AS5048 (18%) (as5048-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: AS5048 (18%) (as5048-il) Reynolds number: 1,000,000 Max Cl/Cd: 96.54 at α=4.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-as5048-il-1000000.txt Download as CSV file: xf-as5048-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: AS5048 (18%)
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
------ -------- --------- --------- -------- -------- --------
-17.000 -0.7696 0.11033 0.10802 -0.0397 1.0000 0.0080
-16.750 -0.8070 0.09867 0.09618 -0.0459 1.0000 0.0080
-16.500 -0.8368 0.08933 0.08666 -0.0506 1.0000 0.0079
-16.250 -0.8618 0.08151 0.07866 -0.0542 1.0000 0.0079
-16.000 -0.8836 0.07478 0.07176 -0.0568 1.0000 0.0079
-15.750 -0.9024 0.06899 0.06580 -0.0586 1.0000 0.0078
-15.500 -0.9193 0.06382 0.06045 -0.0597 1.0000 0.0078
-15.250 -0.9322 0.05952 0.05600 -0.0602 1.0000 0.0079
-15.000 -0.9444 0.05551 0.05182 -0.0602 1.0000 0.0079
-14.750 -0.9441 0.05137 0.04750 -0.0626 0.9989 0.0079
-14.500 -0.9371 0.04758 0.04352 -0.0655 0.9944 0.0079
-14.250 -0.9194 0.04386 0.03958 -0.0700 0.9411 0.0080
-14.000 -0.8620 0.03967 0.03470 -0.0837 0.8368 0.0081
-13.750 -0.8589 0.03821 0.03292 -0.0825 0.7912 0.0081
-13.500 -0.8573 0.03572 0.03019 -0.0807 0.7787 0.0082
-13.250 -0.8505 0.03398 0.02829 -0.0794 0.7697 0.0083
-13.000 -0.8408 0.03257 0.02679 -0.0785 0.7636 0.0084
-12.750 -0.8294 0.03135 0.02550 -0.0778 0.7581 0.0086
-12.500 -0.8171 0.03024 0.02430 -0.0771 0.7532 0.0087
-12.250 -0.8039 0.02917 0.02318 -0.0765 0.7498 0.0088
-12.000 -0.7899 0.02815 0.02211 -0.0759 0.7467 0.0089
-11.750 -0.7753 0.02720 0.02109 -0.0753 0.7437 0.0091
-11.500 -0.7599 0.02631 0.02014 -0.0747 0.7409 0.0093
-11.250 -0.7444 0.02543 0.01919 -0.0741 0.7381 0.0096
-11.000 -0.7283 0.02461 0.01830 -0.0735 0.7352 0.0098
-10.750 -0.7118 0.02377 0.01740 -0.0729 0.7334 0.0101
-10.500 -0.6950 0.02295 0.01654 -0.0723 0.7316 0.0103
-10.250 -0.6770 0.02224 0.01577 -0.0718 0.7297 0.0104
-10.000 -0.6666 0.02097 0.01445 -0.0704 0.7277 0.0107
-9.750 -0.6535 0.01994 0.01339 -0.0694 0.7256 0.0110
-9.500 -0.6372 0.01914 0.01256 -0.0687 0.7236 0.0113
-9.250 -0.6197 0.01844 0.01183 -0.0682 0.7217 0.0116
-9.000 -0.6022 0.01776 0.01110 -0.0675 0.7197 0.0119
-8.750 -0.5844 0.01713 0.01042 -0.0668 0.7175 0.0123
-8.500 -0.5667 0.01652 0.00978 -0.0660 0.7165 0.0127
-8.250 -0.5480 0.01601 0.00925 -0.0651 0.7152 0.0131
-8.000 -0.5380 0.01528 0.00847 -0.0627 0.7138 0.0136
-7.750 -0.5236 0.01475 0.00792 -0.0609 0.7123 0.0141
-7.500 -0.5035 0.01434 0.00750 -0.0600 0.7107 0.0148
-7.250 -0.4823 0.01398 0.00711 -0.0593 0.7091 0.0155
-7.000 -0.4590 0.01371 0.00682 -0.0588 0.7077 0.0162
-6.750 -0.4398 0.01318 0.00626 -0.0577 0.7063 0.0173
-6.500 -0.4165 0.01288 0.00594 -0.0572 0.7049 0.0184
-6.250 -0.3922 0.01262 0.00566 -0.0569 0.7034 0.0194
-6.000 -0.3688 0.01230 0.00530 -0.0565 0.7016 0.0210
-5.750 -0.3438 0.01206 0.00505 -0.0562 0.7000 0.0228
-5.500 -0.3192 0.01177 0.00478 -0.0559 0.6990 0.0256
-5.250 -0.2945 0.01147 0.00451 -0.0556 0.6980 0.0318
-5.000 -0.2789 0.01046 0.00394 -0.0541 0.6968 0.1250
-4.750 -0.2650 0.00918 0.00332 -0.0526 0.6954 0.2762
-4.500 -0.2469 0.00804 0.00278 -0.0517 0.6939 0.4199
-4.250 -0.2242 0.00727 0.00252 -0.0514 0.6924 0.5483
-4.000 -0.1951 0.00723 0.00255 -0.0517 0.6910 0.5820
-3.750 -0.1654 0.00726 0.00257 -0.0522 0.6895 0.5974
-3.500 -0.1356 0.00733 0.00262 -0.0526 0.6879 0.6095
-3.250 -0.1055 0.00742 0.00267 -0.0531 0.6863 0.6168
-3.000 -0.0752 0.00750 0.00270 -0.0537 0.6843 0.6217
-2.750 -0.0452 0.00760 0.00281 -0.0542 0.6826 0.6276
-2.500 -0.0155 0.00767 0.00286 -0.0547 0.6814 0.6328
-2.250 0.0144 0.00772 0.00289 -0.0551 0.6799 0.6370
-2.000 0.0438 0.00771 0.00289 -0.0555 0.6781 0.6404
-1.750 0.0734 0.00772 0.00290 -0.0560 0.6759 0.6428
-1.500 0.1030 0.00773 0.00288 -0.0564 0.6732 0.6453
-1.250 0.1325 0.00773 0.00286 -0.0568 0.6704 0.6475
-1.000 0.1624 0.00779 0.00287 -0.0573 0.6675 0.6496
-0.750 0.1924 0.00785 0.00290 -0.0578 0.6651 0.6516
-0.500 0.2218 0.00784 0.00289 -0.0582 0.6632 0.6535
-0.250 0.2509 0.00776 0.00283 -0.0586 0.6608 0.6559
0.000 0.2803 0.00773 0.00281 -0.0590 0.6581 0.6575
0.250 0.3097 0.00771 0.00279 -0.0594 0.6554 0.6589
0.500 0.3391 0.00770 0.00277 -0.0598 0.6527 0.6603
0.750 0.3687 0.00774 0.00279 -0.0603 0.6489 0.6618
1.000 0.3970 0.00765 0.00273 -0.0604 0.6443 0.6633
1.250 0.4255 0.00759 0.00267 -0.0606 0.6387 0.6647
1.500 0.4545 0.00758 0.00264 -0.0609 0.6346 0.6660
1.750 0.4838 0.00759 0.00265 -0.0613 0.6310 0.6674
2.000 0.5129 0.00757 0.00265 -0.0617 0.6266 0.6686
2.250 0.5419 0.00756 0.00264 -0.0620 0.6212 0.6696
2.500 0.5704 0.00756 0.00261 -0.0622 0.6159 0.6707
2.750 0.5994 0.00749 0.00260 -0.0626 0.6099 0.6723
3.000 0.6277 0.00748 0.00259 -0.0628 0.6026 0.6738
3.250 0.6560 0.00748 0.00261 -0.0630 0.5935 0.6752
3.500 0.6836 0.00751 0.00263 -0.0630 0.5813 0.6766
3.750 0.7108 0.00757 0.00266 -0.0630 0.5662 0.6778
4.000 0.7372 0.00768 0.00272 -0.0628 0.5458 0.6791
4.250 0.7617 0.00789 0.00282 -0.0623 0.5174 0.6804
4.500 0.7848 0.00819 0.00298 -0.0615 0.4826 0.6818
4.750 0.8073 0.00855 0.00319 -0.0607 0.4472 0.6833
5.000 0.8300 0.00889 0.00341 -0.0599 0.4155 0.6846
5.250 0.8525 0.00925 0.00363 -0.0590 0.3865 0.6858
5.500 0.8751 0.00959 0.00386 -0.0582 0.3587 0.6867
5.750 0.8977 0.00990 0.00408 -0.0575 0.3353 0.6880
6.000 0.9198 0.01019 0.00429 -0.0566 0.3112 0.6898
6.250 0.9409 0.01055 0.00455 -0.0556 0.2868 0.6913
6.500 0.9619 0.01091 0.00482 -0.0545 0.2624 0.6927
6.750 0.9825 0.01129 0.00511 -0.0534 0.2417 0.6942
7.000 1.0029 0.01165 0.00540 -0.0523 0.2235 0.6958
7.250 1.0235 0.01200 0.00569 -0.0512 0.2079 0.6974
7.500 1.0441 0.01233 0.00598 -0.0501 0.1947 0.6989
7.750 1.0650 0.01264 0.00626 -0.0490 0.1840 0.7003
8.000 1.0839 0.01298 0.00657 -0.0476 0.1741 0.7017
8.250 1.1011 0.01328 0.00685 -0.0458 0.1657 0.7029
8.500 1.1190 0.01361 0.00716 -0.0442 0.1583 0.7040
8.750 1.1377 0.01394 0.00750 -0.0429 0.1508 0.7060
9.000 1.1565 0.01430 0.00787 -0.0416 0.1434 0.7079
9.250 1.1750 0.01469 0.00826 -0.0403 0.1363 0.7097
9.500 1.1928 0.01511 0.00869 -0.0389 0.1294 0.7116
9.750 1.2099 0.01558 0.00914 -0.0375 0.1217 0.7134
10.000 1.2265 0.01607 0.00964 -0.0360 0.1147 0.7153
10.250 1.2414 0.01666 0.01020 -0.0343 0.1066 0.7171
10.500 1.2569 0.01724 0.01078 -0.0329 0.0994 0.7188
10.750 1.2698 0.01798 0.01149 -0.0312 0.0918 0.7203
11.000 1.2841 0.01868 0.01220 -0.0298 0.0858 0.7222
11.250 1.2966 0.01952 0.01304 -0.0283 0.0794 0.7246
11.500 1.3097 0.02039 0.01393 -0.0271 0.0744 0.7268
11.750 1.3218 0.02140 0.01496 -0.0259 0.0691 0.7291
12.000 1.3352 0.02237 0.01597 -0.0250 0.0650 0.7313
12.250 1.3457 0.02362 0.01721 -0.0239 0.0601 0.7335
12.500 1.3600 0.02462 0.01826 -0.0233 0.0573 0.7357
12.750 1.3708 0.02589 0.01953 -0.0224 0.0538 0.7377
13.000 1.3822 0.02713 0.02082 -0.0217 0.0508 0.7410
13.250 1.3946 0.02830 0.02205 -0.0210 0.0485 0.7443
13.500 1.4042 0.02969 0.02347 -0.0202 0.0460 0.7476
13.750 1.4123 0.03119 0.02500 -0.0193 0.0436 0.7509
14.000 1.4239 0.03242 0.02631 -0.0187 0.0422 0.7541
14.250 1.4334 0.03383 0.02777 -0.0180 0.0404 0.7583
14.500 1.4398 0.03550 0.02948 -0.0171 0.0385 0.7631
14.750 1.4458 0.03720 0.03126 -0.0163 0.0368 0.7683
15.000 1.4558 0.03861 0.03276 -0.0158 0.0358 0.7749
15.250 1.4636 0.04023 0.03447 -0.0152 0.0345 0.7840
15.500 1.4695 0.04206 0.03639 -0.0147 0.0332 0.7975
15.750 1.4726 0.04420 0.03868 -0.0142 0.0318 0.8260
16.000 1.4527 0.04523 0.04009 -0.0077 0.0312 0.9895
16.250 1.4595 0.04688 0.04181 -0.0072 0.0304 1.0000
16.500 1.4658 0.04883 0.04383 -0.0069 0.0296 1.0000
16.750 1.4700 0.05105 0.04609 -0.0067 0.0285 1.0000
17.000 1.4717 0.05356 0.04863 -0.0066 0.0274 1.0000
17.250 1.4693 0.05655 0.05168 -0.0064 0.0262 1.0000
17.500 1.4751 0.05874 0.05395 -0.0065 0.0256 1.0000
17.750 1.4785 0.06123 0.05651 -0.0066 0.0248 1.0000
18.000 1.4795 0.06404 0.05938 -0.0068 0.0240 1.0000
18.250 1.4777 0.06721 0.06261 -0.0072 0.0233 1.0000
18.500 1.4726 0.07085 0.06632 -0.0076 0.0226 1.0000
18.750 1.4629 0.07517 0.07072 -0.0084 0.0220 1.0000
19.000 1.4626 0.07837 0.07401 -0.0090 0.0216 1.0000
19.250 1.4598 0.08194 0.07768 -0.0099 0.0212 1.0000
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