EPPLER 604 AIRFOIL (e604-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: EPPLER 604 AIRFOIL (e604-il) Reynolds number: 1,000,000 Max Cl/Cd: 123.77 at α=5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-e604-il-1000000-n5.txt Download as CSV file: xf-e604-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: EPPLER 604 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.750 -0.5762 0.13523 0.13297 -0.0600 1.0000 0.0033
-18.500 -0.6222 0.12191 0.11949 -0.0660 1.0000 0.0032
-18.250 -0.6515 0.11248 0.10994 -0.0702 1.0000 0.0031
-18.000 -0.6939 0.10075 0.09805 -0.0757 1.0000 0.0031
-17.750 -0.7265 0.09107 0.08823 -0.0803 1.0000 0.0031
-17.500 -0.7593 0.08014 0.07709 -0.0872 0.9996 0.0031
-17.250 -0.7699 0.07302 0.06984 -0.0927 0.9989 0.0030
-17.000 -0.7818 0.06600 0.06266 -0.0980 0.9979 0.0030
-16.750 -0.7901 0.05995 0.05646 -0.1027 0.9961 0.0030
-16.500 -0.7893 0.05611 0.05253 -0.1052 0.9925 0.0030
-16.250 -0.7978 0.05120 0.04748 -0.1082 0.9884 0.0030
-16.000 -0.8086 0.04621 0.04231 -0.1111 0.9828 0.0031
-15.500 -0.7907 0.04065 0.03655 -0.1159 0.9575 0.0031
-15.250 -0.7621 0.03776 0.03352 -0.1222 0.9461 0.0031
-15.000 -0.7279 0.03465 0.03025 -0.1301 0.9371 0.0032
-14.750 -0.6882 0.03177 0.02718 -0.1388 0.9220 0.0033
-14.500 -0.6592 0.03001 0.02519 -0.1433 0.8947 0.0034
-14.250 -0.6499 0.02877 0.02376 -0.1431 0.8693 0.0034
-14.000 -0.6413 0.02777 0.02262 -0.1421 0.8512 0.0034
-13.750 -0.6349 0.02664 0.02137 -0.1410 0.8371 0.0035
-13.500 -0.6267 0.02565 0.02025 -0.1398 0.8252 0.0034
-13.250 -0.6164 0.02478 0.01930 -0.1388 0.8148 0.0035
-13.000 -0.6054 0.02394 0.01838 -0.1378 0.8061 0.0035
-12.750 -0.5957 0.02306 0.01740 -0.1366 0.7973 0.0036
-12.500 -0.5837 0.02227 0.01654 -0.1355 0.7898 0.0037
-12.250 -0.5710 0.02158 0.01578 -0.1344 0.7821 0.0039
-12.000 -0.5586 0.02085 0.01497 -0.1333 0.7749 0.0039
-11.750 -0.5454 0.02019 0.01425 -0.1322 0.7678 0.0038
-11.500 -0.5319 0.01956 0.01355 -0.1310 0.7614 0.0039
-11.250 -0.5176 0.01895 0.01287 -0.1299 0.7555 0.0040
-11.000 -0.5033 0.01837 0.01224 -0.1288 0.7497 0.0042
-10.750 -0.4881 0.01784 0.01165 -0.1277 0.7448 0.0045
-10.500 -0.4727 0.01731 0.01107 -0.1266 0.7398 0.0045
-10.250 -0.4572 0.01682 0.01053 -0.1254 0.7346 0.0045
-10.000 -0.4439 0.01624 0.00989 -0.1239 0.7297 0.0048
-9.750 -0.4286 0.01572 0.00935 -0.1227 0.7251 0.0051
-9.500 -0.4132 0.01526 0.00885 -0.1214 0.7202 0.0052
-9.250 -0.3983 0.01483 0.00837 -0.1200 0.7158 0.0057
-9.000 -0.3835 0.01439 0.00790 -0.1185 0.7121 0.0058
-8.750 -0.3694 0.01398 0.00746 -0.1168 0.7082 0.0063
-8.500 -0.3590 0.01363 0.00707 -0.1144 0.7040 0.0066
-8.250 -0.3436 0.01327 0.00668 -0.1130 0.6999 0.0073
-8.000 -0.3246 0.01296 0.00634 -0.1120 0.6964 0.0083
-7.750 -0.3043 0.01265 0.00602 -0.1112 0.6930 0.0093
-7.500 -0.2829 0.01238 0.00573 -0.1106 0.6896 0.0105
-7.250 -0.2612 0.01211 0.00545 -0.1099 0.6863 0.0124
-7.000 -0.2387 0.01187 0.00519 -0.1094 0.6830 0.0144
-6.750 -0.2152 0.01163 0.00494 -0.1091 0.6801 0.0169
-6.500 -0.1911 0.01139 0.00470 -0.1088 0.6771 0.0197
-6.250 -0.1667 0.01116 0.00447 -0.1086 0.6739 0.0229
-6.000 -0.1421 0.01093 0.00425 -0.1084 0.6710 0.0281
-5.750 -0.1177 0.01069 0.00403 -0.1082 0.6681 0.0362
-5.500 -0.0929 0.01045 0.00382 -0.1081 0.6652 0.0472
-5.250 -0.0674 0.01016 0.00362 -0.1082 0.6628 0.0629
-5.000 -0.0416 0.00988 0.00342 -0.1083 0.6600 0.0819
-4.750 -0.0155 0.00962 0.00323 -0.1084 0.6572 0.1034
-4.500 0.0107 0.00935 0.00304 -0.1086 0.6544 0.1292
-4.250 0.0369 0.00907 0.00286 -0.1088 0.6515 0.1640
-4.000 0.0635 0.00876 0.00267 -0.1091 0.6490 0.2054
-3.750 0.0905 0.00826 0.00244 -0.1097 0.6467 0.2784
-3.500 0.1178 0.00764 0.00216 -0.1105 0.6442 0.3760
-3.250 0.1459 0.00699 0.00190 -0.1115 0.6415 0.4908
-3.000 0.1750 0.00683 0.00186 -0.1121 0.6388 0.5400
-2.750 0.2040 0.00682 0.00184 -0.1125 0.6361 0.5575
-2.250 0.2624 0.00682 0.00184 -0.1134 0.6313 0.5823
-2.000 0.2919 0.00683 0.00184 -0.1139 0.6289 0.5946
-1.750 0.3212 0.00685 0.00187 -0.1144 0.6262 0.6057
-1.500 0.3502 0.00688 0.00190 -0.1148 0.6235 0.6140
-1.250 0.3791 0.00693 0.00193 -0.1151 0.6209 0.6200
-1.000 0.4078 0.00698 0.00193 -0.1155 0.6181 0.6226
-0.750 0.4370 0.00701 0.00192 -0.1159 0.6157 0.6241
-0.500 0.4663 0.00702 0.00193 -0.1164 0.6131 0.6255
-0.250 0.4952 0.00703 0.00194 -0.1168 0.6102 0.6272
0.000 0.5238 0.00706 0.00196 -0.1172 0.6073 0.6290
0.250 0.5522 0.00710 0.00198 -0.1175 0.6042 0.6307
0.500 0.5803 0.00715 0.00201 -0.1177 0.6012 0.6324
0.750 0.6094 0.00717 0.00204 -0.1182 0.5986 0.6340
1.000 0.6381 0.00720 0.00207 -0.1186 0.5954 0.6356
1.250 0.6665 0.00724 0.00210 -0.1189 0.5920 0.6372
1.500 0.6944 0.00730 0.00214 -0.1191 0.5884 0.6389
1.750 0.7221 0.00737 0.00218 -0.1193 0.5849 0.6405
2.000 0.7506 0.00740 0.00223 -0.1197 0.5812 0.6421
2.250 0.7783 0.00744 0.00228 -0.1199 0.5763 0.6438
2.500 0.8051 0.00751 0.00234 -0.1199 0.5712 0.6454
2.750 0.8326 0.00756 0.00241 -0.1200 0.5664 0.6471
3.000 0.8598 0.00762 0.00247 -0.1202 0.5606 0.6488
3.250 0.8855 0.00772 0.00255 -0.1200 0.5543 0.6506
3.500 0.9126 0.00779 0.00263 -0.1200 0.5478 0.6524
3.750 0.9379 0.00790 0.00272 -0.1198 0.5402 0.6543
4.000 0.9639 0.00799 0.00281 -0.1197 0.5331 0.6561
4.250 0.9882 0.00812 0.00291 -0.1192 0.5244 0.6577
4.500 1.0130 0.00823 0.00303 -0.1189 0.5157 0.6596
4.750 1.0358 0.00839 0.00316 -0.1181 0.5057 0.6614
5.000 1.0582 0.00855 0.00331 -0.1173 0.4940 0.6633
5.250 1.0788 0.00872 0.00346 -0.1161 0.4823 0.6652
5.500 1.0975 0.00892 0.00363 -0.1146 0.4702 0.6672
5.750 1.1149 0.00916 0.00384 -0.1128 0.4565 0.6692
6.000 1.1315 0.00946 0.00408 -0.1109 0.4406 0.6712
6.250 1.1478 0.00979 0.00436 -0.1090 0.4252 0.6731
6.500 1.1621 0.01018 0.00468 -0.1068 0.4063 0.6750
6.750 1.1756 0.01059 0.00505 -0.1045 0.3876 0.6774
7.000 1.1877 0.01107 0.00546 -0.1020 0.3682 0.6797
7.250 1.1986 0.01160 0.00592 -0.0994 0.3495 0.6819
7.500 1.2098 0.01214 0.00640 -0.0969 0.3310 0.6842
7.750 1.2199 0.01275 0.00694 -0.0943 0.3125 0.6865
8.000 1.2291 0.01341 0.00754 -0.0917 0.2944 0.6887
8.250 1.2378 0.01415 0.00820 -0.0890 0.2769 0.6906
8.500 1.2460 0.01493 0.00893 -0.0865 0.2602 0.6928
8.750 1.2549 0.01573 0.00970 -0.0841 0.2451 0.6952
9.000 1.2612 0.01669 0.01060 -0.0815 0.2277 0.6977
9.250 1.2695 0.01762 0.01149 -0.0793 0.2134 0.7005
9.500 1.2779 0.01859 0.01242 -0.0772 0.1998 0.7032
9.750 1.2852 0.01965 0.01344 -0.0751 0.1857 0.7057
10.000 1.2917 0.02082 0.01455 -0.0730 0.1713 0.7079
10.250 1.3000 0.02192 0.01563 -0.0713 0.1602 0.7103
10.500 1.3065 0.02316 0.01685 -0.0694 0.1477 0.7129
10.750 1.3138 0.02441 0.01807 -0.0677 0.1371 0.7155
11.000 1.3226 0.02561 0.01926 -0.0662 0.1272 0.7182
11.250 1.3302 0.02691 0.02055 -0.0647 0.1176 0.7208
11.500 1.3359 0.02839 0.02200 -0.0631 0.1069 0.7233
11.750 1.3429 0.02983 0.02341 -0.0617 0.0979 0.7258
12.000 1.3509 0.03124 0.02482 -0.0605 0.0898 0.7287
12.250 1.3585 0.03271 0.02630 -0.0593 0.0831 0.7319
12.500 1.3669 0.03415 0.02775 -0.0583 0.0767 0.7351
12.750 1.3742 0.03573 0.02934 -0.0572 0.0704 0.7381
13.000 1.3820 0.03731 0.03091 -0.0563 0.0648 0.7408
13.250 1.3902 0.03888 0.03251 -0.0554 0.0601 0.7436
13.500 1.3959 0.04069 0.03432 -0.0545 0.0540 0.7467
13.750 1.4040 0.04235 0.03601 -0.0538 0.0496 0.7500
14.000 1.4100 0.04424 0.03791 -0.0531 0.0450 0.7533
14.250 1.4161 0.04615 0.03983 -0.0524 0.0400 0.7564
14.500 1.4228 0.04804 0.04175 -0.0518 0.0367 0.7598
14.750 1.4278 0.05013 0.04386 -0.0513 0.0325 0.7636
15.000 1.4330 0.05226 0.04602 -0.0508 0.0285 0.7677
15.250 1.4385 0.05440 0.04819 -0.0504 0.0260 0.7718
15.500 1.4430 0.05669 0.05051 -0.0501 0.0225 0.7754
15.750 1.4483 0.05892 0.05278 -0.0498 0.0204 0.7796
16.000 1.4532 0.06125 0.05516 -0.0496 0.0184 0.7840
16.250 1.4580 0.06363 0.05759 -0.0496 0.0165 0.7885
16.500 1.4629 0.06605 0.06007 -0.0495 0.0152 0.7930
16.750 1.4674 0.06855 0.06263 -0.0496 0.0141 0.7982
17.000 1.4721 0.07106 0.06522 -0.0497 0.0131 0.8042
17.250 1.4750 0.07383 0.06805 -0.0499 0.0117 0.8101
17.500 1.4787 0.07654 0.07085 -0.0502 0.0109 0.8175
17.750 1.4830 0.07922 0.07361 -0.0506 0.0103 0.8250
18.000 1.4847 0.08228 0.07676 -0.0510 0.0096 0.8336
18.250 1.4873 0.08524 0.07980 -0.0515 0.0089 0.8433
18.750 1.4901 0.09150 0.08628 -0.0527 0.0078 0.8708
19.000 1.4888 0.09480 0.08971 -0.0531 0.0072 0.9008
19.250 1.4878 0.09787 0.09296 -0.0536 0.0069 1.0000
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