FX 76-MP-140 (fx76mp140-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: FX 76-MP-140 (fx76mp140-il) Reynolds number: 1,000,000 Max Cl/Cd: 181.59 at α=3.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx76mp140-il-1000000.txt Download as CSV file: xf-fx76mp140-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: FX 76-MP-140
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
------ -------- --------- --------- -------- -------- --------
-13.000 0.0267 0.11452 0.11158 -0.1286 0.7991 0.0160
-12.750 0.0356 0.11147 0.10853 -0.1301 0.7978 0.0163
-12.500 -0.3785 0.02646 0.02287 -0.1951 0.7921 0.0184
-12.250 -0.3681 0.02472 0.02096 -0.1963 0.7896 0.0188
-12.000 -0.3559 0.02336 0.01948 -0.1964 0.7881 0.0190
-11.750 -0.3396 0.02231 0.01830 -0.1964 0.7864 0.0192
-11.500 -0.3315 0.02027 0.01607 -0.1962 0.7845 0.0197
-11.250 -0.3120 0.01938 0.01511 -0.1962 0.7828 0.0201
-11.000 -0.2896 0.01877 0.01445 -0.1961 0.7812 0.0205
-10.750 -0.2661 0.01825 0.01385 -0.1961 0.7796 0.0209
-10.500 -0.2410 0.01793 0.01349 -0.1961 0.7781 0.0215
-10.250 -0.2175 0.01728 0.01271 -0.1962 0.7764 0.0219
-10.000 -0.1923 0.01682 0.01214 -0.1963 0.7744 0.0224
-9.750 -0.1666 0.01645 0.01166 -0.1964 0.7725 0.0227
-9.500 -0.1455 0.01532 0.01041 -0.1962 0.7713 0.0233
-9.250 -0.1206 0.01481 0.00987 -0.1962 0.7699 0.0239
-9.000 -0.0942 0.01453 0.00957 -0.1962 0.7684 0.0244
-8.750 -0.0679 0.01416 0.00914 -0.1963 0.7668 0.0250
-8.500 -0.0407 0.01398 0.00891 -0.1963 0.7651 0.0258
-8.250 -0.0140 0.01361 0.00845 -0.1964 0.7635 0.0263
-8.000 0.0134 0.01338 0.00815 -0.1965 0.7619 0.0267
-7.750 0.0383 0.01253 0.00720 -0.1965 0.7603 0.0274
-7.500 0.0657 0.01221 0.00684 -0.1967 0.7584 0.0281
-7.250 0.0938 0.01200 0.00657 -0.1969 0.7561 0.0287
-7.000 0.1208 0.01171 0.00626 -0.1969 0.7551 0.0294
-6.750 0.1480 0.01144 0.00595 -0.1969 0.7537 0.0302
-6.500 0.1754 0.01118 0.00565 -0.1969 0.7521 0.0308
-6.250 0.2023 0.01077 0.00519 -0.1970 0.7503 0.0319
-6.000 0.2301 0.01056 0.00498 -0.1971 0.7486 0.0331
-5.750 0.2581 0.01038 0.00478 -0.1972 0.7468 0.0343
-5.500 0.2863 0.01022 0.00456 -0.1973 0.7449 0.0357
-5.250 0.3139 0.00990 0.00421 -0.1974 0.7429 0.0374
-5.000 0.3425 0.00978 0.00407 -0.1976 0.7406 0.0392
-4.750 0.3706 0.00969 0.00395 -0.1977 0.7387 0.0411
-4.500 0.3978 0.00943 0.00370 -0.1977 0.7371 0.0435
-4.250 0.4255 0.00929 0.00358 -0.1977 0.7352 0.0457
-4.000 0.4535 0.00920 0.00347 -0.1977 0.7332 0.0478
-3.750 0.4813 0.00900 0.00326 -0.1978 0.7311 0.0504
-3.500 0.5093 0.00887 0.00313 -0.1978 0.7288 0.0528
-3.250 0.5374 0.00879 0.00302 -0.1979 0.7266 0.0550
-3.000 0.5660 0.00869 0.00288 -0.1981 0.7240 0.0578
-2.750 0.5936 0.00858 0.00280 -0.1981 0.7221 0.0611
-2.500 0.6210 0.00850 0.00273 -0.1981 0.7200 0.0641
-2.250 0.6485 0.00836 0.00262 -0.1980 0.7177 0.0700
-2.000 0.6762 0.00828 0.00254 -0.1980 0.7152 0.0747
-1.750 0.7036 0.00815 0.00244 -0.1980 0.7127 0.0836
-1.500 0.7314 0.00806 0.00236 -0.1980 0.7099 0.0935
-1.250 0.7594 0.00801 0.00232 -0.1981 0.7069 0.1061
-1.000 0.7860 0.00791 0.00229 -0.1979 0.7045 0.1229
-0.750 0.8130 0.00782 0.00227 -0.1978 0.7016 0.1441
-0.500 0.8399 0.00773 0.00224 -0.1977 0.6986 0.1674
-0.250 0.8668 0.00764 0.00222 -0.1976 0.6954 0.1967
0.000 0.8940 0.00759 0.00221 -0.1976 0.6917 0.2342
0.250 0.9196 0.00745 0.00223 -0.1972 0.6884 0.2857
0.500 0.9451 0.00729 0.00226 -0.1969 0.6847 0.3601
0.750 0.9693 0.00700 0.00231 -0.1964 0.6812 0.5089
1.000 0.9913 0.00671 0.00244 -0.1953 0.6776 0.6983
1.250 1.0157 0.00669 0.00253 -0.1945 0.6738 0.7575
1.500 1.0408 0.00669 0.00259 -0.1940 0.6697 0.7851
1.750 1.0659 0.00672 0.00263 -0.1934 0.6653 0.8038
2.000 1.0905 0.00679 0.00268 -0.1927 0.6607 0.8228
2.250 1.1147 0.00680 0.00274 -0.1920 0.6556 0.8391
2.500 1.1384 0.00683 0.00279 -0.1911 0.6498 0.8522
2.750 1.1616 0.00690 0.00284 -0.1901 0.6444 0.8649
3.000 1.1855 0.00693 0.00291 -0.1894 0.6384 0.8779
3.250 1.2077 0.00698 0.00298 -0.1882 0.6323 0.8937
3.500 1.2299 0.00701 0.00305 -0.1871 0.6261 0.9189
3.750 1.2766 0.00703 0.00314 -0.1915 0.6178 1.0000
4.000 1.3010 0.00717 0.00325 -0.1910 0.6091 1.0000
4.250 1.3233 0.00736 0.00337 -0.1901 0.5980 1.0000
4.500 1.3464 0.00753 0.00350 -0.1893 0.5866 1.0000
4.750 1.3676 0.00774 0.00367 -0.1882 0.5745 1.0000
5.000 1.3866 0.00799 0.00386 -0.1866 0.5628 1.0000
5.250 1.4052 0.00828 0.00408 -0.1850 0.5502 1.0000
5.500 1.4254 0.00857 0.00432 -0.1837 0.5366 1.0000
5.750 1.4454 0.00890 0.00460 -0.1825 0.5228 1.0000
6.000 1.4660 0.00925 0.00490 -0.1814 0.5107 1.0000
6.250 1.4862 0.00964 0.00524 -0.1804 0.4992 1.0000
6.500 1.5076 0.01001 0.00558 -0.1796 0.4879 1.0000
6.750 1.5287 0.01041 0.00595 -0.1788 0.4768 1.0000
7.000 1.5480 0.01089 0.00640 -0.1778 0.4658 1.0000
7.250 1.5656 0.01146 0.00692 -0.1765 0.4527 1.0000
7.500 1.5839 0.01200 0.00744 -0.1754 0.4405 1.0000
7.750 1.5998 0.01268 0.00807 -0.1740 0.4274 1.0000
8.000 1.6138 0.01347 0.00881 -0.1724 0.4132 1.0000
8.250 1.6278 0.01429 0.00959 -0.1708 0.4014 1.0000
8.500 1.6426 0.01508 0.01036 -0.1694 0.3893 1.0000
8.750 1.6569 0.01592 0.01118 -0.1680 0.3777 1.0000
9.000 1.6693 0.01689 0.01211 -0.1663 0.3660 1.0000
9.250 1.6795 0.01800 0.01317 -0.1645 0.3519 1.0000
9.500 1.6897 0.01914 0.01426 -0.1626 0.3379 1.0000
9.750 1.6994 0.02029 0.01536 -0.1608 0.3237 1.0000
10.000 1.7080 0.02153 0.01655 -0.1588 0.3091 1.0000
10.250 1.7162 0.02280 0.01777 -0.1568 0.2942 1.0000
10.500 1.7217 0.02425 0.01915 -0.1546 0.2775 1.0000
10.750 1.7291 0.02560 0.02045 -0.1526 0.2639 1.0000
11.000 1.7362 0.02698 0.02179 -0.1506 0.2509 1.0000
11.250 1.7401 0.02860 0.02334 -0.1483 0.2343 1.0000
11.500 1.7457 0.03015 0.02483 -0.1463 0.2206 1.0000
11.750 1.7501 0.03182 0.02644 -0.1442 0.2064 1.0000
12.000 1.7547 0.03351 0.02808 -0.1422 0.1933 1.0000
12.250 1.7572 0.03538 0.02987 -0.1401 0.1780 1.0000
12.500 1.7617 0.03715 0.03160 -0.1383 0.1674 1.0000
12.750 1.7676 0.03883 0.03326 -0.1366 0.1573 1.0000
13.000 1.7742 0.04050 0.03493 -0.1351 0.1498 1.0000
13.250 1.7781 0.04238 0.03678 -0.1333 0.1400 1.0000
13.500 1.7844 0.04413 0.03853 -0.1319 0.1322 1.0000
13.750 1.7885 0.04607 0.04044 -0.1303 0.1234 1.0000
14.000 1.7904 0.04827 0.04261 -0.1287 0.1142 1.0000
14.250 1.7953 0.05021 0.04455 -0.1273 0.1064 1.0000
14.500 1.7961 0.05255 0.04688 -0.1257 0.0968 1.0000
14.750 1.7940 0.05521 0.04948 -0.1240 0.0842 1.0000
15.000 1.7857 0.05856 0.05274 -0.1220 0.0697 1.0000
15.250 1.7746 0.06228 0.05638 -0.1201 0.0533 1.0000
15.500 1.7650 0.06590 0.05995 -0.1183 0.0429 1.0000
16.000 1.7599 0.07193 0.06602 -0.1160 0.0335 1.0000
16.250 1.7585 0.07486 0.06898 -0.1150 0.0302 1.0000
16.500 1.7567 0.07787 0.07203 -0.1142 0.0278 1.0000
16.750 1.7554 0.08084 0.07506 -0.1134 0.0258 1.0000
17.000 1.7548 0.08377 0.07804 -0.1127 0.0243 1.0000
17.250 1.7514 0.08710 0.08142 -0.1120 0.0228 1.0000
17.500 1.7506 0.09012 0.08451 -0.1115 0.0217 1.0000
17.750 1.7489 0.09328 0.08773 -0.1111 0.0205 1.0000
18.000 1.7441 0.09684 0.09135 -0.1108 0.0194 1.0000
18.250 1.7396 0.10037 0.09495 -0.1105 0.0183 1.0000
18.500 1.7386 0.10349 0.09815 -0.1103 0.0175 1.0000
18.750 1.7347 0.10703 0.10176 -0.1103 0.0165 1.0000
19.000 1.7274 0.11105 0.10583 -0.1103 0.0155 1.0000
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