NACA 16-018 (naca16018-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 16-018 (naca16018-il) Reynolds number: 1,000,000 Max Cl/Cd: 40.47 at α=11° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-naca16018-il-1000000-n5.txt Download as CSV file: xf-naca16018-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NACA 16-018
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 -1.2109 0.05796 0.05341 -0.0964 0.9949 0.0092
-19.500 -1.2101 0.05504 0.05039 -0.0971 0.9946 0.0094
-19.250 -1.2072 0.05239 0.04766 -0.0976 0.9943 0.0096
-19.000 -1.2027 0.04996 0.04515 -0.0981 0.9940 0.0098
-18.750 -1.1987 0.04778 0.04288 -0.0980 0.9932 0.0101
-18.500 -1.1938 0.04578 0.04080 -0.0977 0.9922 0.0104
-18.250 -1.1872 0.04393 0.03887 -0.0974 0.9913 0.0106
-18.000 -1.1796 0.04217 0.03703 -0.0972 0.9905 0.0108
-17.750 -1.1719 0.04043 0.03522 -0.0969 0.9897 0.0112
-17.500 -1.1626 0.03883 0.03356 -0.0967 0.9889 0.0116
-17.250 -1.1518 0.03734 0.03202 -0.0965 0.9882 0.0121
-17.000 -1.1396 0.03595 0.03058 -0.0964 0.9876 0.0125
-16.750 -1.1266 0.03467 0.02924 -0.0963 0.9870 0.0129
-16.500 -1.1127 0.03346 0.02796 -0.0962 0.9865 0.0134
-16.250 -1.0980 0.03234 0.02677 -0.0962 0.9860 0.0138
-16.000 -1.0834 0.03122 0.02562 -0.0960 0.9854 0.0144
-15.750 -1.0675 0.03020 0.02456 -0.0959 0.9849 0.0150
-15.500 -1.0505 0.02926 0.02358 -0.0959 0.9843 0.0157
-15.250 -1.0346 0.02838 0.02266 -0.0955 0.9833 0.0164
-15.000 -1.0216 0.02762 0.02185 -0.0943 0.9813 0.0170
-14.750 -1.0066 0.02684 0.02102 -0.0935 0.9797 0.0175
-14.500 -0.9907 0.02604 0.02020 -0.0929 0.9784 0.0183
-14.250 -0.9729 0.02534 0.01947 -0.0925 0.9771 0.0190
-14.000 -0.9547 0.02465 0.01875 -0.0922 0.9759 0.0198
-13.750 -0.9363 0.02399 0.01805 -0.0918 0.9747 0.0204
-13.500 -0.9169 0.02338 0.01740 -0.0916 0.9737 0.0210
-13.250 -0.8974 0.02279 0.01675 -0.0913 0.9728 0.0216
-13.000 -0.8835 0.02218 0.01613 -0.0898 0.9704 0.0224
-12.750 -0.8672 0.02163 0.01555 -0.0887 0.9681 0.0231
-12.500 -0.8491 0.02111 0.01501 -0.0879 0.9661 0.0238
-12.250 -0.8305 0.02060 0.01447 -0.0872 0.9643 0.0245
-12.000 -0.8113 0.02011 0.01394 -0.0866 0.9628 0.0251
-11.750 -0.7912 0.01965 0.01344 -0.0861 0.9614 0.0257
-11.500 -0.7713 0.01924 0.01298 -0.0855 0.9598 0.0261
-11.250 -0.7552 0.01873 0.01246 -0.0842 0.9572 0.0270
-11.000 -0.7376 0.01827 0.01198 -0.0831 0.9548 0.0279
-10.750 -0.7188 0.01784 0.01153 -0.0822 0.9527 0.0287
-10.500 -0.6990 0.01744 0.01111 -0.0814 0.9508 0.0296
-10.250 -0.6785 0.01705 0.01069 -0.0808 0.9490 0.0304
-10.000 -0.6575 0.01667 0.01028 -0.0802 0.9472 0.0311
-9.750 -0.6378 0.01635 0.00993 -0.0794 0.9449 0.0316
-9.500 -0.6189 0.01597 0.00953 -0.0783 0.9425 0.0329
-9.250 -0.5990 0.01562 0.00917 -0.0775 0.9402 0.0341
-9.000 -0.5786 0.01528 0.00882 -0.0767 0.9379 0.0355
-8.750 -0.5575 0.01495 0.00848 -0.0760 0.9358 0.0369
-8.500 -0.5357 0.01464 0.00814 -0.0755 0.9338 0.0380
-8.250 -0.5149 0.01432 0.00782 -0.0747 0.9319 0.0406
-8.000 -0.4945 0.01403 0.00754 -0.0739 0.9296 0.0435
-7.750 -0.4735 0.01375 0.00727 -0.0731 0.9271 0.0469
-7.500 -0.4530 0.01344 0.00698 -0.0722 0.9245 0.0527
-7.250 -0.4324 0.01312 0.00669 -0.0713 0.9221 0.0608
-7.000 -0.4115 0.01279 0.00640 -0.0706 0.9201 0.0708
-6.750 -0.3897 0.01250 0.00613 -0.0699 0.9180 0.0806
-6.500 -0.3691 0.01224 0.00591 -0.0690 0.9156 0.0912
-6.250 -0.3486 0.01197 0.00569 -0.0680 0.9129 0.1038
-6.000 -0.3283 0.01168 0.00547 -0.0670 0.9103 0.1190
-5.750 -0.3082 0.01137 0.00523 -0.0660 0.9079 0.1374
-5.500 -0.2879 0.01105 0.00498 -0.0650 0.9055 0.1586
-5.250 -0.2676 0.01072 0.00473 -0.0640 0.9032 0.1840
-5.000 -0.2507 0.01036 0.00452 -0.0623 0.9005 0.2198
-4.750 -0.2346 0.00998 0.00430 -0.0604 0.8975 0.2607
-4.500 -0.2213 0.00951 0.00404 -0.0579 0.8943 0.3130
-4.250 -0.2110 0.00894 0.00372 -0.0548 0.8911 0.3792
-4.000 -0.2025 0.00833 0.00338 -0.0512 0.8880 0.4518
-3.750 -0.1985 0.00781 0.00312 -0.0465 0.8843 0.5135
-3.500 -0.1949 0.00733 0.00285 -0.0416 0.8801 0.5701
-3.250 -0.1975 0.00679 0.00255 -0.0352 0.8760 0.6325
-3.000 -0.1906 0.00645 0.00234 -0.0308 0.8727 0.6742
-2.750 -0.1831 0.00628 0.00227 -0.0264 0.8689 0.7026
-2.500 -0.1747 0.00612 0.00220 -0.0221 0.8651 0.7288
-2.250 -0.1624 0.00599 0.00214 -0.0187 0.8619 0.7516
-2.000 -0.1473 0.00590 0.00210 -0.0159 0.8590 0.7727
-1.750 -0.1401 0.00588 0.00214 -0.0113 0.8554 0.7906
-1.500 -0.1323 0.00590 0.00220 -0.0067 0.8514 0.8037
-1.250 -0.1197 0.00589 0.00217 -0.0033 0.8478 0.8127
-1.000 -0.0898 0.00589 0.00219 -0.0040 0.8457 0.8177
-0.750 -0.0644 0.00588 0.00216 -0.0037 0.8433 0.8229
-0.500 -0.0520 0.00588 0.00216 -0.0003 0.8397 0.8279
-0.250 -0.0253 0.00589 0.00219 -0.0003 0.8367 0.8307
0.000 0.0000 0.00589 0.00221 0.0000 0.8336 0.8336
0.250 0.0253 0.00589 0.00219 0.0003 0.8307 0.8367
0.500 0.0520 0.00588 0.00216 0.0003 0.8279 0.8397
0.750 0.0644 0.00588 0.00216 0.0037 0.8229 0.8433
1.000 0.0899 0.00589 0.00219 0.0040 0.8177 0.8457
1.250 0.1198 0.00589 0.00217 0.0033 0.8127 0.8479
1.500 0.1324 0.00590 0.00220 0.0067 0.8037 0.8514
1.750 0.1402 0.00588 0.00214 0.0112 0.7906 0.8554
2.000 0.1474 0.00590 0.00210 0.0159 0.7727 0.8590
2.250 0.1626 0.00599 0.00214 0.0187 0.7517 0.8619
2.500 0.1750 0.00611 0.00220 0.0220 0.7291 0.8651
2.750 0.1838 0.00627 0.00227 0.0262 0.7032 0.8689
3.000 0.1921 0.00644 0.00234 0.0304 0.6762 0.8727
3.250 0.1963 0.00681 0.00255 0.0355 0.6295 0.8760
3.500 0.1951 0.00733 0.00285 0.0416 0.5700 0.8801
3.750 0.1981 0.00783 0.00312 0.0466 0.5118 0.8843
4.000 0.2028 0.00833 0.00338 0.0511 0.4521 0.8880
4.250 0.2116 0.00893 0.00372 0.0546 0.3804 0.8910
4.500 0.2216 0.00951 0.00404 0.0578 0.3128 0.8943
4.750 0.2352 0.00997 0.00430 0.0602 0.2615 0.8975
5.000 0.2511 0.01036 0.00452 0.0622 0.2198 0.9004
5.250 0.2680 0.01072 0.00473 0.0639 0.1838 0.9031
5.500 0.2884 0.01105 0.00498 0.0649 0.1585 0.9055
5.750 0.3087 0.01137 0.00523 0.0659 0.1372 0.9079
6.250 0.3492 0.01196 0.00569 0.0679 0.1037 0.9129
6.500 0.3697 0.01223 0.00591 0.0689 0.0911 0.9156
6.750 0.3904 0.01249 0.00612 0.0698 0.0806 0.9180
7.000 0.4122 0.01279 0.00639 0.0704 0.0708 0.9200
7.250 0.4331 0.01311 0.00669 0.0712 0.0607 0.9221
7.500 0.4538 0.01344 0.00698 0.0720 0.0527 0.9244
7.750 0.4743 0.01375 0.00726 0.0729 0.0468 0.9270
8.000 0.4954 0.01402 0.00753 0.0737 0.0435 0.9295
8.250 0.5158 0.01431 0.00781 0.0745 0.0406 0.9319
8.500 0.5367 0.01463 0.00813 0.0752 0.0381 0.9338
8.750 0.5585 0.01494 0.00847 0.0758 0.0369 0.9358
9.000 0.5797 0.01527 0.00881 0.0765 0.0355 0.9379
9.250 0.6001 0.01561 0.00917 0.0772 0.0342 0.9402
9.500 0.6200 0.01596 0.00952 0.0781 0.0330 0.9425
9.750 0.6390 0.01634 0.00992 0.0791 0.0316 0.9449
10.000 0.6587 0.01667 0.01027 0.0800 0.0311 0.9472
10.250 0.6797 0.01704 0.01068 0.0805 0.0304 0.9489
10.500 0.7003 0.01743 0.01110 0.0812 0.0295 0.9507
10.750 0.7201 0.01783 0.01152 0.0819 0.0287 0.9526
11.000 0.7390 0.01826 0.01196 0.0828 0.0279 0.9547
11.250 0.7566 0.01872 0.01245 0.0839 0.0269 0.9572
11.500 0.7729 0.01922 0.01297 0.0852 0.0261 0.9597
11.750 0.7927 0.01964 0.01343 0.0858 0.0257 0.9614
12.000 0.8129 0.02010 0.01393 0.0863 0.0252 0.9628
12.250 0.8322 0.02059 0.01445 0.0869 0.0245 0.9644
12.500 0.8509 0.02109 0.01499 0.0876 0.0237 0.9661
12.750 0.8689 0.02161 0.01553 0.0884 0.0230 0.9682
13.000 0.8854 0.02216 0.01610 0.0894 0.0223 0.9704
13.250 0.8992 0.02277 0.01674 0.0909 0.0215 0.9728
13.500 0.9190 0.02336 0.01737 0.0912 0.0210 0.9738
13.750 0.9383 0.02396 0.01802 0.0915 0.0204 0.9748
14.000 0.9569 0.02462 0.01872 0.0918 0.0197 0.9759
14.250 0.9751 0.02531 0.01944 0.0921 0.0190 0.9772
14.500 0.9929 0.02601 0.02017 0.0925 0.0183 0.9785
14.750 1.0088 0.02680 0.02098 0.0931 0.0175 0.9799
15.000 1.0238 0.02757 0.02180 0.0939 0.0169 0.9815
15.250 1.0366 0.02833 0.02261 0.0952 0.0164 0.9836
15.500 1.0531 0.02922 0.02354 0.0954 0.0157 0.9844
15.750 1.0702 0.03016 0.02451 0.0954 0.0150 0.9850
16.000 1.0862 0.03118 0.02556 0.0955 0.0143 0.9855
16.250 1.1009 0.03229 0.02672 0.0956 0.0137 0.9861
16.500 1.1158 0.03341 0.02791 0.0957 0.0134 0.9866
16.750 1.1297 0.03462 0.02918 0.0958 0.0129 0.9871
17.000 1.1429 0.03590 0.03052 0.0959 0.0125 0.9877
17.250 1.1551 0.03728 0.03195 0.0960 0.0120 0.9884
17.500 1.1659 0.03876 0.03349 0.0961 0.0115 0.9891
17.750 1.1752 0.04037 0.03515 0.0964 0.0112 0.9899
18.000 1.1830 0.04209 0.03695 0.0967 0.0108 0.9907
18.250 1.1908 0.04383 0.03877 0.0969 0.0106 0.9916
18.500 1.1973 0.04567 0.04070 0.0972 0.0103 0.9925
18.750 1.2022 0.04766 0.04276 0.0975 0.0100 0.9935
19.000 1.2071 0.04986 0.04505 0.0974 0.0098 0.9941
19.250 1.2115 0.05229 0.04756 0.0969 0.0095 0.9944
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