Eiffel 385 (S.T. Ae) (eiffel385-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: Eiffel 385 (S.T. Ae) (eiffel385-il) Reynolds number: 1,000,000 Max Cl/Cd: 123.41 at α=2.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-eiffel385-il-1000000.txt Download as CSV file: xf-eiffel385-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: Eiffel 385 (S.T. Ae)
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
------ -------- --------- --------- -------- -------- --------
-19.750 -0.8357 0.08945 0.08659 -0.0724 1.0000 0.0266
-19.500 -0.8391 0.08593 0.08304 -0.0741 1.0000 0.0270
-19.250 -0.8425 0.08238 0.07947 -0.0758 1.0000 0.0272
-19.000 -0.8492 0.07838 0.07543 -0.0779 1.0000 0.0274
-18.750 -0.8551 0.07458 0.07161 -0.0798 1.0000 0.0277
-18.500 -0.8622 0.07073 0.06774 -0.0817 1.0000 0.0278
-18.250 -0.8745 0.06631 0.06326 -0.0841 1.0000 0.0280
-18.000 -0.8882 0.06204 0.05895 -0.0863 1.0000 0.0282
-17.750 -0.9091 0.05717 0.05403 -0.0889 1.0000 0.0283
-17.500 -0.9361 0.05194 0.04875 -0.0914 1.0000 0.0283
-17.250 -0.9819 0.04579 0.04254 -0.0935 1.0000 0.0282
-17.000 -1.0736 0.03326 0.02977 -0.1022 0.9987 0.0277
-16.750 -1.0499 0.02823 0.02454 -0.1099 0.9963 0.0280
-16.500 -1.0222 0.02618 0.02238 -0.1131 0.9943 0.0286
-16.250 -0.9944 0.02458 0.02068 -0.1154 0.9925 0.0290
-16.000 -0.9683 0.02333 0.01933 -0.1165 0.9895 0.0294
-15.750 -0.9398 0.02219 0.01809 -0.1179 0.9869 0.0298
-15.500 -0.9087 0.02129 0.01711 -0.1192 0.9850 0.0302
-15.250 -0.8781 0.02019 0.01590 -0.1208 0.9833 0.0306
-15.000 -0.8483 0.01874 0.01438 -0.1226 0.9819 0.0314
-14.750 -0.8252 0.01786 0.01344 -0.1221 0.9771 0.0319
-14.500 -0.7962 0.01709 0.01261 -0.1227 0.9744 0.0324
-14.250 -0.7652 0.01639 0.01185 -0.1235 0.9725 0.0330
-14.000 -0.7329 0.01577 0.01117 -0.1245 0.9710 0.0337
-13.750 -0.6995 0.01519 0.01053 -0.1255 0.9697 0.0343
-13.500 -0.6695 0.01470 0.00997 -0.1259 0.9669 0.0348
-13.250 -0.6427 0.01410 0.00930 -0.1256 0.9622 0.0353
-13.000 -0.6126 0.01333 0.00848 -0.1262 0.9589 0.0364
-12.750 -0.5795 0.01277 0.00787 -0.1272 0.9562 0.0373
-12.500 -0.5494 0.01233 0.00738 -0.1274 0.9517 0.0382
-12.250 -0.5208 0.01195 0.00696 -0.1273 0.9454 0.0393
-12.000 -0.4878 0.01158 0.00652 -0.1280 0.9409 0.0402
-11.750 -0.4609 0.01108 0.00598 -0.1277 0.9338 0.0420
-11.500 -0.4316 0.01068 0.00554 -0.1277 0.9267 0.0439
-11.250 -0.4030 0.01038 0.00518 -0.1275 0.9191 0.0458
-11.000 -0.3762 0.00996 0.00474 -0.1270 0.9103 0.0503
-10.750 -0.3499 0.00956 0.00434 -0.1264 0.9020 0.0587
-10.500 -0.3239 0.00917 0.00403 -0.1258 0.8928 0.0757
-10.250 -0.2968 0.00902 0.00388 -0.1252 0.8835 0.0853
-10.000 -0.2695 0.00888 0.00374 -0.1247 0.8732 0.0914
-9.750 -0.2422 0.00884 0.00364 -0.1240 0.8625 0.0946
-9.500 -0.2156 0.00870 0.00344 -0.1234 0.8510 0.0981
-9.250 -0.1893 0.00859 0.00329 -0.1226 0.8374 0.1014
-9.000 -0.1629 0.00852 0.00315 -0.1218 0.8220 0.1041
-8.750 -0.1367 0.00848 0.00303 -0.1210 0.8047 0.1059
-8.500 -0.1112 0.00844 0.00288 -0.1201 0.7846 0.1079
-8.250 -0.0865 0.00834 0.00269 -0.1191 0.7619 0.1113
-8.000 -0.0618 0.00829 0.00256 -0.1181 0.7378 0.1142
-7.750 -0.0369 0.00829 0.00244 -0.1171 0.7152 0.1165
-7.250 0.0143 0.00825 0.00222 -0.1154 0.6810 0.1220
-7.000 0.0404 0.00817 0.00212 -0.1147 0.6691 0.1264
-6.750 0.0665 0.00813 0.00203 -0.1141 0.6587 0.1304
-6.500 0.0933 0.00807 0.00194 -0.1135 0.6496 0.1358
-6.250 0.1195 0.00801 0.00188 -0.1129 0.6403 0.1452
-6.000 0.1464 0.00795 0.00187 -0.1124 0.6319 0.1615
-5.750 0.1732 0.00799 0.00189 -0.1118 0.6244 0.1738
-5.500 0.2012 0.00797 0.00190 -0.1115 0.6195 0.1819
-5.250 0.2290 0.00801 0.00192 -0.1112 0.6139 0.1876
-5.000 0.2565 0.00809 0.00194 -0.1108 0.6083 0.1905
-4.750 0.2839 0.00803 0.00190 -0.1104 0.6036 0.1957
-4.500 0.3118 0.00803 0.00191 -0.1101 0.5987 0.1998
-4.250 0.3393 0.00806 0.00192 -0.1098 0.5937 0.2028
-4.000 0.3664 0.00812 0.00193 -0.1094 0.5884 0.2051
-3.750 0.3946 0.00813 0.00193 -0.1092 0.5843 0.2065
-3.500 0.4219 0.00808 0.00189 -0.1089 0.5794 0.2094
-3.250 0.4489 0.00806 0.00186 -0.1085 0.5743 0.2125
-3.000 0.4758 0.00808 0.00187 -0.1081 0.5693 0.2151
-2.750 0.5036 0.00805 0.00187 -0.1079 0.5645 0.2174
-2.500 0.5309 0.00806 0.00187 -0.1076 0.5591 0.2195
-2.250 0.5577 0.00811 0.00188 -0.1072 0.5537 0.2216
-2.000 0.5853 0.00811 0.00190 -0.1069 0.5486 0.2231
-1.750 0.6125 0.00811 0.00190 -0.1066 0.5425 0.2255
-1.500 0.6387 0.00812 0.00190 -0.1062 0.5363 0.2294
-1.250 0.6659 0.00811 0.00192 -0.1059 0.5307 0.2322
-1.000 0.6927 0.00813 0.00194 -0.1056 0.5236 0.2348
-0.750 0.7189 0.00818 0.00197 -0.1051 0.5164 0.2373
-0.500 0.7459 0.00820 0.00200 -0.1049 0.5083 0.2397
-0.250 0.7716 0.00827 0.00204 -0.1044 0.4985 0.2422
0.000 0.7977 0.00829 0.00208 -0.1040 0.4881 0.2488
0.250 0.8231 0.00835 0.00214 -0.1034 0.4766 0.2562
0.500 0.8478 0.00843 0.00222 -0.1028 0.4629 0.2690
0.750 0.8719 0.00849 0.00233 -0.1021 0.4492 0.3016
1.000 0.8964 0.00854 0.00247 -0.1015 0.4356 0.3504
1.250 0.9210 0.00865 0.00260 -0.1008 0.4228 0.3761
1.500 0.9449 0.00880 0.00273 -0.1001 0.4078 0.3933
1.750 0.9682 0.00897 0.00288 -0.0993 0.3913 0.4078
2.000 0.9912 0.00916 0.00303 -0.0984 0.3749 0.4228
2.250 1.0140 0.00933 0.00319 -0.0976 0.3600 0.4428
2.500 1.0355 0.00941 0.00339 -0.0965 0.3471 0.5065
2.750 1.1008 0.00892 0.00386 -0.1054 0.3299 1.0000
3.000 1.1237 0.00915 0.00404 -0.1045 0.3186 1.0000
3.250 1.1467 0.00937 0.00422 -0.1037 0.3078 1.0000
3.500 1.1688 0.00963 0.00442 -0.1028 0.2970 1.0000
3.750 1.1913 0.00987 0.00461 -0.1019 0.2862 1.0000
4.000 1.2135 0.01011 0.00482 -0.1010 0.2756 1.0000
4.250 1.2346 0.01040 0.00505 -0.0999 0.2641 1.0000
4.500 1.2558 0.01068 0.00528 -0.0989 0.2523 1.0000
4.750 1.2761 0.01099 0.00554 -0.0977 0.2385 1.0000
5.000 1.2938 0.01141 0.00585 -0.0961 0.2201 1.0000
5.250 1.3085 0.01188 0.00621 -0.0938 0.1978 1.0000
5.500 1.3160 0.01262 0.00673 -0.0904 0.1629 1.0000
5.750 1.3167 0.01370 0.00753 -0.0859 0.1194 1.0000
6.000 1.3215 0.01467 0.00830 -0.0823 0.0879 1.0000
6.250 1.3300 0.01551 0.00901 -0.0795 0.0686 1.0000
6.500 1.3441 0.01611 0.00957 -0.0776 0.0626 1.0000
6.750 1.3591 0.01667 0.01013 -0.0760 0.0598 1.0000
7.000 1.3732 0.01730 0.01076 -0.0742 0.0570 1.0000
7.250 1.3884 0.01788 0.01137 -0.0727 0.0552 1.0000
7.500 1.4046 0.01842 0.01195 -0.0715 0.0538 1.0000
7.750 1.4190 0.01908 0.01263 -0.0701 0.0522 1.0000
8.000 1.4321 0.01984 0.01341 -0.0686 0.0507 1.0000
8.250 1.4430 0.02075 0.01434 -0.0669 0.0491 1.0000
8.500 1.4552 0.02162 0.01526 -0.0655 0.0480 1.0000
8.750 1.4696 0.02237 0.01605 -0.0644 0.0474 1.0000
9.000 1.4831 0.02320 0.01693 -0.0633 0.0466 1.0000
9.250 1.4957 0.02411 0.01788 -0.0622 0.0456 1.0000
9.500 1.5068 0.02517 0.01897 -0.0610 0.0447 1.0000
9.750 1.5164 0.02637 0.02021 -0.0599 0.0437 1.0000
10.000 1.5230 0.02785 0.02173 -0.0586 0.0427 1.0000
10.250 1.5276 0.02956 0.02351 -0.0573 0.0417 1.0000
10.500 1.5403 0.03065 0.02465 -0.0568 0.0411 1.0000
10.750 1.5507 0.03196 0.02602 -0.0561 0.0405 1.0000
11.000 1.5603 0.03338 0.02749 -0.0555 0.0396 1.0000
11.250 1.5685 0.03498 0.02914 -0.0549 0.0389 1.0000
11.500 1.5757 0.03670 0.03090 -0.0544 0.0380 1.0000
11.750 1.5800 0.03876 0.03299 -0.0539 0.0372 1.0000
12.000 1.5784 0.04150 0.03580 -0.0534 0.0362 1.0000
12.250 1.5859 0.04336 0.03772 -0.0532 0.0357 1.0000
12.500 1.5940 0.04515 0.03958 -0.0530 0.0350 1.0000
12.750 1.6011 0.04708 0.04157 -0.0530 0.0341 1.0000
13.000 1.6047 0.04942 0.04396 -0.0528 0.0334 1.0000
13.250 1.6087 0.05172 0.04630 -0.0528 0.0325 1.0000
13.500 1.6073 0.05469 0.04931 -0.0528 0.0316 1.0000
13.750 1.6068 0.05757 0.05227 -0.0528 0.0308 1.0000
14.000 1.6102 0.06005 0.05482 -0.0530 0.0301 1.0000
14.250 1.6123 0.06269 0.05753 -0.0531 0.0292 1.0000
14.500 1.6122 0.06565 0.06054 -0.0534 0.0284 1.0000
14.750 1.6097 0.06894 0.06387 -0.0537 0.0275 1.0000
15.000 1.6022 0.07292 0.06791 -0.0542 0.0267 1.0000
15.250 1.6015 0.07608 0.07115 -0.0546 0.0260 1.0000
15.500 1.5998 0.07940 0.07455 -0.0552 0.0252 1.0000
15.750 1.5954 0.08310 0.07831 -0.0558 0.0244 1.0000
16.000 1.5887 0.08717 0.08244 -0.0566 0.0237 1.0000
16.250 1.5787 0.09176 0.08709 -0.0575 0.0230 1.0000
16.500 1.5726 0.09586 0.09128 -0.0585 0.0223 1.0000
16.750 1.5666 0.09991 0.09542 -0.0595 0.0218 1.0000
17.000 1.5593 0.10420 0.09978 -0.0606 0.0212 1.0000
17.250 1.5513 0.10863 0.10428 -0.0618 0.0205 1.0000
17.500 1.5413 0.11342 0.10913 -0.0632 0.0200 1.0000
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