WORTMANN FX 75-193 (fx75193-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: WORTMANN FX 75-193 (fx75193-il) Reynolds number: 500,000 Max Cl/Cd: 91.67 at α=6.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx75193-il-500000.txt Download as CSV file: xf-fx75193-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 75-193
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-15.000 -0.2951 0.06903 0.06499 -0.1628 0.8173 0.0142
-14.750 -0.3067 0.06397 0.05976 -0.1666 0.8169 0.0140
-14.500 -0.3286 0.05830 0.05392 -0.1697 0.8165 0.0140
-14.250 -0.3378 0.05415 0.04971 -0.1709 0.8160 0.0137
-14.000 -0.3521 0.05021 0.04562 -0.1721 0.8154 0.0136
-13.750 -0.3662 0.04665 0.04189 -0.1725 0.8146 0.0136
-13.500 -0.3770 0.04347 0.03857 -0.1723 0.8137 0.0133
-13.250 -0.3855 0.04087 0.03578 -0.1716 0.8125 0.0133
-13.000 -0.3927 0.03841 0.03313 -0.1706 0.8116 0.0134
-12.750 -0.3956 0.03630 0.03084 -0.1693 0.8106 0.0134
-12.500 -0.3943 0.03454 0.02892 -0.1681 0.8096 0.0134
-12.250 -0.3907 0.03313 0.02735 -0.1668 0.8086 0.0135
-12.000 -0.3831 0.03166 0.02574 -0.1656 0.8077 0.0135
-11.750 -0.3727 0.03044 0.02440 -0.1645 0.8068 0.0134
-11.500 -0.3626 0.02942 0.02325 -0.1632 0.8058 0.0136
-11.250 -0.3485 0.02842 0.02214 -0.1622 0.8047 0.0136
-11.000 -0.3340 0.02759 0.02121 -0.1611 0.8036 0.0136
-10.750 -0.3202 0.02696 0.02049 -0.1599 0.8025 0.0137
-10.500 -0.3051 0.02634 0.01981 -0.1587 0.8014 0.0137
-10.250 -0.2914 0.02576 0.01918 -0.1572 0.8001 0.0138
-10.000 -0.2770 0.02507 0.01847 -0.1559 0.7987 0.0138
-9.750 -0.2632 0.02445 0.01781 -0.1545 0.7970 0.0139
-9.500 -0.2525 0.02368 0.01704 -0.1526 0.7955 0.0141
-9.250 -0.2433 0.02298 0.01635 -0.1506 0.7941 0.0146
-9.000 -0.2334 0.02238 0.01574 -0.1487 0.7927 0.0148
-8.750 -0.2227 0.02184 0.01519 -0.1468 0.7913 0.0151
-8.500 -0.2119 0.02131 0.01463 -0.1448 0.7900 0.0153
-8.250 -0.2026 0.02074 0.01403 -0.1426 0.7885 0.0155
-8.000 -0.1917 0.02024 0.01351 -0.1406 0.7871 0.0156
-7.750 -0.1814 0.01979 0.01301 -0.1384 0.7857 0.0158
-7.500 -0.1733 0.01952 0.01270 -0.1358 0.7841 0.0160
-7.250 -0.1692 0.01926 0.01243 -0.1325 0.7824 0.0164
-7.000 -0.1674 0.01898 0.01216 -0.1288 0.7804 0.0166
-6.750 -0.1598 0.01868 0.01185 -0.1262 0.7782 0.0170
-6.500 -0.1478 0.01831 0.01147 -0.1244 0.7761 0.0183
-6.250 -0.1308 0.01795 0.01112 -0.1234 0.7742 0.0204
-6.000 -0.1117 0.01759 0.01080 -0.1226 0.7725 0.0281
-5.750 -0.0908 0.01725 0.01048 -0.1220 0.7711 0.0408
-5.500 -0.0693 0.01692 0.01021 -0.1216 0.7698 0.0532
-5.250 -0.0459 0.01666 0.00998 -0.1215 0.7686 0.0674
-5.000 -0.0234 0.01637 0.00978 -0.1213 0.7673 0.0894
-4.750 -0.0057 0.01600 0.00962 -0.1204 0.7649 0.1323
-4.500 0.0105 0.01529 0.00930 -0.1197 0.7619 0.2168
-4.250 0.0294 0.01404 0.00870 -0.1201 0.7594 0.3762
-4.000 0.0522 0.01301 0.00836 -0.1206 0.7575 0.5514
-3.750 0.0805 0.01318 0.00873 -0.1204 0.7560 0.6021
-3.500 0.1107 0.01357 0.00913 -0.1206 0.7547 0.6241
-3.250 0.1418 0.01386 0.00933 -0.1211 0.7536 0.6392
-3.000 0.1730 0.01414 0.00954 -0.1216 0.7525 0.6476
-2.750 0.2038 0.01450 0.00985 -0.1220 0.7515 0.6535
-2.500 0.2311 0.01473 0.00999 -0.1221 0.7496 0.6608
-2.250 0.2519 0.01507 0.01039 -0.1208 0.7458 0.6629
-2.000 0.2785 0.01535 0.01069 -0.1204 0.7434 0.6658
-1.750 0.3072 0.01566 0.01099 -0.1203 0.7417 0.6708
-1.500 0.3368 0.01592 0.01121 -0.1204 0.7402 0.6783
-1.250 0.3650 0.01620 0.01152 -0.1199 0.7390 0.6809
-1.000 0.3949 0.01628 0.01158 -0.1201 0.7379 0.6830
-0.750 0.4263 0.01619 0.01146 -0.1209 0.7369 0.6853
-0.500 0.4587 0.01607 0.01127 -0.1220 0.7359 0.6885
-0.250 0.4777 0.01606 0.01126 -0.1212 0.7304 0.6938
0.000 0.5045 0.01585 0.01106 -0.1211 0.7279 0.6949
0.250 0.5336 0.01565 0.01085 -0.1215 0.7262 0.6961
0.500 0.5636 0.01547 0.01066 -0.1221 0.7248 0.6973
0.750 0.5946 0.01529 0.01046 -0.1229 0.7237 0.6985
1.000 0.6260 0.01511 0.01026 -0.1237 0.7226 0.7001
1.250 0.6580 0.01491 0.01005 -0.1248 0.7217 0.7021
1.500 0.6742 0.01503 0.01023 -0.1230 0.7160 0.7047
1.750 0.7039 0.01481 0.01000 -0.1238 0.7136 0.7075
2.000 0.7371 0.01459 0.00973 -0.1253 0.7117 0.7103
2.250 0.7675 0.01416 0.00931 -0.1260 0.7100 0.7116
2.500 0.7994 0.01383 0.00897 -0.1269 0.7085 0.7128
2.750 0.8290 0.01365 0.00879 -0.1275 0.7065 0.7140
3.000 0.8469 0.01370 0.00893 -0.1258 0.7016 0.7154
3.250 0.8743 0.01354 0.00880 -0.1259 0.6985 0.7168
3.500 0.9050 0.01331 0.00856 -0.1267 0.6957 0.7183
3.750 0.9374 0.01307 0.00830 -0.1278 0.6931 0.7200
4.000 0.9605 0.01303 0.00831 -0.1272 0.6884 0.7220
4.250 0.9843 0.01298 0.00828 -0.1268 0.6831 0.7243
4.500 1.0141 0.01288 0.00816 -0.1275 0.6792 0.7265
4.750 1.0441 0.01275 0.00802 -0.1283 0.6746 0.7282
5.000 1.0588 0.01262 0.00796 -0.1259 0.6661 0.7297
5.250 1.0828 0.01243 0.00776 -0.1252 0.6577 0.7311
5.500 1.0988 0.01239 0.00775 -0.1230 0.6479 0.7325
5.750 1.1178 0.01239 0.00776 -0.1215 0.6395 0.7339
6.000 1.1331 0.01239 0.00774 -0.1192 0.6297 0.7352
6.250 1.1430 0.01248 0.00784 -0.1160 0.6197 0.7366
6.500 1.1559 0.01261 0.00791 -0.1133 0.6077 0.7382
6.750 1.1614 0.01290 0.00817 -0.1094 0.5938 0.7400
7.000 1.1608 0.01336 0.00861 -0.1045 0.5782 0.7416
7.250 1.1604 0.01393 0.00914 -0.1000 0.5627 0.7428
7.500 1.1581 0.01467 0.00983 -0.0955 0.5456 0.7438
7.750 1.1593 0.01547 0.01058 -0.0918 0.5301 0.7446
8.000 1.1603 0.01633 0.01138 -0.0882 0.5135 0.7453
8.250 1.1614 0.01714 0.01213 -0.0847 0.4969 0.7462
8.500 1.1630 0.01798 0.01293 -0.0813 0.4799 0.7471
8.750 1.1627 0.01896 0.01385 -0.0777 0.4607 0.7482
9.000 1.1595 0.02011 0.01490 -0.0738 0.4376 0.7491
9.250 1.1548 0.02139 0.01606 -0.0698 0.4114 0.7498
9.500 1.1451 0.02297 0.01748 -0.0654 0.3785 0.7503
9.750 1.1406 0.02444 0.01880 -0.0618 0.3501 0.7507
10.000 1.1359 0.02604 0.02025 -0.0584 0.3196 0.7512
10.250 1.1306 0.02778 0.02182 -0.0550 0.2850 0.7518
10.500 1.1245 0.02969 0.02352 -0.0518 0.2493 0.7525
10.750 1.1161 0.03186 0.02545 -0.0486 0.2065 0.7530
11.000 1.1119 0.03389 0.02727 -0.0460 0.1682 0.7534
11.250 1.1029 0.03635 0.02946 -0.0432 0.1227 0.7536
11.500 1.0964 0.03878 0.03165 -0.0407 0.0846 0.7539
11.750 1.0971 0.04076 0.03350 -0.0391 0.0624 0.7544
12.000 1.0952 0.04304 0.03562 -0.0373 0.0395 0.7548
12.250 1.0971 0.04511 0.03761 -0.0359 0.0244 0.7551
12.500 1.1002 0.04716 0.03964 -0.0347 0.0192 0.7552
12.750 1.1080 0.04883 0.04137 -0.0339 0.0176 0.7554
13.000 1.1158 0.05056 0.04314 -0.0332 0.0165 0.7555
13.250 1.1214 0.05253 0.04515 -0.0325 0.0158 0.7558
13.500 1.1299 0.05427 0.04696 -0.0319 0.0152 0.7563
13.750 1.1370 0.05619 0.04894 -0.0314 0.0147 0.7565
14.000 1.1442 0.05812 0.05094 -0.0309 0.0144 0.7566
14.250 1.1501 0.06025 0.05313 -0.0305 0.0140 0.7567
14.500 1.1558 0.06243 0.05536 -0.0302 0.0137 0.7568
14.750 1.1609 0.06474 0.05774 -0.0300 0.0136 0.7569
15.000 1.1639 0.06730 0.06035 -0.0297 0.0133 0.7570
15.250 1.1664 0.06999 0.06311 -0.0296 0.0132 0.7571
15.500 1.1681 0.07282 0.06600 -0.0295 0.0131 0.7571
15.750 1.1710 0.07557 0.06882 -0.0296 0.0130 0.7572
16.000 1.1760 0.07810 0.07142 -0.0297 0.0129 0.7573
16.250 1.1804 0.08073 0.07412 -0.0299 0.0129 0.7575
16.500 1.1850 0.08336 0.07682 -0.0302 0.0128 0.7576
16.750 1.1904 0.08590 0.07942 -0.0304 0.0127 0.7577
17.000 1.1957 0.08849 0.08208 -0.0308 0.0127 0.7578
17.250 1.2016 0.09098 0.08464 -0.0312 0.0127 0.7580
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