WORTMANN FX 79-K-144/17 AIRFOIL (fx79k144-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: WORTMANN FX 79-K-144/17 AIRFOIL (fx79k144-il) Reynolds number: 1,000,000 Max Cl/Cd: 110.64 at α=4.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx79k144-il-1000000.txt Download as CSV file: xf-fx79k144-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 79-K-144/17 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
------ -------- --------- --------- -------- -------- --------
-15.000 -0.7383 0.10162 0.09918 -0.0348 0.7928 0.0078
-14.750 -0.9222 0.05615 0.05319 -0.0647 0.7931 0.0073
-14.500 -0.9499 0.04822 0.04503 -0.0701 0.7927 0.0073
-14.250 -0.9685 0.04317 0.03978 -0.0720 0.7924 0.0072
-14.000 -0.9812 0.03941 0.03583 -0.0721 0.7922 0.0073
-13.750 -0.9889 0.03643 0.03267 -0.0713 0.7920 0.0073
-13.500 -0.9924 0.03395 0.03001 -0.0702 0.7917 0.0073
-13.250 -0.9926 0.03178 0.02768 -0.0688 0.7913 0.0073
-13.000 -0.9894 0.02987 0.02560 -0.0674 0.7906 0.0074
-12.750 -0.9829 0.02823 0.02380 -0.0661 0.7899 0.0074
-12.500 -0.9762 0.02694 0.02236 -0.0642 0.7891 0.0075
-12.250 -0.9648 0.02574 0.02102 -0.0628 0.7885 0.0076
-12.000 -0.9499 0.02461 0.01976 -0.0619 0.7879 0.0077
-11.750 -0.9335 0.02355 0.01856 -0.0610 0.7872 0.0078
-11.500 -0.9159 0.02252 0.01739 -0.0602 0.7867 0.0079
-11.250 -0.8970 0.02157 0.01631 -0.0595 0.7861 0.0080
-11.000 -0.8768 0.02071 0.01533 -0.0589 0.7855 0.0081
-10.750 -0.8555 0.01994 0.01444 -0.0585 0.7849 0.0082
-10.500 -0.8360 0.01887 0.01325 -0.0578 0.7843 0.0085
-10.250 -0.8136 0.01815 0.01246 -0.0574 0.7839 0.0089
-10.000 -0.7895 0.01763 0.01189 -0.0573 0.7834 0.0093
-9.750 -0.7647 0.01718 0.01140 -0.0572 0.7829 0.0097
-9.500 -0.7397 0.01677 0.01094 -0.0571 0.7825 0.0101
-9.250 -0.7144 0.01635 0.01045 -0.0571 0.7820 0.0106
-9.000 -0.6891 0.01592 0.00999 -0.0570 0.7815 0.0113
-8.750 -0.6626 0.01569 0.00977 -0.0571 0.7809 0.0122
-8.500 -0.6358 0.01549 0.00954 -0.0572 0.7803 0.0134
-8.250 -0.6094 0.01524 0.00926 -0.0573 0.7798 0.0147
-8.000 -0.5821 0.01516 0.00919 -0.0576 0.7792 0.0161
-7.750 -0.5544 0.01521 0.00922 -0.0578 0.7784 0.0175
-7.500 -0.5269 0.01498 0.00896 -0.0581 0.7779 0.0185
-7.250 -0.5008 0.01454 0.00852 -0.0582 0.7773 0.0199
-7.000 -0.4732 0.01433 0.00830 -0.0585 0.7765 0.0209
-6.750 -0.4456 0.01412 0.00808 -0.0588 0.7754 0.0218
-6.500 -0.4178 0.01392 0.00786 -0.0591 0.7742 0.0225
-6.250 -0.3896 0.01381 0.00774 -0.0594 0.7731 0.0230
-6.000 -0.3640 0.01322 0.00709 -0.0594 0.7721 0.0241
-5.750 -0.3369 0.01289 0.00674 -0.0595 0.7712 0.0250
-5.500 -0.3094 0.01262 0.00645 -0.0598 0.7701 0.0257
-5.250 -0.2816 0.01237 0.00618 -0.0600 0.7691 0.0265
-5.000 -0.2537 0.01214 0.00593 -0.0603 0.7681 0.0274
-4.750 -0.2257 0.01192 0.00568 -0.0605 0.7674 0.0281
-4.500 -0.1976 0.01171 0.00545 -0.0608 0.7666 0.0286
-4.250 -0.1696 0.01147 0.00518 -0.0610 0.7657 0.0299
-4.000 -0.1418 0.01128 0.00498 -0.0613 0.7646 0.0322
-3.750 -0.1133 0.01110 0.00481 -0.0616 0.7634 0.0347
-3.500 -0.0847 0.01084 0.00458 -0.0620 0.7621 0.0407
-3.250 -0.0567 0.01044 0.00436 -0.0624 0.7605 0.0752
-3.000 -0.0286 0.01007 0.00418 -0.0629 0.7590 0.1218
-2.750 -0.0002 0.00976 0.00403 -0.0634 0.7576 0.1666
-2.500 0.0285 0.00944 0.00389 -0.0640 0.7563 0.2168
-2.250 0.0572 0.00907 0.00373 -0.0646 0.7551 0.2794
-2.000 0.0858 0.00850 0.00353 -0.0653 0.7540 0.3889
-1.750 0.1153 0.00752 0.00325 -0.0666 0.7528 0.5982
-1.500 0.1450 0.00693 0.00316 -0.0673 0.7516 0.7327
-1.250 0.1738 0.00700 0.00331 -0.0674 0.7502 0.7897
-1.000 0.2033 0.00707 0.00338 -0.0678 0.7485 0.8039
-0.750 0.2336 0.00709 0.00338 -0.0683 0.7461 0.8121
-0.500 0.2620 0.00712 0.00345 -0.0683 0.7437 0.8199
-0.250 0.2906 0.00718 0.00350 -0.0683 0.7415 0.8299
0.000 0.3188 0.00718 0.00350 -0.0683 0.7396 0.8356
0.250 0.3486 0.00719 0.00348 -0.0687 0.7380 0.8412
0.500 0.3765 0.00715 0.00344 -0.0686 0.7364 0.8455
0.750 0.4050 0.00715 0.00346 -0.0687 0.7341 0.8484
1.000 0.4342 0.00712 0.00345 -0.0691 0.7308 0.8511
1.250 0.4638 0.00707 0.00341 -0.0696 0.7276 0.8545
1.500 0.4933 0.00699 0.00332 -0.0699 0.7245 0.8580
1.750 0.5214 0.00688 0.00321 -0.0700 0.7215 0.8606
2.000 0.5505 0.00683 0.00320 -0.0703 0.7154 0.8622
2.250 0.5802 0.00672 0.00308 -0.0708 0.7097 0.8634
2.500 0.6099 0.00666 0.00304 -0.0714 0.7014 0.8644
2.750 0.6396 0.00657 0.00292 -0.0720 0.6874 0.8654
3.000 0.6687 0.00654 0.00283 -0.0724 0.6686 0.8663
3.250 0.6971 0.00660 0.00280 -0.0727 0.6514 0.8672
3.750 0.7529 0.00690 0.00295 -0.0733 0.6216 0.8690
4.000 0.7803 0.00710 0.00308 -0.0735 0.5978 0.8701
4.250 0.8077 0.00730 0.00322 -0.0738 0.5757 0.8713
4.500 0.8341 0.00754 0.00335 -0.0738 0.5459 0.8726
4.750 0.8583 0.00787 0.00354 -0.0735 0.5124 0.8740
5.000 0.8822 0.00827 0.00379 -0.0732 0.4736 0.8749
5.250 0.9015 0.00899 0.00419 -0.0722 0.4055 0.8760
5.500 0.9209 0.00969 0.00462 -0.0712 0.3471 0.8771
5.750 0.9369 0.01061 0.00517 -0.0698 0.2734 0.8782
6.000 0.9467 0.01191 0.00597 -0.0675 0.1776 0.8797
6.250 0.9615 0.01283 0.00658 -0.0659 0.1178 0.8808
6.500 0.9788 0.01356 0.00712 -0.0648 0.0816 0.8816
6.750 0.9946 0.01433 0.00770 -0.0635 0.0471 0.8824
7.000 1.0123 0.01487 0.00818 -0.0623 0.0345 0.8831
7.250 1.0298 0.01533 0.00863 -0.0611 0.0293 0.8839
7.500 1.0494 0.01584 0.00913 -0.0604 0.0260 0.8846
7.750 1.0700 0.01634 0.00964 -0.0600 0.0238 0.8852
8.000 1.0897 0.01694 0.01025 -0.0596 0.0213 0.8859
8.250 1.1096 0.01762 0.01094 -0.0593 0.0186 0.8865
8.500 1.1293 0.01830 0.01163 -0.0591 0.0156 0.8870
8.750 1.1482 0.01898 0.01231 -0.0587 0.0127 0.8880
9.000 1.1657 0.01971 0.01304 -0.0580 0.0108 0.8891
9.250 1.1827 0.02047 0.01381 -0.0573 0.0100 0.8900
9.500 1.1992 0.02124 0.01461 -0.0565 0.0095 0.8909
9.750 1.2145 0.02210 0.01551 -0.0555 0.0090 0.8918
10.000 1.2289 0.02301 0.01646 -0.0545 0.0087 0.8927
10.250 1.2437 0.02389 0.01739 -0.0535 0.0086 0.8936
10.500 1.2574 0.02484 0.01841 -0.0524 0.0084 0.8946
10.750 1.2705 0.02584 0.01946 -0.0512 0.0083 0.8956
11.000 1.2831 0.02688 0.02056 -0.0501 0.0081 0.8967
11.250 1.2944 0.02802 0.02176 -0.0489 0.0080 0.8977
11.500 1.3053 0.02920 0.02300 -0.0476 0.0078 0.8988
11.750 1.3155 0.03045 0.02431 -0.0463 0.0077 0.8998
12.000 1.3245 0.03180 0.02572 -0.0450 0.0076 0.9008
12.250 1.3329 0.03320 0.02719 -0.0437 0.0074 0.9017
12.500 1.3400 0.03473 0.02880 -0.0423 0.0073 0.9027
12.750 1.3465 0.03631 0.03045 -0.0409 0.0072 0.9041
13.000 1.3513 0.03804 0.03227 -0.0395 0.0071 0.9055
13.250 1.3549 0.03995 0.03427 -0.0380 0.0070 0.9069
13.500 1.3575 0.04204 0.03645 -0.0367 0.0069 0.9083
13.750 1.3579 0.04440 0.03891 -0.0352 0.0068 0.9097
14.000 1.3565 0.04701 0.04164 -0.0338 0.0066 0.9112
14.250 1.3542 0.04979 0.04454 -0.0324 0.0066 0.9127
14.500 1.3556 0.05227 0.04713 -0.0314 0.0065 0.9142
14.750 1.3596 0.05456 0.04952 -0.0307 0.0065 0.9158
15.000 1.3633 0.05695 0.05201 -0.0301 0.0065 0.9174
15.250 1.3657 0.05949 0.05466 -0.0296 0.0065 0.9196
15.500 1.3675 0.06212 0.05742 -0.0291 0.0064 0.9219
15.750 1.3683 0.06490 0.06031 -0.0286 0.0064 0.9244
16.000 1.3680 0.06789 0.06342 -0.0283 0.0064 0.9272
16.250 1.3668 0.07107 0.06673 -0.0281 0.0064 0.9304
16.500 1.3645 0.07438 0.07018 -0.0279 0.0064 0.9345
16.750 1.3609 0.07786 0.07380 -0.0279 0.0063 0.9404
17.000 1.3557 0.08155 0.07764 -0.0279 0.0063 0.9482
17.250 1.3465 0.08506 0.08133 -0.0271 0.0063 0.9816
17.500 1.3397 0.08946 0.08587 -0.0281 0.0063 1.0000
17.750 1.3326 0.09411 0.09066 -0.0293 0.0063 1.0000
18.000 1.3236 0.09912 0.09580 -0.0307 0.0063 1.0000
18.250 1.3138 0.10440 0.10123 -0.0325 0.0063 1.0000
18.500 1.3024 0.11009 0.10707 -0.0345 0.0063 1.0000
18.750 1.2908 0.11604 0.11315 -0.0371 0.0063 1.0000
19.000 1.2777 0.12237 0.11963 -0.0399 0.0063 1.0000
19.250 1.2628 0.12923 0.12665 -0.0433 0.0063 1.0000
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