WORTMANN FX 76-100 (fx76100-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 76-100 (fx76100-il) Reynolds number: 500,000 Max Cl/Cd: 61.35 at α=6.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx76100-il-500000-n5.txt Download as CSV file: xf-fx76100-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 76-100
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-17.750 -0.9325 0.14501 0.14229 0.0191 1.0000 0.0097
-17.500 -0.9716 0.13157 0.12869 0.0122 1.0000 0.0097
-17.250 -0.9999 0.12126 0.11825 0.0068 1.0000 0.0095
-17.000 -1.0249 0.11195 0.10882 0.0019 1.0000 0.0096
-16.750 -1.0538 0.10233 0.09906 -0.0032 1.0000 0.0094
-16.500 -1.0778 0.09383 0.09046 -0.0078 1.0000 0.0096
-16.250 -1.1067 0.08484 0.08131 -0.0126 1.0000 0.0095
-16.000 -1.1292 0.07695 0.07327 -0.0169 1.0000 0.0093
-15.750 -1.1543 0.06856 0.06477 -0.0219 1.0000 0.0095
-15.500 -1.1728 0.06138 0.05742 -0.0263 1.0000 0.0094
-15.250 -1.1906 0.05440 0.05027 -0.0308 1.0000 0.0094
-15.000 -1.2036 0.04859 0.04429 -0.0345 1.0000 0.0095
-14.750 -1.2114 0.04398 0.03956 -0.0372 1.0000 0.0097
-14.500 -1.2191 0.04000 0.03539 -0.0389 1.0000 0.0097
-14.250 -1.2171 0.03752 0.03282 -0.0395 1.0000 0.0100
-14.000 -1.2189 0.03495 0.03011 -0.0393 1.0000 0.0100
-13.750 -1.2201 0.03270 0.02773 -0.0385 1.0000 0.0102
-13.500 -1.2152 0.03117 0.02610 -0.0374 1.0000 0.0105
-13.250 -1.2097 0.02980 0.02462 -0.0358 1.0000 0.0107
-13.000 -1.2038 0.02855 0.02326 -0.0339 1.0000 0.0110
-12.750 -1.1991 0.02733 0.02192 -0.0315 1.0000 0.0112
-12.500 -1.1912 0.02638 0.02086 -0.0291 1.0000 0.0116
-12.250 -1.1837 0.02540 0.01977 -0.0265 1.0000 0.0118
-12.000 -1.1729 0.02443 0.01868 -0.0243 1.0000 0.0120
-11.750 -1.1618 0.02342 0.01757 -0.0222 1.0000 0.0124
-11.500 -1.1485 0.02252 0.01660 -0.0203 1.0000 0.0128
-11.250 -1.1330 0.02177 0.01578 -0.0186 1.0000 0.0133
-11.000 -1.1162 0.02109 0.01504 -0.0171 1.0000 0.0138
-10.750 -1.0993 0.02039 0.01426 -0.0155 1.0000 0.0144
-10.500 -1.0814 0.01977 0.01356 -0.0140 1.0000 0.0150
-10.250 -1.0628 0.01920 0.01288 -0.0126 1.0000 0.0156
-10.000 -1.0454 0.01850 0.01213 -0.0110 1.0000 0.0164
-9.750 -1.0266 0.01792 0.01152 -0.0096 1.0000 0.0172
-9.500 -1.0068 0.01742 0.01098 -0.0083 1.0000 0.0182
-9.250 -0.9870 0.01693 0.01042 -0.0070 1.0000 0.0192
-9.000 -0.9668 0.01649 0.00989 -0.0056 1.0000 0.0199
-8.750 -0.9479 0.01591 0.00928 -0.0041 1.0000 0.0210
-8.500 -0.9280 0.01545 0.00880 -0.0027 1.0000 0.0223
-8.250 -0.9075 0.01505 0.00837 -0.0014 1.0000 0.0237
-8.000 -0.8869 0.01469 0.00795 0.0000 1.0000 0.0251
-7.750 -0.8671 0.01424 0.00747 0.0015 1.0000 0.0267
-7.500 -0.8472 0.01384 0.00705 0.0029 1.0000 0.0284
-7.250 -0.8269 0.01349 0.00668 0.0044 1.0000 0.0303
-7.000 -0.8062 0.01320 0.00635 0.0058 1.0000 0.0321
-6.750 -0.7866 0.01281 0.00596 0.0073 1.0000 0.0349
-6.500 -0.7666 0.01250 0.00564 0.0088 1.0000 0.0378
-6.250 -0.7440 0.01223 0.00534 0.0098 0.9997 0.0406
-6.000 -0.7114 0.01184 0.00498 0.0086 0.9972 0.0469
-5.750 -0.6791 0.01151 0.00465 0.0075 0.9941 0.0532
-5.500 -0.6468 0.01118 0.00435 0.0064 0.9910 0.0622
-5.250 -0.6145 0.01083 0.00406 0.0053 0.9883 0.0748
-5.000 -0.5840 0.01048 0.00378 0.0046 0.9848 0.0907
-4.750 -0.5519 0.01013 0.00353 0.0035 0.9821 0.1119
-4.500 -0.5212 0.00980 0.00331 0.0028 0.9785 0.1353
-4.250 -0.4905 0.00953 0.00311 0.0021 0.9743 0.1562
-4.000 -0.4564 0.00925 0.00292 0.0007 0.9710 0.1771
-3.750 -0.4249 0.00900 0.00274 -0.0001 0.9638 0.1968
-3.500 -0.3878 0.00873 0.00255 -0.0021 0.9593 0.2202
-3.250 -0.3569 0.00851 0.00241 -0.0028 0.9526 0.2400
-3.000 -0.3222 0.00827 0.00226 -0.0043 0.9464 0.2647
-2.750 -0.2894 0.00802 0.00212 -0.0053 0.9365 0.2940
-2.500 -0.2554 0.00778 0.00197 -0.0066 0.9246 0.3234
-2.250 -0.2235 0.00756 0.00185 -0.0074 0.9106 0.3549
-2.000 -0.1936 0.00737 0.00173 -0.0078 0.8938 0.3854
-1.750 -0.1651 0.00721 0.00163 -0.0077 0.8733 0.4152
-1.500 -0.1383 0.00706 0.00153 -0.0074 0.8510 0.4474
-1.250 -0.1130 0.00694 0.00145 -0.0066 0.8242 0.4791
-1.000 -0.0892 0.00683 0.00137 -0.0056 0.7942 0.5153
-0.750 -0.0661 0.00676 0.00132 -0.0043 0.7626 0.5523
-0.500 -0.0438 0.00672 0.00128 -0.0030 0.7291 0.5885
-0.250 -0.0217 0.00670 0.00125 -0.0015 0.6947 0.6230
0.000 0.0001 0.00670 0.00124 0.0000 0.6579 0.6570
0.250 0.0217 0.00670 0.00125 0.0015 0.6220 0.6944
0.750 0.0661 0.00677 0.00132 0.0043 0.5518 0.7619
1.000 0.0892 0.00682 0.00138 0.0056 0.5172 0.7964
1.250 0.1131 0.00694 0.00145 0.0066 0.4797 0.8247
1.500 0.1382 0.00706 0.00153 0.0074 0.4468 0.8509
1.750 0.1651 0.00721 0.00163 0.0078 0.4145 0.8734
2.000 0.1936 0.00737 0.00173 0.0078 0.3855 0.8939
2.250 0.2234 0.00757 0.00185 0.0074 0.3535 0.9109
2.750 0.2894 0.00801 0.00211 0.0053 0.2950 0.9364
3.000 0.3221 0.00827 0.00226 0.0043 0.2646 0.9463
3.250 0.3569 0.00851 0.00241 0.0028 0.2411 0.9525
3.500 0.3879 0.00874 0.00256 0.0021 0.2192 0.9593
3.750 0.4249 0.00900 0.00274 0.0001 0.1958 0.9638
4.000 0.4564 0.00925 0.00292 -0.0007 0.1766 0.9709
4.250 0.4905 0.00953 0.00311 -0.0021 0.1554 0.9744
4.500 0.5214 0.00980 0.00331 -0.0028 0.1354 0.9786
4.750 0.5521 0.01013 0.00353 -0.0035 0.1131 0.9821
5.000 0.5841 0.01047 0.00378 -0.0046 0.0913 0.9848
5.250 0.6146 0.01084 0.00406 -0.0053 0.0742 0.9884
5.500 0.6468 0.01119 0.00435 -0.0064 0.0616 0.9911
5.750 0.6791 0.01152 0.00466 -0.0075 0.0527 0.9941
6.000 0.7114 0.01185 0.00499 -0.0086 0.0466 0.9973
6.250 0.7440 0.01224 0.00534 -0.0098 0.0404 0.9997
6.500 0.7664 0.01250 0.00564 -0.0088 0.0377 1.0000
6.750 0.7865 0.01282 0.00596 -0.0073 0.0349 1.0000
7.000 0.8060 0.01322 0.00636 -0.0057 0.0322 1.0000
7.250 0.8266 0.01351 0.00671 -0.0043 0.0306 1.0000
7.500 0.8471 0.01384 0.00707 -0.0029 0.0286 1.0000
7.750 0.8670 0.01425 0.00748 -0.0014 0.0267 1.0000
8.000 0.8869 0.01468 0.00794 0.0000 0.0250 1.0000
8.250 0.9076 0.01504 0.00835 0.0014 0.0237 1.0000
8.500 0.9280 0.01545 0.00880 0.0027 0.0223 1.0000
8.750 0.9479 0.01591 0.00929 0.0041 0.0211 1.0000
9.000 0.9667 0.01649 0.00990 0.0056 0.0200 1.0000
9.250 0.9868 0.01695 0.01044 0.0070 0.0192 1.0000
9.500 1.0070 0.01741 0.01096 0.0083 0.0182 1.0000
9.750 1.0267 0.01791 0.01151 0.0096 0.0173 1.0000
10.000 1.0457 0.01848 0.01211 0.0110 0.0164 1.0000
10.250 1.0633 0.01916 0.01284 0.0125 0.0156 1.0000
10.500 1.0816 0.01977 0.01356 0.0140 0.0151 1.0000
10.750 1.0996 0.02039 0.01426 0.0155 0.0144 1.0000
11.000 1.1168 0.02106 0.01501 0.0170 0.0138 1.0000
11.250 1.1336 0.02173 0.01575 0.0185 0.0133 1.0000
11.500 1.1489 0.02251 0.01659 0.0202 0.0129 1.0000
11.750 1.1623 0.02340 0.01755 0.0221 0.0124 1.0000
12.000 1.1735 0.02441 0.01865 0.0242 0.0120 1.0000
12.250 1.1855 0.02533 0.01970 0.0262 0.0117 1.0000
12.500 1.1934 0.02629 0.02077 0.0288 0.0115 1.0000
12.750 1.2008 0.02726 0.02185 0.0313 0.0111 1.0000
13.000 1.2091 0.02825 0.02294 0.0334 0.0107 1.0000
13.250 1.2123 0.02967 0.02448 0.0356 0.0106 1.0000
13.500 1.2198 0.03088 0.02579 0.0370 0.0103 1.0000
13.750 1.2217 0.03266 0.02768 0.0383 0.0101 1.0000
14.000 1.2244 0.03452 0.02965 0.0391 0.0099 1.0000
14.250 1.2240 0.03691 0.03216 0.0393 0.0097 1.0000
14.500 1.2202 0.04000 0.03540 0.0387 0.0097 1.0000
14.750 1.2142 0.04381 0.03934 0.0370 0.0095 1.0000
15.000 1.2004 0.04929 0.04499 0.0338 0.0093 1.0000
15.250 1.1897 0.05481 0.05067 0.0302 0.0093 1.0000
15.750 1.1537 0.06901 0.06519 0.0212 0.0093 1.0000
16.000 1.1271 0.07765 0.07396 0.0162 0.0092 1.0000
16.250 1.1086 0.08488 0.08134 0.0122 0.0093 1.0000
16.500 1.0810 0.09370 0.09029 0.0074 0.0093 1.0000
16.750 1.0559 0.10233 0.09907 0.0028 0.0095 1.0000
17.000 1.0300 0.11145 0.10830 -0.0020 0.0095 1.0000
17.250 1.0046 0.12077 0.11774 -0.0069 0.0095 1.0000
17.500 0.9743 0.13152 0.12863 -0.0125 0.0096 1.0000
17.750 0.9430 0.14307 0.14031 -0.0185 0.0095 1.0000
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