WORTMANN FX 76-120 (fx76120-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: WORTMANN FX 76-120 (fx76120-il) Reynolds number: 500,000 Max Cl/Cd: 67.87 at α=6.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx76120-il-500000.txt Download as CSV file: xf-fx76120-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 76-120
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
------ -------- --------- --------- -------- -------- --------
-18.500 -1.0271 0.12070 0.11749 -0.0068 1.0000 0.0201
-18.250 -1.0513 0.11186 0.10850 -0.0119 1.0000 0.0203
-18.000 -1.0681 0.10464 0.10116 -0.0160 1.0000 0.0204
-17.750 -1.0918 0.09657 0.09291 -0.0203 1.0000 0.0205
-17.500 -1.1068 0.09008 0.08629 -0.0240 1.0000 0.0207
-17.250 -1.1200 0.08401 0.08010 -0.0274 1.0000 0.0209
-17.000 -1.1352 0.07806 0.07401 -0.0303 1.0000 0.0208
-16.750 -1.1439 0.07278 0.06859 -0.0336 1.0000 0.0212
-16.500 -1.1563 0.06742 0.06308 -0.0363 1.0000 0.0213
-16.250 -1.1638 0.06283 0.05836 -0.0387 1.0000 0.0215
-16.000 -1.1720 0.05829 0.05366 -0.0409 1.0000 0.0217
-15.750 -1.1810 0.05391 0.04915 -0.0427 1.0000 0.0220
-15.500 -1.1888 0.04992 0.04507 -0.0440 1.0000 0.0224
-15.250 -1.1920 0.04654 0.04162 -0.0451 1.0000 0.0228
-15.000 -1.1935 0.04350 0.03849 -0.0460 1.0000 0.0231
-14.750 -1.1929 0.04082 0.03573 -0.0465 1.0000 0.0234
-14.500 -1.1911 0.03843 0.03325 -0.0467 1.0000 0.0240
-14.250 -1.1878 0.03634 0.03107 -0.0466 1.0000 0.0245
-14.000 -1.1851 0.03431 0.02892 -0.0461 1.0000 0.0249
-13.750 -1.1803 0.03262 0.02710 -0.0453 1.0000 0.0254
-13.500 -1.1752 0.03103 0.02540 -0.0442 1.0000 0.0258
-13.250 -1.1719 0.02939 0.02365 -0.0426 1.0000 0.0265
-13.000 -1.1706 0.02773 0.02193 -0.0406 1.0000 0.0272
-12.750 -1.1631 0.02666 0.02084 -0.0388 1.0000 0.0280
-12.500 -1.1552 0.02566 0.01978 -0.0367 1.0000 0.0286
-12.250 -1.1450 0.02488 0.01893 -0.0347 1.0000 0.0296
-12.000 -1.1355 0.02408 0.01804 -0.0323 1.0000 0.0305
-11.750 -1.1241 0.02349 0.01735 -0.0300 1.0000 0.0311
-11.500 -1.1220 0.02237 0.01618 -0.0262 1.0000 0.0321
-11.250 -1.1149 0.02152 0.01531 -0.0231 1.0000 0.0331
-11.000 -1.1015 0.02090 0.01466 -0.0210 1.0000 0.0343
-10.750 -1.0867 0.02035 0.01405 -0.0189 1.0000 0.0356
-10.500 -1.0699 0.01990 0.01353 -0.0171 1.0000 0.0369
-10.250 -1.0579 0.01910 0.01267 -0.0146 1.0000 0.0380
-10.000 -1.0459 0.01832 0.01189 -0.0120 1.0000 0.0397
-9.750 -1.0298 0.01782 0.01136 -0.0100 1.0000 0.0414
-9.500 -1.0128 0.01738 0.01087 -0.0081 1.0000 0.0431
-9.250 -0.9963 0.01691 0.01033 -0.0061 1.0000 0.0448
-9.000 -0.9836 0.01620 0.00964 -0.0035 1.0000 0.0472
-8.750 -0.9673 0.01576 0.00918 -0.0014 1.0000 0.0494
-8.500 -0.9501 0.01539 0.00875 0.0006 1.0000 0.0517
-8.250 -0.9358 0.01484 0.00820 0.0031 1.0000 0.0550
-8.000 -0.9198 0.01442 0.00779 0.0053 1.0000 0.0585
-7.750 -0.9024 0.01411 0.00743 0.0073 1.0000 0.0620
-7.500 -0.8876 0.01360 0.00696 0.0096 1.0000 0.0676
-7.250 -0.8706 0.01324 0.00659 0.0117 1.0000 0.0738
-7.000 -0.8541 0.01284 0.00623 0.0137 1.0000 0.0824
-6.750 -0.8372 0.01245 0.00590 0.0157 1.0000 0.0936
-6.500 -0.8197 0.01211 0.00562 0.0176 1.0000 0.1078
-6.250 -0.7994 0.01178 0.00538 0.0189 0.9997 0.1246
-6.000 -0.7647 0.01146 0.00517 0.0172 0.9972 0.1450
-5.750 -0.7290 0.01122 0.00499 0.0154 0.9947 0.1627
-5.500 -0.6947 0.01098 0.00480 0.0138 0.9916 0.1790
-5.250 -0.6586 0.01076 0.00464 0.0120 0.9890 0.1944
-5.000 -0.6232 0.01053 0.00446 0.0103 0.9861 0.2089
-4.750 -0.5869 0.01030 0.00428 0.0085 0.9823 0.2237
-4.500 -0.5462 0.01005 0.00409 0.0057 0.9796 0.2397
-4.250 -0.5118 0.00980 0.00390 0.0043 0.9745 0.2558
-4.000 -0.4747 0.00955 0.00372 0.0024 0.9712 0.2748
-3.750 -0.4361 0.00928 0.00354 0.0001 0.9690 0.2963
-3.500 -0.4050 0.00900 0.00337 -0.0005 0.9632 0.3184
-3.250 -0.3661 0.00869 0.00317 -0.0028 0.9597 0.3454
-3.000 -0.3241 0.00834 0.00296 -0.0058 0.9569 0.3785
-2.750 -0.2942 0.00806 0.00280 -0.0060 0.9482 0.4093
-2.500 -0.2571 0.00775 0.00262 -0.0079 0.9430 0.4435
-2.250 -0.2304 0.00749 0.00249 -0.0075 0.9325 0.4765
-2.000 -0.2012 0.00723 0.00237 -0.0075 0.9224 0.5137
-1.750 -0.1718 0.00698 0.00225 -0.0076 0.9110 0.5518
-1.500 -0.1468 0.00678 0.00216 -0.0067 0.8967 0.5888
-1.250 -0.1219 0.00661 0.00209 -0.0057 0.8813 0.6229
-1.000 -0.0971 0.00646 0.00202 -0.0047 0.8653 0.6557
-0.750 -0.0727 0.00632 0.00197 -0.0036 0.8476 0.6896
-0.500 -0.0483 0.00623 0.00193 -0.0024 0.8275 0.7219
-0.250 -0.0242 0.00616 0.00191 -0.0012 0.8037 0.7504
0.000 0.0000 0.00616 0.00189 0.0000 0.7783 0.7782
0.250 0.0242 0.00616 0.00191 0.0012 0.7503 0.8038
0.500 0.0483 0.00623 0.00193 0.0024 0.7216 0.8274
0.750 0.0726 0.00632 0.00197 0.0036 0.6894 0.8471
1.000 0.0971 0.00646 0.00202 0.0047 0.6554 0.8656
1.250 0.1220 0.00661 0.00209 0.0057 0.6229 0.8818
1.500 0.1467 0.00678 0.00216 0.0067 0.5884 0.8966
1.750 0.1721 0.00698 0.00225 0.0075 0.5519 0.9106
2.000 0.2012 0.00723 0.00237 0.0075 0.5138 0.9226
2.250 0.2303 0.00749 0.00249 0.0075 0.4767 0.9324
2.500 0.2570 0.00774 0.00262 0.0079 0.4438 0.9430
2.750 0.2943 0.00806 0.00280 0.0060 0.4090 0.9483
3.000 0.3244 0.00834 0.00296 0.0057 0.3789 0.9569
3.250 0.3662 0.00869 0.00317 0.0028 0.3452 0.9598
3.500 0.4050 0.00900 0.00337 0.0005 0.3185 0.9632
3.750 0.4364 0.00928 0.00354 -0.0001 0.2960 0.9691
4.000 0.4749 0.00955 0.00372 -0.0024 0.2750 0.9712
4.250 0.5116 0.00980 0.00390 -0.0043 0.2561 0.9744
4.500 0.5463 0.01005 0.00409 -0.0057 0.2398 0.9796
4.750 0.5870 0.01030 0.00428 -0.0085 0.2235 0.9823
5.000 0.6234 0.01053 0.00446 -0.0103 0.2085 0.9861
5.250 0.6587 0.01076 0.00463 -0.0120 0.1939 0.9890
5.500 0.6948 0.01098 0.00480 -0.0139 0.1791 0.9916
5.750 0.7290 0.01122 0.00499 -0.0154 0.1635 0.9947
6.000 0.7645 0.01145 0.00517 -0.0171 0.1457 0.9972
6.250 0.7995 0.01178 0.00538 -0.0189 0.1245 0.9997
6.500 0.8197 0.01210 0.00562 -0.0176 0.1081 1.0000
6.750 0.8372 0.01244 0.00590 -0.0157 0.0937 1.0000
7.000 0.8540 0.01284 0.00623 -0.0137 0.0823 1.0000
7.250 0.8705 0.01324 0.00659 -0.0116 0.0739 1.0000
7.500 0.8875 0.01359 0.00696 -0.0096 0.0680 1.0000
7.750 0.9023 0.01411 0.00743 -0.0072 0.0620 1.0000
8.000 0.9197 0.01442 0.00779 -0.0052 0.0586 1.0000
8.250 0.9358 0.01484 0.00820 -0.0031 0.0550 1.0000
8.500 0.9498 0.01541 0.00877 -0.0006 0.0518 1.0000
8.750 0.9673 0.01575 0.00917 0.0014 0.0494 1.0000
9.000 0.9836 0.01620 0.00963 0.0035 0.0471 1.0000
9.250 0.9957 0.01695 0.01038 0.0062 0.0446 1.0000
9.500 1.0127 0.01738 0.01087 0.0081 0.0431 1.0000
9.750 1.0298 0.01782 0.01136 0.0100 0.0413 1.0000
10.000 1.0460 0.01832 0.01189 0.0120 0.0397 1.0000
10.250 1.0580 0.01910 0.01267 0.0145 0.0381 1.0000
10.500 1.0709 0.01983 0.01347 0.0170 0.0367 1.0000
10.750 1.0871 0.02032 0.01403 0.0188 0.0355 1.0000
11.000 1.1019 0.02089 0.01464 0.0209 0.0342 1.0000
11.250 1.1152 0.02152 0.01531 0.0231 0.0331 1.0000
11.500 1.1218 0.02240 0.01621 0.0263 0.0320 1.0000
11.750 1.1238 0.02354 0.01739 0.0300 0.0312 1.0000
12.000 1.1353 0.02414 0.01810 0.0323 0.0305 1.0000
12.250 1.1455 0.02488 0.01893 0.0346 0.0296 1.0000
12.500 1.1541 0.02579 0.01992 0.0368 0.0288 1.0000
12.750 1.1649 0.02655 0.02071 0.0385 0.0278 1.0000
13.000 1.1712 0.02773 0.02194 0.0405 0.0272 1.0000
13.250 1.1720 0.02945 0.02370 0.0425 0.0265 1.0000
13.500 1.1748 0.03115 0.02551 0.0441 0.0259 1.0000
13.750 1.1813 0.03260 0.02709 0.0452 0.0254 1.0000
14.000 1.1853 0.03438 0.02899 0.0460 0.0250 1.0000
14.250 1.1890 0.03631 0.03103 0.0465 0.0244 1.0000
14.500 1.1920 0.03844 0.03326 0.0466 0.0238 1.0000
14.750 1.1939 0.04083 0.03574 0.0463 0.0234 1.0000
15.000 1.1942 0.04354 0.03854 0.0458 0.0231 1.0000
15.250 1.1950 0.04634 0.04141 0.0449 0.0228 1.0000
15.500 1.1902 0.04991 0.04504 0.0437 0.0223 1.0000
15.750 1.1837 0.05376 0.04899 0.0425 0.0220 1.0000
16.000 1.1729 0.05838 0.05376 0.0406 0.0216 1.0000
16.250 1.1669 0.06268 0.05821 0.0383 0.0214 1.0000
16.500 1.1578 0.06756 0.06323 0.0357 0.0212 1.0000
16.750 1.1471 0.07271 0.06853 0.0331 0.0211 1.0000
17.000 1.1365 0.07816 0.07411 0.0299 0.0207 1.0000
17.250 1.1209 0.08426 0.08035 0.0269 0.0207 1.0000
17.500 1.1071 0.09040 0.08662 0.0234 0.0205 1.0000
17.750 1.0937 0.09673 0.09308 0.0197 0.0203 1.0000
18.000 1.0745 0.10403 0.10052 0.0158 0.0202 1.0000
18.250 1.0570 0.11136 0.10798 0.0116 0.0200 1.0000
18.500 1.0314 0.12038 0.11716 0.0066 0.0200 1.0000
18.750 0.9952 0.13205 0.12903 -0.0001 0.0200 1.0000
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