WORTMANN FX 75-193 (fx75193-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: WORTMANN FX 75-193 (fx75193-il) Reynolds number: 1,000,000 Max Cl/Cd: 122.66 at α=4.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx75193-il-1000000.txt Download as CSV file: xf-fx75193-il-1000000.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 = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-16.000 -0.3708 0.08335 0.08005 -0.1341 0.7883 0.0080
-15.750 -0.4008 0.07262 0.06913 -0.1418 0.7880 0.0078
-15.500 -0.4230 0.06403 0.06034 -0.1487 0.7877 0.0080
-15.250 -0.4362 0.05783 0.05397 -0.1536 0.7873 0.0078
-15.000 -0.4489 0.05227 0.04821 -0.1576 0.7869 0.0077
-14.750 -0.4525 0.04829 0.04408 -0.1606 0.7864 0.0077
-14.500 -0.4554 0.04470 0.04032 -0.1631 0.7858 0.0079
-14.250 -0.4592 0.04127 0.03671 -0.1649 0.7851 0.0078
-14.000 -0.4544 0.03896 0.03428 -0.1664 0.7843 0.0080
-13.750 -0.4489 0.03689 0.03209 -0.1675 0.7834 0.0081
-13.500 -0.4483 0.03479 0.02985 -0.1671 0.7831 0.0080
-13.250 -0.4426 0.03334 0.02831 -0.1667 0.7827 0.0082
-13.000 -0.4366 0.03200 0.02686 -0.1662 0.7823 0.0084
-12.750 -0.4294 0.03076 0.02552 -0.1655 0.7817 0.0085
-12.500 -0.4212 0.02967 0.02434 -0.1648 0.7810 0.0086
-12.250 -0.4161 0.02911 0.02370 -0.1640 0.7802 0.0087
-11.750 -0.3900 0.02675 0.02119 -0.1624 0.7788 0.0087
-11.500 -0.3757 0.02527 0.01960 -0.1614 0.7780 0.0090
-11.250 -0.3611 0.02444 0.01872 -0.1605 0.7772 0.0090
-11.000 -0.3465 0.02361 0.01786 -0.1595 0.7764 0.0090
-10.750 -0.3332 0.02279 0.01703 -0.1584 0.7755 0.0093
-10.500 -0.3192 0.02207 0.01627 -0.1573 0.7745 0.0093
-10.250 -0.3054 0.02138 0.01554 -0.1561 0.7733 0.0093
-10.000 -0.2911 0.02075 0.01487 -0.1549 0.7720 0.0094
-9.750 -0.2774 0.02010 0.01419 -0.1537 0.7708 0.0094
-9.500 -0.2639 0.01950 0.01356 -0.1523 0.7698 0.0095
-9.250 -0.2498 0.01898 0.01301 -0.1511 0.7687 0.0096
-9.000 -0.2378 0.01854 0.01255 -0.1494 0.7670 0.0097
-8.750 -0.2257 0.01806 0.01206 -0.1476 0.7661 0.0097
-8.500 -0.2130 0.01750 0.01149 -0.1459 0.7654 0.0098
-8.250 -0.2020 0.01690 0.01087 -0.1440 0.7645 0.0099
-8.000 -0.1896 0.01639 0.01035 -0.1421 0.7634 0.0100
-7.750 -0.1775 0.01590 0.00985 -0.1402 0.7622 0.0102
-7.500 -0.1670 0.01545 0.00939 -0.1380 0.7610 0.0104
-7.250 -0.1614 0.01504 0.00896 -0.1348 0.7597 0.0105
-7.000 -0.1523 0.01468 0.00858 -0.1324 0.7585 0.0107
-6.750 -0.1362 0.01428 0.00816 -0.1312 0.7574 0.0109
-6.500 -0.1178 0.01389 0.00774 -0.1303 0.7563 0.0111
-6.250 -0.0970 0.01357 0.00739 -0.1297 0.7553 0.0112
-6.000 -0.0756 0.01323 0.00701 -0.1292 0.7542 0.0116
-5.750 -0.0531 0.01291 0.00666 -0.1288 0.7532 0.0124
-5.500 -0.0296 0.01267 0.00638 -0.1286 0.7522 0.0137
-5.250 -0.0090 0.01245 0.00627 -0.1280 0.7505 0.0331
-5.000 0.0160 0.01215 0.00601 -0.1280 0.7497 0.0422
-4.500 0.0661 0.01152 0.00555 -0.1281 0.7474 0.0737
-4.250 0.0904 0.01108 0.00528 -0.1282 0.7459 0.1147
-4.000 0.1145 0.01050 0.00497 -0.1284 0.7444 0.1849
-3.750 0.1378 0.00960 0.00454 -0.1289 0.7430 0.3091
-3.500 0.1609 0.00837 0.00397 -0.1296 0.7417 0.5001
-3.250 0.1884 0.00797 0.00382 -0.1300 0.7405 0.5806
-3.000 0.2179 0.00794 0.00389 -0.1305 0.7395 0.6125
-2.750 0.2485 0.00811 0.00408 -0.1311 0.7385 0.6318
-2.500 0.2795 0.00818 0.00407 -0.1319 0.7376 0.6433
-2.250 0.3102 0.00832 0.00419 -0.1325 0.7365 0.6476
-2.000 0.3395 0.00843 0.00429 -0.1330 0.7351 0.6512
-1.750 0.3682 0.00848 0.00433 -0.1333 0.7334 0.6552
-1.500 0.3973 0.00851 0.00433 -0.1337 0.7314 0.6590
-1.250 0.4265 0.00857 0.00439 -0.1340 0.7294 0.6624
-1.000 0.4561 0.00869 0.00455 -0.1343 0.7275 0.6656
-0.750 0.4861 0.00882 0.00469 -0.1347 0.7259 0.6693
-0.500 0.5163 0.00891 0.00476 -0.1353 0.7244 0.6730
-0.250 0.5467 0.00895 0.00476 -0.1359 0.7230 0.6757
0.000 0.5766 0.00888 0.00466 -0.1366 0.7216 0.6772
0.250 0.6037 0.00879 0.00461 -0.1367 0.7192 0.6786
0.500 0.6317 0.00874 0.00458 -0.1370 0.7167 0.6798
0.750 0.6603 0.00867 0.00452 -0.1373 0.7141 0.6809
1.000 0.6891 0.00859 0.00444 -0.1377 0.7115 0.6820
1.250 0.7184 0.00850 0.00434 -0.1382 0.7089 0.6831
1.500 0.7468 0.00848 0.00430 -0.1385 0.7058 0.6844
1.750 0.7740 0.00847 0.00432 -0.1386 0.7022 0.6857
2.000 0.8018 0.00845 0.00432 -0.1389 0.6987 0.6871
2.250 0.8301 0.00843 0.00427 -0.1392 0.6953 0.6885
2.500 0.8583 0.00844 0.00424 -0.1395 0.6912 0.6899
2.750 0.8846 0.00846 0.00430 -0.1395 0.6863 0.6912
3.000 0.9116 0.00849 0.00433 -0.1396 0.6812 0.6922
3.250 0.9388 0.00856 0.00435 -0.1397 0.6764 0.6930
3.500 0.9642 0.00843 0.00427 -0.1395 0.6703 0.6947
3.750 0.9890 0.00840 0.00423 -0.1392 0.6621 0.6958
4.000 1.0126 0.00842 0.00425 -0.1385 0.6513 0.6967
4.250 1.0350 0.00850 0.00429 -0.1377 0.6410 0.6977
4.500 1.0561 0.00861 0.00438 -0.1365 0.6296 0.6987
4.750 1.0749 0.00877 0.00451 -0.1349 0.6154 0.6999
5.000 1.0929 0.00895 0.00466 -0.1332 0.6027 0.7012
5.250 1.1085 0.00916 0.00482 -0.1310 0.5905 0.7025
5.500 1.1231 0.00933 0.00497 -0.1286 0.5776 0.7037
5.750 1.1302 0.00952 0.00513 -0.1246 0.5623 0.7047
6.000 1.1354 0.00982 0.00538 -0.1204 0.5454 0.7058
6.250 1.1352 0.01030 0.00579 -0.1153 0.5269 0.7070
6.500 1.1312 0.01091 0.00633 -0.1097 0.5086 0.7080
6.750 1.1247 0.01170 0.00706 -0.1040 0.4903 0.7087
7.000 1.1171 0.01276 0.00804 -0.0987 0.4703 0.7093
7.250 1.1123 0.01390 0.00910 -0.0941 0.4503 0.7098
7.500 1.1060 0.01514 0.01023 -0.0894 0.4277 0.7102
7.750 1.1064 0.01603 0.01104 -0.0857 0.4075 0.7111
8.000 1.1029 0.01713 0.01201 -0.0816 0.3808 0.7118
8.250 1.0965 0.01841 0.01314 -0.0771 0.3516 0.7126
8.500 1.0928 0.01963 0.01421 -0.0731 0.3208 0.7133
8.750 1.0880 0.02096 0.01537 -0.0692 0.2875 0.7139
9.000 1.0813 0.02248 0.01666 -0.0651 0.2478 0.7144
9.250 1.0751 0.02410 0.01806 -0.0613 0.2072 0.7147
9.500 1.0640 0.02608 0.01972 -0.0571 0.1541 0.7150
9.750 1.0621 0.02770 0.02116 -0.0542 0.1200 0.7153
10.000 1.0602 0.02939 0.02266 -0.0514 0.0848 0.7158
10.250 1.0606 0.03106 0.02418 -0.0490 0.0580 0.7163
10.500 1.0657 0.03248 0.02550 -0.0472 0.0402 0.7166
10.750 1.0700 0.03401 0.02693 -0.0454 0.0223 0.7171
11.000 1.0801 0.03519 0.02810 -0.0442 0.0171 0.7175
11.250 1.0904 0.03639 0.02929 -0.0430 0.0123 0.7178
11.500 1.1010 0.03761 0.03051 -0.0420 0.0104 0.7179
11.750 1.1135 0.03869 0.03163 -0.0411 0.0101 0.7182
12.000 1.1258 0.03981 0.03278 -0.0403 0.0097 0.7185
12.250 1.1375 0.04101 0.03400 -0.0395 0.0095 0.7188
12.500 1.1473 0.04238 0.03541 -0.0386 0.0091 0.7189
12.750 1.1583 0.04369 0.03676 -0.0378 0.0089 0.7189
13.000 1.1682 0.04510 0.03821 -0.0370 0.0088 0.7190
13.250 1.1776 0.04661 0.03976 -0.0363 0.0087 0.7191
13.500 1.1861 0.04820 0.04141 -0.0355 0.0086 0.7192
13.750 1.1934 0.04996 0.04322 -0.0348 0.0085 0.7192
14.000 1.2016 0.05167 0.04498 -0.0341 0.0084 0.7193
14.250 1.2094 0.05345 0.04681 -0.0335 0.0084 0.7194
14.500 1.2161 0.05537 0.04880 -0.0330 0.0083 0.7195
14.750 1.2241 0.05719 0.05067 -0.0326 0.0084 0.7196
15.000 1.2295 0.05933 0.05287 -0.0321 0.0083 0.7197
15.250 1.2359 0.06140 0.05500 -0.0318 0.0083 0.7198
15.500 1.2409 0.06368 0.05734 -0.0315 0.0083 0.7199
15.750 1.2455 0.06603 0.05976 -0.0312 0.0083 0.7200
16.000 1.2511 0.06831 0.06211 -0.0311 0.0083 0.7201
16.250 1.2550 0.07083 0.06470 -0.0311 0.0082 0.7202
16.500 1.2607 0.07319 0.06712 -0.0311 0.0082 0.7203
16.750 1.2628 0.07602 0.07003 -0.0312 0.0082 0.7204
17.000 1.2671 0.07863 0.07270 -0.0314 0.0081 0.7205
17.250 1.2689 0.08160 0.07575 -0.0317 0.0081 0.7206
17.500 1.2721 0.08441 0.07863 -0.0320 0.0081 0.7208
17.750 1.2745 0.08739 0.08169 -0.0325 0.0081 0.7209
18.000 1.2771 0.09037 0.08474 -0.0330 0.0081 0.7211
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