WORTMANN FX 049-915 AIRFOIL (fx049915-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
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Airfoil: WORTMANN FX 049-915 AIRFOIL (fx049915-il) Reynolds number: 1,000,000 Max Cl/Cd: 152.65 at α=8.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx049915-il-1000000-n5.txt Download as CSV file: xf-fx049915-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 049-915 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
------ -------- --------- --------- -------- -------- --------
-12.500 -0.3610 0.08069 0.07679 -0.0715 0.4685 0.0074
-12.250 -0.6790 0.03802 0.03376 -0.0893 0.4735 0.0067
-12.000 -0.7044 0.03169 0.02705 -0.0860 0.4732 0.0066
-11.750 -0.7069 0.02767 0.02275 -0.0836 0.4724 0.0067
-11.500 -0.6962 0.02548 0.02038 -0.0820 0.4714 0.0068
-11.250 -0.6829 0.02386 0.01859 -0.0803 0.4703 0.0069
-11.000 -0.6650 0.02277 0.01737 -0.0791 0.4693 0.0071
-10.750 -0.6474 0.02167 0.01612 -0.0778 0.4681 0.0072
-10.500 -0.6289 0.02064 0.01494 -0.0765 0.4670 0.0074
-10.250 -0.6085 0.01982 0.01400 -0.0754 0.4659 0.0075
-10.000 -0.5879 0.01904 0.01307 -0.0743 0.4647 0.0076
-9.750 -0.5665 0.01833 0.01224 -0.0732 0.4635 0.0077
-9.500 -0.5448 0.01764 0.01143 -0.0722 0.4624 0.0078
-9.250 -0.5233 0.01691 0.01059 -0.0712 0.4611 0.0081
-9.000 -0.5005 0.01632 0.00991 -0.0703 0.4599 0.0084
-8.750 -0.4767 0.01582 0.00935 -0.0695 0.4593 0.0086
-8.500 -0.4526 0.01535 0.00882 -0.0688 0.4587 0.0089
-8.250 -0.4282 0.01491 0.00830 -0.0681 0.4580 0.0091
-8.000 -0.4035 0.01450 0.00783 -0.0674 0.4572 0.0095
-7.750 -0.3785 0.01413 0.00738 -0.0668 0.4564 0.0098
-7.500 -0.3533 0.01379 0.00697 -0.0662 0.4556 0.0100
-7.250 -0.3279 0.01346 0.00658 -0.0656 0.4547 0.0103
-7.000 -0.3032 0.01303 0.00611 -0.0649 0.4538 0.0110
-6.750 -0.2777 0.01272 0.00576 -0.0643 0.4528 0.0116
-6.500 -0.2520 0.01244 0.00543 -0.0638 0.4519 0.0122
-6.250 -0.2262 0.01219 0.00512 -0.0633 0.4507 0.0128
-6.000 -0.2002 0.01196 0.00485 -0.0628 0.4498 0.0133
-5.750 -0.1746 0.01168 0.00453 -0.0622 0.4488 0.0142
-5.500 -0.1490 0.01142 0.00425 -0.0617 0.4479 0.0154
-5.250 -0.1230 0.01122 0.00401 -0.0612 0.4470 0.0166
-5.000 -0.0969 0.01105 0.00380 -0.0607 0.4460 0.0176
-4.750 -0.0714 0.01083 0.00357 -0.0601 0.4450 0.0204
-4.500 -0.0453 0.01066 0.00339 -0.0596 0.4442 0.0229
-4.250 -0.0190 0.01050 0.00325 -0.0592 0.4438 0.0289
-4.000 0.0077 0.01037 0.00314 -0.0589 0.4433 0.0337
-3.750 0.0352 0.01033 0.00314 -0.0587 0.4428 0.0401
-3.500 0.0626 0.01029 0.00309 -0.0584 0.4422 0.0435
-3.250 0.0900 0.01024 0.00302 -0.0582 0.4416 0.0450
-3.000 0.1173 0.01020 0.00296 -0.0580 0.4410 0.0459
-2.750 0.1443 0.01011 0.00287 -0.0577 0.4404 0.0483
-2.500 0.1717 0.01007 0.00284 -0.0575 0.4397 0.0500
-2.250 0.1995 0.01008 0.00285 -0.0574 0.4390 0.0521
-2.000 0.2271 0.01007 0.00283 -0.0572 0.4383 0.0541
-1.750 0.2544 0.01003 0.00277 -0.0570 0.4375 0.0551
-1.500 0.2815 0.00996 0.00268 -0.0568 0.4366 0.0558
-1.250 0.3086 0.00991 0.00261 -0.0565 0.4359 0.0565
-1.000 0.3357 0.00987 0.00256 -0.0563 0.4352 0.0569
-0.750 0.3625 0.00979 0.00246 -0.0560 0.4345 0.0579
-0.500 0.3890 0.00970 0.00236 -0.0557 0.4338 0.0606
-0.250 0.4160 0.00966 0.00233 -0.0555 0.4331 0.0623
0.000 0.4430 0.00964 0.00229 -0.0553 0.4325 0.0634
0.250 0.4701 0.00962 0.00227 -0.0551 0.4318 0.0645
0.500 0.4971 0.00962 0.00226 -0.0549 0.4310 0.0657
0.750 0.5240 0.00963 0.00226 -0.0547 0.4302 0.0667
1.000 0.5510 0.00965 0.00228 -0.0545 0.4293 0.0679
1.250 0.5782 0.00964 0.00229 -0.0544 0.4289 0.0688
1.500 0.6056 0.00964 0.00229 -0.0543 0.4285 0.0698
1.750 0.6329 0.00964 0.00231 -0.0542 0.4280 0.0705
2.000 0.6600 0.00962 0.00232 -0.0541 0.4275 0.0728
2.250 0.6871 0.00962 0.00235 -0.0540 0.4269 0.0759
2.500 0.7143 0.00963 0.00239 -0.0539 0.4264 0.0790
2.750 0.7413 0.00964 0.00244 -0.0538 0.4258 0.0847
3.000 0.7681 0.00963 0.00249 -0.0536 0.4253 0.1015
3.250 0.7672 0.00805 0.00263 -0.0481 0.4248 0.7797
3.750 0.9255 0.00800 0.00304 -0.0710 0.4232 0.9885
4.250 0.9990 0.00818 0.00321 -0.0752 0.4215 0.9957
4.500 1.0403 0.00824 0.00328 -0.0783 0.4209 0.9985
4.750 1.0771 0.00831 0.00336 -0.0805 0.4202 1.0000
5.000 1.1019 0.00839 0.00345 -0.0800 0.4196 1.0000
5.250 1.1266 0.00847 0.00355 -0.0795 0.4188 1.0000
5.500 1.1514 0.00856 0.00364 -0.0791 0.4180 1.0000
5.750 1.1761 0.00866 0.00375 -0.0786 0.4171 1.0000
6.000 1.2007 0.00877 0.00388 -0.0781 0.4161 1.0000
6.250 1.2251 0.00891 0.00401 -0.0776 0.4144 1.0000
6.500 1.2503 0.00894 0.00410 -0.0773 0.4131 1.0000
6.750 1.2757 0.00895 0.00417 -0.0770 0.4107 1.0000
7.000 1.3010 0.00900 0.00425 -0.0766 0.4083 1.0000
7.250 1.3260 0.00905 0.00434 -0.0763 0.4057 1.0000
7.500 1.3502 0.00911 0.00438 -0.0758 0.4012 1.0000
7.750 1.3753 0.00916 0.00448 -0.0755 0.3964 1.0000
8.000 1.4001 0.00923 0.00458 -0.0751 0.3910 1.0000
8.250 1.4237 0.00935 0.00470 -0.0745 0.3849 1.0000
8.500 1.4471 0.00948 0.00483 -0.0740 0.3730 1.0000
8.750 1.4646 0.00993 0.00515 -0.0724 0.3441 1.0000
9.000 1.4691 0.01114 0.00608 -0.0689 0.2937 1.0000
9.250 1.4711 0.01245 0.00717 -0.0650 0.2524 1.0000
9.500 1.4683 0.01389 0.00839 -0.0604 0.2107 1.0000
9.750 1.4480 0.01595 0.01018 -0.0533 0.1603 1.0000
10.000 1.4195 0.01776 0.01187 -0.0451 0.1312 1.0000
10.250 1.3965 0.02042 0.01452 -0.0406 0.1137 1.0000
10.500 1.3778 0.02499 0.01917 -0.0406 0.1038 1.0000
10.750 1.3704 0.02889 0.02315 -0.0410 0.0992 1.0000
11.000 1.3443 0.03417 0.02846 -0.0403 0.0895 1.0000
11.250 1.3340 0.03758 0.03194 -0.0396 0.0862 1.0000
11.500 1.3179 0.04145 0.03583 -0.0386 0.0799 1.0000
11.750 1.3063 0.04489 0.03929 -0.0378 0.0742 1.0000
12.000 1.2975 0.04807 0.04248 -0.0371 0.0671 1.0000
12.250 1.2840 0.05183 0.04621 -0.0365 0.0549 1.0000
12.500 1.2632 0.05654 0.05079 -0.0360 0.0320 1.0000
12.750 1.2590 0.05965 0.05391 -0.0357 0.0250 1.0000
13.000 1.2591 0.06232 0.05657 -0.0355 0.0188 1.0000
13.250 1.2617 0.06477 0.05906 -0.0353 0.0169 1.0000
13.500 1.2636 0.06733 0.06164 -0.0352 0.0149 1.0000
13.750 1.2687 0.06952 0.06387 -0.0352 0.0139 1.0000
14.000 1.2728 0.07184 0.06620 -0.0351 0.0126 1.0000
14.250 1.2756 0.07436 0.06877 -0.0351 0.0116 1.0000
14.500 1.2797 0.07675 0.07120 -0.0351 0.0109 1.0000
14.750 1.2846 0.07901 0.07348 -0.0352 0.0100 1.0000
15.000 1.2900 0.08122 0.07573 -0.0352 0.0097 1.0000
15.250 1.2933 0.08374 0.07828 -0.0353 0.0091 1.0000
15.500 1.2962 0.08635 0.08093 -0.0355 0.0084 1.0000
15.750 1.3015 0.08864 0.08325 -0.0356 0.0080 1.0000
16.000 1.3063 0.09096 0.08561 -0.0358 0.0077 1.0000
16.250 1.3095 0.09353 0.08822 -0.0360 0.0073 1.0000
16.500 1.3121 0.09622 0.09095 -0.0363 0.0069 1.0000
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