WORTMANN FX 057-816 (fx057816-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: WORTMANN FX 057-816 (fx057816-il) Reynolds number: 500,000 Max Cl/Cd: 113.83 at α=9.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx057816-il-500000.txt Download as CSV file: xf-fx057816-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 057-816
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-12.500 -0.5768 0.05402 0.05010 -0.0824 0.6068 0.0198
-12.250 -0.6347 0.04547 0.04131 -0.0856 0.6066 0.0195
-12.000 -0.6742 0.04022 0.03574 -0.0839 0.6063 0.0196
-11.750 -0.7019 0.03659 0.03181 -0.0801 0.6059 0.0196
-11.500 -0.7119 0.03435 0.02927 -0.0768 0.6054 0.0198
-11.250 -0.7214 0.03109 0.02566 -0.0739 0.6049 0.0202
-11.000 -0.7114 0.02963 0.02407 -0.0723 0.6043 0.0205
-10.750 -0.6944 0.02891 0.02330 -0.0713 0.6037 0.0210
-10.500 -0.6780 0.02791 0.02216 -0.0703 0.6030 0.0215
-10.250 -0.6606 0.02689 0.02097 -0.0693 0.6024 0.0222
-10.000 -0.6431 0.02569 0.01954 -0.0683 0.6017 0.0228
-9.750 -0.6240 0.02468 0.01829 -0.0675 0.6010 0.0235
-9.500 -0.6056 0.02334 0.01678 -0.0666 0.6004 0.0243
-9.250 -0.5827 0.02282 0.01626 -0.0662 0.5999 0.0252
-9.000 -0.5583 0.02252 0.01593 -0.0659 0.5993 0.0262
-8.750 -0.5343 0.02195 0.01524 -0.0655 0.5986 0.0274
-8.500 -0.5112 0.02107 0.01421 -0.0650 0.5978 0.0286
-8.250 -0.4864 0.02076 0.01392 -0.0647 0.5970 0.0298
-8.000 -0.4606 0.02058 0.01372 -0.0645 0.5962 0.0311
-7.750 -0.4351 0.02016 0.01318 -0.0643 0.5955 0.0328
-7.500 -0.4100 0.01976 0.01275 -0.0641 0.5948 0.0345
-7.250 -0.3829 0.01996 0.01299 -0.0641 0.5940 0.0360
-7.000 -0.3563 0.01988 0.01283 -0.0640 0.5933 0.0382
-6.750 -0.3304 0.01952 0.01240 -0.0638 0.5926 0.0403
-6.500 -0.3032 0.01972 0.01262 -0.0638 0.5919 0.0418
-6.250 -0.2761 0.01979 0.01265 -0.0638 0.5912 0.0441
-6.000 -0.2495 0.01957 0.01230 -0.0637 0.5906 0.0466
-5.750 -0.2226 0.01957 0.01234 -0.0638 0.5899 0.0483
-5.500 -0.1954 0.01963 0.01238 -0.0638 0.5893 0.0504
-5.250 -0.1680 0.01962 0.01228 -0.0638 0.5886 0.0529
-5.000 -0.1413 0.01916 0.01174 -0.0638 0.5879 0.0554
-4.750 -0.1143 0.01899 0.01159 -0.0639 0.5873 0.0573
-4.500 -0.0871 0.01896 0.01153 -0.0639 0.5867 0.0596
-4.250 -0.0598 0.01893 0.01145 -0.0639 0.5861 0.0620
-4.000 -0.0324 0.01918 0.01162 -0.0640 0.5855 0.0637
-3.750 -0.0070 0.01847 0.01094 -0.0639 0.5847 0.0663
-3.500 0.0200 0.01824 0.01076 -0.0640 0.5842 0.0685
-3.250 0.0471 0.01806 0.01061 -0.0640 0.5836 0.0704
-3.000 0.0742 0.01793 0.01049 -0.0641 0.5829 0.0725
-2.750 0.1013 0.01787 0.01044 -0.0641 0.5821 0.0741
-2.500 0.1283 0.01784 0.01042 -0.0642 0.5812 0.0752
-2.250 0.1540 0.01747 0.01007 -0.0641 0.5801 0.0769
-2.000 0.1799 0.01720 0.00985 -0.0640 0.5791 0.0793
-1.750 0.2066 0.01711 0.00979 -0.0641 0.5782 0.0811
-1.500 0.2334 0.01708 0.00977 -0.0642 0.5774 0.0830
-1.250 0.2605 0.01707 0.00977 -0.0643 0.5766 0.0849
-1.000 0.2877 0.01709 0.00980 -0.0644 0.5759 0.0871
-0.750 0.3152 0.01713 0.00983 -0.0646 0.5752 0.0886
-0.500 0.3423 0.01705 0.00976 -0.0647 0.5746 0.0917
-0.250 0.3698 0.01703 0.00977 -0.0649 0.5740 0.0953
0.000 0.3976 0.01707 0.00981 -0.0651 0.5735 0.0991
0.250 0.4254 0.01712 0.00986 -0.0653 0.5729 0.1037
0.500 0.4532 0.01709 0.00988 -0.0656 0.5722 0.1186
0.750 0.4733 0.01521 0.01004 -0.0656 0.5717 0.7510
1.000 0.4989 0.01556 0.01047 -0.0649 0.5711 0.8087
1.250 0.5241 0.01596 0.01089 -0.0642 0.5706 0.8281
1.500 0.5481 0.01643 0.01137 -0.0633 0.5700 0.8428
1.750 0.5719 0.01706 0.01201 -0.0627 0.5692 0.8536
2.000 0.5913 0.01767 0.01278 -0.0616 0.5674 0.8611
2.250 0.6131 0.01848 0.01367 -0.0613 0.5651 0.8683
2.500 0.6330 0.01895 0.01423 -0.0601 0.5631 0.8738
2.750 0.6550 0.01945 0.01477 -0.0594 0.5618 0.8813
3.000 0.6773 0.01981 0.01518 -0.0586 0.5607 0.8869
3.250 0.6981 0.02014 0.01554 -0.0574 0.5598 0.8935
3.500 0.7239 0.02040 0.01580 -0.0573 0.5590 0.8990
3.750 0.7507 0.02024 0.01566 -0.0570 0.5583 0.9018
4.000 0.7776 0.01998 0.01539 -0.0565 0.5576 0.9056
4.250 0.8049 0.01975 0.01514 -0.0560 0.5570 0.9109
4.500 0.8346 0.01964 0.01503 -0.0564 0.5564 0.9141
4.750 0.8656 0.01948 0.01485 -0.0571 0.5557 0.9152
5.000 0.8955 0.01940 0.01477 -0.0577 0.5551 0.9159
5.250 0.9169 0.01997 0.01542 -0.0573 0.5530 0.9174
5.500 0.9247 0.02143 0.01709 -0.0559 0.5468 0.9197
5.750 0.9598 0.02072 0.01636 -0.0569 0.5459 0.9202
6.000 0.9923 0.02032 0.01597 -0.0576 0.5450 0.9210
6.250 1.0284 0.01953 0.01517 -0.0587 0.5442 0.9216
6.500 1.0653 0.01863 0.01423 -0.0598 0.5431 0.9222
6.750 1.0991 0.01809 0.01370 -0.0608 0.5423 0.9230
7.000 1.1324 0.01765 0.01326 -0.0617 0.5415 0.9238
7.250 1.1672 0.01706 0.01265 -0.0628 0.5405 0.9246
7.500 1.1957 0.01694 0.01260 -0.0632 0.5383 0.9259
7.750 1.2190 0.01694 0.01275 -0.0630 0.5336 0.9277
8.000 1.2583 0.01551 0.01128 -0.0644 0.5297 0.9286
8.250 1.2973 0.01428 0.00998 -0.0658 0.5264 0.9293
8.500 1.3225 0.01407 0.00991 -0.0657 0.5209 0.9309
8.750 1.3529 0.01333 0.00921 -0.0661 0.5137 0.9323
9.000 1.3785 0.01307 0.00907 -0.0659 0.5038 0.9341
9.250 1.4052 0.01274 0.00879 -0.0659 0.4877 0.9360
9.500 1.4274 0.01254 0.00845 -0.0652 0.4489 0.9386
9.750 1.4122 0.01421 0.00970 -0.0596 0.3758 0.9450
10.000 1.3759 0.01633 0.01177 -0.0514 0.3469 0.9605
10.250 1.3400 0.02236 0.01781 -0.0512 0.3228 1.0000
10.500 1.3099 0.02673 0.02210 -0.0487 0.3037 1.0000
10.750 1.2848 0.03052 0.02577 -0.0462 0.2839 1.0000
11.000 1.2682 0.03369 0.02885 -0.0442 0.2658 1.0000
11.250 1.2591 0.03638 0.03145 -0.0426 0.2488 1.0000
11.500 1.2530 0.03906 0.03404 -0.0414 0.2303 1.0000
11.750 1.2516 0.04145 0.03633 -0.0405 0.2085 1.0000
12.000 1.2448 0.04438 0.03909 -0.0395 0.1785 1.0000
12.250 1.2363 0.04749 0.04196 -0.0385 0.1437 1.0000
12.500 1.2317 0.05032 0.04458 -0.0376 0.1160 1.0000
12.750 1.2338 0.05262 0.04680 -0.0371 0.1013 1.0000
13.000 1.2383 0.05473 0.04885 -0.0367 0.0902 1.0000
13.250 1.2460 0.05659 0.05069 -0.0365 0.0816 1.0000
13.500 1.2536 0.05848 0.05255 -0.0363 0.0724 1.0000
13.750 1.2589 0.06064 0.05467 -0.0361 0.0606 1.0000
14.000 1.2614 0.06312 0.05701 -0.0359 0.0442 1.0000
14.250 1.2640 0.06562 0.05942 -0.0357 0.0345 1.0000
14.500 1.2686 0.06801 0.06181 -0.0356 0.0304 1.0000
14.750 1.2714 0.07065 0.06445 -0.0356 0.0275 1.0000
15.000 1.2779 0.07291 0.06677 -0.0356 0.0260 1.0000
15.250 1.2837 0.07528 0.06919 -0.0358 0.0243 1.0000
15.500 1.2864 0.07809 0.07204 -0.0360 0.0232 1.0000
15.750 1.2869 0.08119 0.07517 -0.0362 0.0223 1.0000
16.000 1.2930 0.08365 0.07772 -0.0365 0.0216 1.0000
16.250 1.2979 0.08631 0.08045 -0.0369 0.0209 1.0000
16.500 1.3025 0.08902 0.08323 -0.0373 0.0201 1.0000
16.750 1.3051 0.09204 0.08630 -0.0379 0.0194 1.0000
17.000 1.3037 0.09557 0.08987 -0.0385 0.0187 1.0000
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