AS5048 (18%) (as5048-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: AS5048 (18%) (as5048-il) Reynolds number: 1,000,000 Max Cl/Cd: 79.85 at α=4.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-as5048-il-1000000-n5.txt Download as CSV file: xf-as5048-il-1000000-n5.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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -0.9732 0.11784 0.11493 -0.0329 1.0000 0.0049
-19.500 -0.9962 0.10965 0.10660 -0.0369 1.0000 0.0049
-19.250 -1.0152 0.10247 0.09927 -0.0404 1.0000 0.0049
-19.000 -1.0324 0.09582 0.09249 -0.0434 1.0000 0.0049
-18.750 -1.0463 0.08987 0.08641 -0.0460 1.0000 0.0049
-18.500 -1.0578 0.08447 0.08090 -0.0481 1.0000 0.0049
-18.250 -1.0674 0.07955 0.07586 -0.0500 1.0000 0.0049
-18.000 -1.0755 0.07498 0.07119 -0.0516 1.0000 0.0050
-17.750 -1.0814 0.07086 0.06697 -0.0528 1.0000 0.0050
-17.500 -1.0831 0.06681 0.06280 -0.0547 0.9997 0.0050
-17.250 -1.0790 0.06292 0.05880 -0.0573 0.9989 0.0050
-17.000 -1.0746 0.05934 0.05512 -0.0595 0.9974 0.0051
-16.750 -1.0735 0.05636 0.05206 -0.0600 0.9940 0.0051
-16.250 -1.0086 0.04842 0.04378 -0.0765 0.9252 0.0053
-16.000 -0.9980 0.04653 0.04125 -0.0777 0.7853 0.0054
-15.750 -0.9934 0.04455 0.03911 -0.0775 0.7675 0.0054
-15.500 -0.9883 0.04261 0.03706 -0.0772 0.7571 0.0055
-15.250 -0.9815 0.04087 0.03521 -0.0769 0.7498 0.0055
-15.000 -0.9747 0.03914 0.03339 -0.0766 0.7440 0.0056
-14.750 -0.9668 0.03757 0.03173 -0.0762 0.7388 0.0056
-14.500 -0.9590 0.03606 0.03012 -0.0757 0.7343 0.0057
-14.250 -0.9496 0.03467 0.02866 -0.0752 0.7310 0.0058
-14.000 -0.9396 0.03334 0.02725 -0.0747 0.7276 0.0058
-13.750 -0.9284 0.03213 0.02597 -0.0741 0.7244 0.0059
-13.500 -0.9166 0.03098 0.02476 -0.0736 0.7214 0.0060
-13.000 -0.8962 0.02845 0.02210 -0.0722 0.7163 0.0062
-12.750 -0.8839 0.02735 0.02096 -0.0716 0.7142 0.0063
-12.500 -0.8702 0.02635 0.01991 -0.0710 0.7120 0.0065
-12.250 -0.8555 0.02543 0.01895 -0.0705 0.7096 0.0066
-12.000 -0.8407 0.02453 0.01800 -0.0700 0.7074 0.0067
-11.750 -0.8252 0.02367 0.01710 -0.0694 0.7054 0.0068
-11.500 -0.8095 0.02283 0.01621 -0.0689 0.7035 0.0070
-11.250 -0.7933 0.02203 0.01537 -0.0684 0.7016 0.0071
-11.000 -0.7767 0.02124 0.01454 -0.0679 0.7000 0.0073
-10.750 -0.7599 0.02047 0.01372 -0.0674 0.6988 0.0074
-10.500 -0.7428 0.01971 0.01293 -0.0668 0.6975 0.0076
-10.250 -0.7250 0.01900 0.01219 -0.0664 0.6962 0.0078
-10.000 -0.7070 0.01833 0.01147 -0.0658 0.6948 0.0080
-9.750 -0.6890 0.01767 0.01078 -0.0653 0.6933 0.0081
-9.500 -0.6726 0.01695 0.01003 -0.0645 0.6917 0.0084
-9.250 -0.6544 0.01638 0.00944 -0.0637 0.6900 0.0087
-9.000 -0.6359 0.01589 0.00891 -0.0629 0.6885 0.0090
-8.750 -0.6174 0.01545 0.00845 -0.0619 0.6870 0.0093
-8.500 -0.6004 0.01506 0.00803 -0.0605 0.6856 0.0096
-8.250 -0.5832 0.01473 0.00767 -0.0591 0.6842 0.0099
-8.000 -0.5623 0.01441 0.00730 -0.0583 0.6829 0.0103
-7.750 -0.5412 0.01405 0.00693 -0.0575 0.6821 0.0107
-7.500 -0.5196 0.01370 0.00659 -0.0568 0.6811 0.0113
-7.250 -0.4967 0.01341 0.00629 -0.0563 0.6800 0.0119
-7.000 -0.4731 0.01314 0.00601 -0.0559 0.6788 0.0125
-6.750 -0.4491 0.01289 0.00574 -0.0555 0.6774 0.0131
-6.500 -0.4256 0.01258 0.00543 -0.0550 0.6762 0.0138
-6.250 -0.4013 0.01232 0.00516 -0.0547 0.6750 0.0146
-6.000 -0.3763 0.01209 0.00492 -0.0544 0.6739 0.0155
-5.750 -0.3510 0.01188 0.00469 -0.0542 0.6727 0.0165
-5.500 -0.3258 0.01164 0.00446 -0.0540 0.6714 0.0181
-5.250 -0.3001 0.01144 0.00425 -0.0539 0.6701 0.0200
-5.000 -0.2743 0.01123 0.00405 -0.0537 0.6687 0.0236
-4.750 -0.2493 0.01095 0.00382 -0.0535 0.6673 0.0372
-4.500 -0.2290 0.01027 0.00343 -0.0527 0.6660 0.1075
-4.250 -0.2107 0.00931 0.00296 -0.0517 0.6651 0.2222
-4.000 -0.1897 0.00846 0.00256 -0.0512 0.6639 0.3295
-3.750 -0.1670 0.00765 0.00218 -0.0510 0.6627 0.4384
-3.500 -0.1418 0.00705 0.00197 -0.0510 0.6613 0.5405
-3.250 -0.1127 0.00696 0.00196 -0.0514 0.6598 0.5681
-3.000 -0.0831 0.00694 0.00194 -0.0518 0.6582 0.5802
-2.750 -0.0534 0.00693 0.00193 -0.0523 0.6565 0.5917
-2.500 -0.0237 0.00694 0.00192 -0.0528 0.6548 0.6005
-2.250 0.0060 0.00695 0.00192 -0.0532 0.6530 0.6071
-2.000 0.0357 0.00697 0.00192 -0.0537 0.6511 0.6119
-1.750 0.0655 0.00700 0.00191 -0.0542 0.6489 0.6153
-1.500 0.0953 0.00699 0.00189 -0.0547 0.6465 0.6182
-1.250 0.1249 0.00697 0.00186 -0.0551 0.6431 0.6204
-1.000 0.1543 0.00695 0.00185 -0.0555 0.6395 0.6230
-0.750 0.1838 0.00696 0.00185 -0.0559 0.6366 0.6259
-0.500 0.2132 0.00698 0.00184 -0.0564 0.6339 0.6285
-0.250 0.2429 0.00699 0.00185 -0.0568 0.6312 0.6305
0.000 0.2727 0.00699 0.00185 -0.0573 0.6281 0.6320
0.250 0.3023 0.00699 0.00184 -0.0578 0.6242 0.6335
0.500 0.3317 0.00700 0.00183 -0.0582 0.6203 0.6349
0.750 0.3607 0.00702 0.00182 -0.0586 0.6155 0.6360
1.000 0.3898 0.00700 0.00181 -0.0589 0.6060 0.6373
1.250 0.4180 0.00701 0.00179 -0.0591 0.5935 0.6388
1.500 0.4463 0.00705 0.00180 -0.0592 0.5824 0.6402
1.750 0.4748 0.00709 0.00183 -0.0595 0.5711 0.6416
2.000 0.5027 0.00716 0.00186 -0.0596 0.5565 0.6428
2.250 0.5295 0.00730 0.00191 -0.0595 0.5356 0.6441
2.500 0.5557 0.00748 0.00200 -0.0593 0.5101 0.6456
2.750 0.5817 0.00768 0.00211 -0.0591 0.4871 0.6470
3.000 0.6077 0.00789 0.00223 -0.0589 0.4636 0.6483
3.250 0.6328 0.00815 0.00238 -0.0586 0.4375 0.6495
3.500 0.6575 0.00842 0.00255 -0.0581 0.4092 0.6506
3.750 0.6823 0.00869 0.00271 -0.0577 0.3853 0.6517
4.000 0.7075 0.00893 0.00287 -0.0574 0.3649 0.6527
4.250 0.7320 0.00918 0.00304 -0.0570 0.3429 0.6541
4.500 0.7557 0.00947 0.00324 -0.0564 0.3196 0.6556
4.750 0.7793 0.00976 0.00344 -0.0558 0.2958 0.6568
5.000 0.8022 0.01008 0.00367 -0.0550 0.2730 0.6581
5.250 0.8258 0.01035 0.00388 -0.0545 0.2552 0.6593
5.500 0.8490 0.01064 0.00410 -0.0538 0.2368 0.6606
5.750 0.8721 0.01093 0.00433 -0.0531 0.2212 0.6619
6.000 0.8950 0.01122 0.00456 -0.0524 0.2068 0.6634
6.500 0.9396 0.01182 0.00506 -0.0508 0.1797 0.6662
6.750 0.9621 0.01210 0.00531 -0.0500 0.1698 0.6674
7.000 0.9839 0.01240 0.00557 -0.0491 0.1606 0.6685
7.250 1.0063 0.01266 0.00582 -0.0484 0.1533 0.6695
7.500 1.0272 0.01297 0.00610 -0.0473 0.1454 0.6705
7.750 1.0475 0.01320 0.00635 -0.0461 0.1393 0.6720
8.000 1.0643 0.01352 0.00665 -0.0443 0.1318 0.6734
8.250 1.0844 0.01379 0.00695 -0.0431 0.1262 0.6748
8.500 1.1026 0.01419 0.00732 -0.0417 0.1185 0.6763
8.750 1.1226 0.01452 0.00767 -0.0406 0.1129 0.6778
9.000 1.1398 0.01499 0.00810 -0.0391 0.1044 0.6795
9.250 1.1582 0.01540 0.00852 -0.0378 0.0984 0.6811
9.500 1.1744 0.01592 0.00901 -0.0363 0.0911 0.6826
9.750 1.1908 0.01643 0.00952 -0.0348 0.0847 0.6840
10.000 1.2064 0.01700 0.01008 -0.0333 0.0791 0.6853
10.250 1.2220 0.01759 0.01067 -0.0318 0.0740 0.6865
10.500 1.2365 0.01826 0.01134 -0.0303 0.0690 0.6878
10.750 1.2518 0.01892 0.01203 -0.0291 0.0649 0.6894
11.000 1.2649 0.01974 0.01285 -0.0277 0.0604 0.6911
11.250 1.2800 0.02050 0.01365 -0.0267 0.0569 0.6927
11.500 1.2931 0.02145 0.01461 -0.0256 0.0531 0.6944
11.750 1.3070 0.02239 0.01558 -0.0247 0.0500 0.6961
12.000 1.3206 0.02340 0.01662 -0.0239 0.0470 0.6978
12.250 1.3328 0.02454 0.01778 -0.0230 0.0440 0.6995
12.500 1.3468 0.02557 0.01885 -0.0224 0.0421 0.7013
12.750 1.3593 0.02672 0.02002 -0.0217 0.0399 0.7030
13.250 1.3829 0.02916 0.02254 -0.0203 0.0364 0.7069
13.500 1.3950 0.03035 0.02379 -0.0196 0.0349 0.7091
13.750 1.4057 0.03164 0.02513 -0.0189 0.0335 0.7112
14.000 1.4148 0.03307 0.02660 -0.0181 0.0321 0.7134
14.250 1.4244 0.03447 0.02804 -0.0174 0.0308 0.7156
14.500 1.4340 0.03587 0.02950 -0.0167 0.0297 0.7177
14.750 1.4423 0.03737 0.03105 -0.0160 0.0285 0.7198
15.250 1.4556 0.04074 0.03452 -0.0146 0.0262 0.7247
15.500 1.4638 0.04234 0.03620 -0.0141 0.0255 0.7276
15.750 1.4705 0.04409 0.03802 -0.0135 0.0247 0.7307
16.000 1.4766 0.04594 0.03994 -0.0130 0.0239 0.7338
16.250 1.4803 0.04808 0.04212 -0.0126 0.0227 0.7369
16.500 1.4848 0.05019 0.04430 -0.0122 0.0220 0.7409
16.750 1.4898 0.05232 0.04654 -0.0121 0.0213 0.7460
17.000 1.4940 0.05455 0.04884 -0.0119 0.0203 0.7514
17.250 1.4966 0.05702 0.05139 -0.0118 0.0195 0.7576
17.500 1.4975 0.05974 0.05420 -0.0119 0.0187 0.7661
17.750 1.4991 0.06247 0.05704 -0.0121 0.0180 0.7768
18.000 1.5014 0.06520 0.05989 -0.0124 0.0175 0.7945
18.250 1.5031 0.06813 0.06309 -0.0131 0.0169 0.8511
18.500 1.4847 0.07005 0.06530 -0.0086 0.0167 0.9795
18.750 1.4801 0.07324 0.06857 -0.0085 0.0163 0.9868
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