0.1378 0.6230 0.6492
4.500 1.0730 0.00756 0.00280 -0.1373 0.6183 0.6504
4.750 1.0977 0.00760 0.00289 -0.1369 0.6120 0.6514
5.000 1.1205 0.00768 0.00297 -0.1361 0.6056 0.6524
5.250 1.1434 0.00776 0.00307 -0.1353 0.5971 0.6533
5.500 1.1623 0.00789 0.00318 -0.1337 0.5835 0.6543
5.750 1.1783 0.00808 0.00333 -0.1315 0.5667 0.6553
6.000 1.1845 0.00837 0.00353 -0.1272 0.5439 0.6563
6.250 1.1824 0.00888 0.00390 -0.1214 0.5105 0.6573
6.500 1.1771 0.00960 0.00446 -0.1153 0.4761 0.6585
6.750 1.1667 0.01060 0.00528 -0.1086 0.4393 0.6595
7.000 1.1519 0.01209 0.00657 -0.1021 0.3962 0.6606
7.250 1.1481 0.01356 0.00790 -0.0981 0.3631 0.6615
7.500 1.1517 0.01488 0.00911 -0.0955 0.3367 0.6624
7.750 1.1474 0.01678 0.01082 -0.0922 0.2971 0.6634
8.000 1.1494 0.01842 0.01232 -0.0899 0.2636 0.6650
8.250 1.1531 0.02000 0.01376 -0.0878 0.2332 0.6661
8.500 1.1586 0.02148 0.01513 -0.0860 0.2072 0.6672
8.750 1.1643 0.02297 0.01650 -0.0843 0.1802 0.6684
9.000 1.1732 0.02427 0.01772 -0.0829 0.1601 0.6695
9.250 1.1820 0.02559 0.01897 -0.0816 0.1398 0.6707
9.500 1.1887 0.02711 0.02037 -0.0800 0.1167 0.6717
9.750 1.1998 0.02834 0.02155 -0.0790 0.1018 0.6729
10.000 1.2089 0.02974 0.02288 -0.0779 0.0852 0.6740
10.250 1.2220 0.03089 0.02400 -0.0771 0.0754 0.6752
10.500 1.2320 0.03227 0.02532 -0.0760 0.0621 0.6762
10.750 1.2442 0.03351 0.02654 -0.0752 0.0541 0.6773
11.000 1.2560 0.03477 0.02776 -0.0744 0.0463 0.6783
11.250 1.2692 0.03599 0.02899 -0.0738 0.0411 0.6794
11.500 1.2829 0.03726 0.03026 -0.0733 0.0366 0.6807
11.750 1.2970 0.03847 0.03149 -0.0729 0.0333 0.6821
12.000 1.3106 0.03968 0.03273 -0.0724 0.0304 0.6834
12.250 1.3246 0.04092 0.03401 -0.0720 0.0285 0.6850
12.500 1.3374 0.04226 0.03535 -0.0715 0.0259 0.6867
12.750 1.3501 0.04358 0.03670 -0.0710 0.0239 0.6885
13.000 1.3639 0.04484 0.03801 -0.0706 0.0226 0.6899
13.250 1.3754 0.04627 0.03947 -0.0700 0.0209 0.6915
13.500 1.3868 0.04770 0.04092 -0.0694 0.0194 0.6932
13.750 1.3987 0.04909 0.04235 -0.0689 0.0179 0.6945
14.000 1.4102 0.05064 0.04394 -0.0685 0.0166 0.6962
14.250 1.4216 0.05221 0.04555 -0.0682 0.0156 0.6981
14.500 1.4329 0.05378 0.04716 -0.0678 0.0144 0.7000
14.750 1.4437 0.05541 0.04885 -0.0675 0.0135 0.7020
15.000 1.4537 0.05708 0.05058 -0.0671 0.0130 0.7041
15.250 1.4620 0.05889 0.05241 -0.0665 0.0115 0.7060
15.500 1.4714 0.06066 0.05424 -0.0662 0.0108 0.7082
15.750 1.4800 0.06249 0.05612 -0.0657 0.0101 0.7102
16.000 1.4892 0.06435 0.05805 -0.0655 0.0096 0.7125
16.250 1.4969 0.06641 0.06018 -0.0653 0.0092 0.7152
16.500 1.5040 0.06849 0.06232 -0.0650 0.0084 0.7179
16.750 1.5109 0.07060 0.06449 -0.0647 0.0077 0.7207
17.000 1.5166 0.07284 0.06679 -0.0644 0.0073 0.7237
17.500 1.5270 0.07760 0.07169 -0.0642 0.0065 0.7302
17.750 1.5322 0.08004 0.07421 -0.0641 0.0062 0.7345
18.000 1.5368 0.08257 0.07684 -0.0641 0.0059 0.7388
18.250 1.5416 0.08514 0.07949 -0.0642 0.0056 0.7440
18.500 1.5450 0.08790 0.08235 -0.0645 0.0054 0.7495
18.750 1.5473 0.09078 0.08531 -0.0647 0.0050 0.7557
19.000 1.5498 0.09382 0.08845 -0.0652 0.0050 0.7627
19.250 1.5528 0.09686 0.09159 -0.0658 0.0048 0.7716
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