WORTMANN FX 049-915 AIRFOIL (fx049915-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
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Airfoil: WORTMANN FX 049-915 AIRFOIL (fx049915-il) Reynolds number: 1,000,000 Max Cl/Cd: 155.01 at α=9.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx049915-il-1000000.txt Download as CSV file: xf-fx049915-il-1000000.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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-12.500 -0.6974 0.03660 0.03259 -0.0902 0.4968 0.0117
-12.250 -0.7269 0.03248 0.02819 -0.0854 0.4962 0.0118
-12.000 -0.7299 0.03010 0.02560 -0.0825 0.4948 0.0119
-11.750 -0.7277 0.02804 0.02334 -0.0799 0.4931 0.0120
-11.500 -0.7158 0.02680 0.02200 -0.0781 0.4923 0.0122
-11.250 -0.7039 0.02542 0.02047 -0.0762 0.4915 0.0123
-11.000 -0.6890 0.02430 0.01922 -0.0746 0.4905 0.0126
-10.750 -0.6719 0.02334 0.01814 -0.0732 0.4893 0.0128
-10.500 -0.6543 0.02237 0.01705 -0.0718 0.4882 0.0131
-10.250 -0.6371 0.02129 0.01580 -0.0703 0.4870 0.0134
-10.000 -0.6177 0.02043 0.01480 -0.0690 0.4858 0.0137
-9.750 -0.5975 0.01964 0.01387 -0.0678 0.4845 0.0139
-9.500 -0.5761 0.01897 0.01306 -0.0667 0.4832 0.0141
-9.250 -0.5571 0.01796 0.01188 -0.0653 0.4819 0.0145
-9.000 -0.5371 0.01714 0.01094 -0.0640 0.4804 0.0150
-8.750 -0.5145 0.01664 0.01036 -0.0631 0.4786 0.0154
-8.500 -0.4909 0.01627 0.00992 -0.0622 0.4770 0.0159
-8.250 -0.4671 0.01578 0.00935 -0.0614 0.4764 0.0164
-8.000 -0.4430 0.01529 0.00878 -0.0606 0.4758 0.0168
-7.750 -0.4182 0.01491 0.00832 -0.0600 0.4749 0.0173
-7.500 -0.3955 0.01423 0.00754 -0.0589 0.4741 0.0180
-7.250 -0.3712 0.01380 0.00706 -0.0582 0.4732 0.0188
-7.000 -0.3460 0.01347 0.00669 -0.0575 0.4722 0.0195
-6.750 -0.3206 0.01316 0.00633 -0.0569 0.4712 0.0203
-6.500 -0.2950 0.01290 0.00600 -0.0563 0.4703 0.0210
-6.250 -0.2707 0.01246 0.00552 -0.0555 0.4694 0.0225
-6.000 -0.2449 0.01223 0.00527 -0.0550 0.4684 0.0239
-5.750 -0.2188 0.01204 0.00502 -0.0545 0.4675 0.0251
-5.500 -0.1937 0.01173 0.00471 -0.0538 0.4666 0.0273
-5.250 -0.1675 0.01157 0.00452 -0.0533 0.4656 0.0293
-5.000 -0.1416 0.01140 0.00434 -0.0528 0.4646 0.0320
-4.750 -0.1148 0.01136 0.00428 -0.0524 0.4632 0.0348
-4.500 -0.0882 0.01138 0.00430 -0.0521 0.4615 0.0380
-4.250 -0.0600 0.01140 0.00432 -0.0519 0.4610 0.0408
-4.000 -0.0330 0.01130 0.00423 -0.0516 0.4606 0.0433
-3.750 -0.0046 0.01137 0.00431 -0.0516 0.4600 0.0455
-3.500 0.0238 0.01145 0.00439 -0.0515 0.4594 0.0478
-3.250 0.0522 0.01154 0.00446 -0.0515 0.4587 0.0490
-3.000 0.0777 0.01127 0.00420 -0.0509 0.4580 0.0515
-2.750 0.1057 0.01131 0.00425 -0.0508 0.4573 0.0534
-2.500 0.1333 0.01131 0.00424 -0.0506 0.4566 0.0552
-2.250 0.1610 0.01132 0.00423 -0.0505 0.4558 0.0568
-2.000 0.1892 0.01139 0.00429 -0.0504 0.4551 0.0578
-1.750 0.2132 0.01096 0.00386 -0.0496 0.4543 0.0605
-1.500 0.2401 0.01090 0.00380 -0.0493 0.4536 0.0623
-1.250 0.2671 0.01084 0.00373 -0.0491 0.4529 0.0640
-1.000 0.2940 0.01077 0.00365 -0.0488 0.4521 0.0656
-0.750 0.3209 0.01069 0.00356 -0.0485 0.4513 0.0669
-0.500 0.3478 0.01064 0.00349 -0.0482 0.4505 0.0678
-0.250 0.3743 0.01055 0.00339 -0.0479 0.4497 0.0692
0.000 0.3999 0.01041 0.00323 -0.0474 0.4489 0.0715
0.250 0.4265 0.01039 0.00321 -0.0471 0.4480 0.0734
0.500 0.4533 0.01045 0.00326 -0.0469 0.4470 0.0752
0.750 0.4802 0.01052 0.00334 -0.0467 0.4461 0.0773
1.000 0.5074 0.01050 0.00332 -0.0465 0.4458 0.0792
1.250 0.5346 0.01049 0.00333 -0.0464 0.4454 0.0804
1.500 0.5614 0.01044 0.00329 -0.0461 0.4449 0.0839
1.750 0.5883 0.01041 0.00329 -0.0459 0.4444 0.0881
2.000 0.6154 0.01040 0.00330 -0.0458 0.4437 0.0921
2.250 0.6422 0.01037 0.00332 -0.0455 0.4430 0.1052
2.500 0.6407 0.00868 0.00341 -0.0399 0.4425 0.7611
2.750 0.7708 0.00857 0.00381 -0.0622 0.4414 0.9855
3.000 0.8191 0.00871 0.00393 -0.0667 0.4407 0.9915
3.250 0.8651 0.00881 0.00401 -0.0707 0.4400 0.9954
3.500 0.9084 0.00885 0.00405 -0.0741 0.4392 0.9982
3.750 0.9478 0.00890 0.00409 -0.0767 0.4384 1.0000
4.000 0.9719 0.00896 0.00415 -0.0761 0.4376 1.0000
4.250 0.9961 0.00903 0.00422 -0.0755 0.4369 1.0000
4.500 1.0204 0.00911 0.00431 -0.0749 0.4362 1.0000
4.750 1.0448 0.00920 0.00440 -0.0743 0.4356 1.0000
5.000 1.0692 0.00931 0.00451 -0.0737 0.4349 1.0000
5.250 1.0937 0.00942 0.00464 -0.0732 0.4341 1.0000
5.500 1.1182 0.00958 0.00480 -0.0727 0.4330 1.0000
5.750 1.1421 0.00991 0.00513 -0.0721 0.4313 1.0000
6.000 1.1667 0.00994 0.00520 -0.0716 0.4308 1.0000
6.250 1.1911 0.00988 0.00520 -0.0710 0.4295 1.0000
6.500 1.2156 0.00985 0.00522 -0.0704 0.4279 1.0000
6.750 1.2403 0.00985 0.00525 -0.0700 0.4262 1.0000
7.000 1.2654 0.00979 0.00521 -0.0695 0.4240 1.0000
7.250 1.2906 0.00966 0.00507 -0.0690 0.4211 1.0000
7.500 1.3153 0.00970 0.00511 -0.0686 0.4189 1.0000
7.750 1.3396 0.00975 0.00520 -0.0681 0.4159 1.0000
8.000 1.3643 0.00970 0.00522 -0.0676 0.4133 1.0000
8.250 1.3892 0.00966 0.00523 -0.0671 0.4102 1.0000
8.500 1.4140 0.00961 0.00520 -0.0667 0.4063 1.0000
8.750 1.4379 0.00966 0.00526 -0.0661 0.4018 1.0000
9.000 1.4632 0.00965 0.00533 -0.0658 0.3967 1.0000
9.250 1.4871 0.00969 0.00538 -0.0653 0.3905 1.0000
9.500 1.5113 0.00975 0.00549 -0.0648 0.3805 1.0000
9.750 1.5314 0.01000 0.00566 -0.0637 0.3567 1.0000
10.000 1.5364 0.01112 0.00649 -0.0602 0.3049 1.0000
10.250 1.5325 0.01273 0.00781 -0.0555 0.2546 1.0000
10.500 1.5255 0.01434 0.00921 -0.0504 0.2123 1.0000
10.750 1.5088 0.01617 0.01084 -0.0440 0.1732 1.0000
11.000 1.4875 0.01772 0.01230 -0.0369 0.1525 1.0000
11.250 1.4578 0.02094 0.01553 -0.0324 0.1322 1.0000
11.500 1.4349 0.02637 0.02104 -0.0331 0.1211 1.0000
11.750 1.4071 0.03208 0.02679 -0.0330 0.1107 1.0000
12.000 1.3835 0.03677 0.03151 -0.0320 0.1034 1.0000
12.250 1.3647 0.04085 0.03563 -0.0311 0.0963 1.0000
12.500 1.3426 0.04522 0.03999 -0.0302 0.0864 1.0000
12.750 1.3256 0.04915 0.04390 -0.0294 0.0772 1.0000
13.000 1.3164 0.05253 0.04725 -0.0289 0.0677 1.0000
13.250 1.3037 0.05644 0.05110 -0.0286 0.0539 1.0000
13.500 1.2888 0.06060 0.05514 -0.0283 0.0352 1.0000
13.750 1.2795 0.06433 0.05883 -0.0282 0.0263 1.0000
14.000 1.2782 0.06720 0.06170 -0.0281 0.0226 1.0000
14.250 1.2802 0.06974 0.06426 -0.0280 0.0208 1.0000
14.500 1.2820 0.07236 0.06692 -0.0280 0.0197 1.0000
14.750 1.2834 0.07500 0.06960 -0.0280 0.0186 1.0000
15.000 1.2855 0.07761 0.07225 -0.0281 0.0174 1.0000
15.250 1.2888 0.08011 0.07480 -0.0282 0.0168 1.0000
15.500 1.2913 0.08271 0.07744 -0.0283 0.0160 1.0000
15.750 1.2947 0.08523 0.07999 -0.0285 0.0154 1.0000
16.000 1.2935 0.08834 0.08315 -0.0287 0.0145 1.0000
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