NACA 16-018 (naca16018-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 16-018 (naca16018-il) Reynolds number: 500,000 Max Cl/Cd: 33.28 at α=3.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-naca16018-il-500000-n5.txt Download as CSV file: xf-naca16018-il-500000-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 = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.0909 0.08379 0.07948 -0.0801 0.9983 0.0128
-19.500 -1.1006 0.07873 0.07427 -0.0823 0.9978 0.0130
-19.250 -1.1077 0.07419 0.06959 -0.0841 0.9973 0.0132
-19.000 -1.1129 0.07006 0.06531 -0.0856 0.9967 0.0134
-18.750 -1.1159 0.06634 0.06144 -0.0869 0.9961 0.0136
-18.500 -1.1175 0.06288 0.05784 -0.0879 0.9955 0.0139
-18.250 -1.1184 0.05954 0.05441 -0.0888 0.9950 0.0142
-18.000 -1.1160 0.05667 0.05144 -0.0896 0.9944 0.0145
-17.750 -1.1110 0.05416 0.04884 -0.0903 0.9940 0.0149
-17.500 -1.1063 0.05195 0.04654 -0.0903 0.9931 0.0153
-17.250 -1.1010 0.04990 0.04440 -0.0901 0.9920 0.0157
-17.000 -1.0943 0.04798 0.04238 -0.0899 0.9909 0.0162
-16.750 -1.0867 0.04615 0.04044 -0.0897 0.9898 0.0167
-16.500 -1.0774 0.04444 0.03861 -0.0896 0.9888 0.0172
-16.250 -1.0686 0.04269 0.03678 -0.0894 0.9879 0.0176
-16.000 -1.0573 0.04117 0.03520 -0.0894 0.9870 0.0182
-15.750 -1.0448 0.03979 0.03376 -0.0894 0.9862 0.0187
-15.500 -1.0309 0.03853 0.03242 -0.0894 0.9856 0.0193
-15.250 -1.0165 0.03730 0.03111 -0.0894 0.9850 0.0200
-15.000 -1.0011 0.03616 0.02987 -0.0894 0.9845 0.0207
-14.750 -0.9843 0.03510 0.02870 -0.0896 0.9840 0.0213
-14.500 -0.9768 0.03397 0.02753 -0.0878 0.9815 0.0219
-14.250 -0.9640 0.03296 0.02647 -0.0869 0.9797 0.0226
-14.000 -0.9483 0.03205 0.02552 -0.0865 0.9784 0.0233
-13.750 -0.9316 0.03117 0.02457 -0.0862 0.9773 0.0240
-13.500 -0.9139 0.03032 0.02364 -0.0861 0.9764 0.0248
-13.250 -0.8947 0.02953 0.02277 -0.0861 0.9756 0.0256
-13.000 -0.8749 0.02874 0.02190 -0.0862 0.9749 0.0262
-12.750 -0.8576 0.02772 0.02086 -0.0861 0.9743 0.0272
-12.500 -0.8372 0.02691 0.02001 -0.0863 0.9737 0.0280
-12.250 -0.8159 0.02618 0.01923 -0.0866 0.9732 0.0290
-12.000 -0.8018 0.02560 0.01860 -0.0851 0.9709 0.0298
-11.750 -0.7875 0.02505 0.01800 -0.0835 0.9682 0.0306
-11.500 -0.7684 0.02446 0.01735 -0.0830 0.9666 0.0313
-11.250 -0.7496 0.02376 0.01660 -0.0826 0.9652 0.0322
-11.000 -0.7302 0.02303 0.01585 -0.0823 0.9640 0.0334
-10.750 -0.7089 0.02242 0.01522 -0.0822 0.9630 0.0345
-10.500 -0.6871 0.02186 0.01461 -0.0821 0.9621 0.0357
-10.250 -0.6646 0.02132 0.01403 -0.0822 0.9613 0.0369
-10.000 -0.6414 0.02080 0.01346 -0.0823 0.9605 0.0379
-9.750 -0.6321 0.02044 0.01307 -0.0792 0.9560 0.0389
-9.500 -0.6142 0.01993 0.01256 -0.0781 0.9537 0.0407
-9.250 -0.5939 0.01946 0.01207 -0.0775 0.9520 0.0425
-9.000 -0.5721 0.01902 0.01159 -0.0772 0.9506 0.0445
-8.750 -0.5493 0.01857 0.01112 -0.0770 0.9494 0.0467
-8.500 -0.5266 0.01808 0.01065 -0.0769 0.9482 0.0504
-8.000 -0.4916 0.01737 0.00995 -0.0741 0.9431 0.0610
-7.750 -0.4742 0.01701 0.00962 -0.0726 0.9403 0.0689
-7.500 -0.4539 0.01663 0.00926 -0.0718 0.9382 0.0786
-6.750 -0.3883 0.01535 0.00814 -0.0703 0.9336 0.1211
-6.500 -0.3704 0.01498 0.00785 -0.0690 0.9314 0.1404
-6.250 -0.3581 0.01470 0.00765 -0.0663 0.9273 0.1612
-6.000 -0.3420 0.01427 0.00734 -0.0645 0.9244 0.1914
-5.750 -0.3255 0.01374 0.00698 -0.0629 0.9221 0.2315
-5.500 -0.3097 0.01316 0.00660 -0.0611 0.9202 0.2797
-5.250 -0.2946 0.01254 0.00618 -0.0592 0.9184 0.3327
-5.000 -0.2917 0.01209 0.00596 -0.0545 0.9137 0.3837
-4.750 -0.2925 0.01143 0.00558 -0.0490 0.9092 0.4509
-4.500 -0.2970 0.01058 0.00506 -0.0426 0.9057 0.5302
-4.250 -0.3030 0.00978 0.00460 -0.0356 0.9025 0.6084
-4.000 -0.3168 0.00956 0.00459 -0.0265 0.8956 0.6560
-3.750 -0.3091 0.00928 0.00449 -0.0221 0.8924 0.7032
-3.500 -0.2876 0.00912 0.00442 -0.0209 0.8905 0.7318
-3.250 -0.2621 0.00902 0.00433 -0.0206 0.8890 0.7492
-3.000 -0.2484 0.00903 0.00437 -0.0175 0.8858 0.7652
-2.750 -0.2445 0.00910 0.00448 -0.0121 0.8808 0.7805
-2.500 -0.2250 0.00914 0.00457 -0.0103 0.8781 0.7989
-2.250 -0.2058 0.00919 0.00463 -0.0083 0.8759 0.8143
-2.000 -0.1713 0.00928 0.00472 -0.0099 0.8749 0.8219
-1.750 -0.1668 0.00924 0.00466 -0.0047 0.8713 0.8290
-1.500 -0.1421 0.00941 0.00484 -0.0042 0.8678 0.8325
-1.250 -0.1232 0.00945 0.00488 -0.0023 0.8647 0.8371
-1.000 -0.1166 0.00930 0.00468 0.0024 0.8613 0.8432
-0.750 -0.0764 0.00931 0.00469 -0.0008 0.8603 0.8445
-0.500 -0.0376 0.00931 0.00468 -0.0037 0.8593 0.8459
-0.250 0.0012 0.00931 0.00467 -0.0065 0.8583 0.8473
0.000 0.0000 0.00946 0.00485 0.0000 0.8520 0.8520
0.250 -0.0012 0.00931 0.00467 0.0065 0.8473 0.8583
0.500 0.0376 0.00931 0.00468 0.0037 0.8459 0.8593
0.750 0.0764 0.00931 0.00469 0.0008 0.8445 0.8603
1.000 0.1167 0.00930 0.00468 -0.0024 0.8432 0.8613
1.250 0.1233 0.00945 0.00488 0.0023 0.8371 0.8647
1.500 0.1422 0.00941 0.00484 0.0042 0.8325 0.8678
1.750 0.1670 0.00924 0.00466 0.0047 0.8290 0.8713
2.000 0.1715 0.00928 0.00472 0.0099 0.8219 0.8749
2.250 0.2059 0.00919 0.00463 0.0083 0.8143 0.8759
2.500 0.2252 0.00914 0.00457 0.0102 0.7989 0.8781
2.750 0.2444 0.00910 0.00448 0.0122 0.7805 0.8808
3.000 0.2482 0.00903 0.00437 0.0176 0.7651 0.8859
3.500 0.2877 0.00912 0.00442 0.0208 0.7318 0.8905
3.750 0.3088 0.00928 0.00449 0.0222 0.7018 0.8924
4.000 0.3165 0.00956 0.00459 0.0266 0.6551 0.8956
4.250 0.3038 0.00978 0.00460 0.0355 0.6087 0.9024
4.500 0.2972 0.01058 0.00506 0.0426 0.5300 0.9057
4.750 0.2924 0.01144 0.00558 0.0490 0.4500 0.9093
5.000 0.2919 0.01209 0.00595 0.0544 0.3834 0.9137
5.250 0.2948 0.01254 0.00618 0.0591 0.3325 0.9184
5.500 0.3101 0.01316 0.00659 0.0610 0.2796 0.9202
5.750 0.3258 0.01374 0.00698 0.0628 0.2311 0.9222
6.000 0.3423 0.01427 0.00734 0.0644 0.1909 0.9245
6.250 0.3585 0.01470 0.00764 0.0662 0.1611 0.9274
6.500 0.3708 0.01497 0.00784 0.0689 0.1403 0.9314
6.750 0.3888 0.01535 0.00813 0.0702 0.1209 0.9336
7.500 0.4544 0.01662 0.00925 0.0717 0.0786 0.9382
7.750 0.4747 0.01701 0.00961 0.0725 0.0688 0.9404
8.000 0.4921 0.01736 0.00994 0.0740 0.0610 0.9431
8.250 0.5036 0.01764 0.01019 0.0767 0.0548 0.9471
8.500 0.5273 0.01807 0.01064 0.0767 0.0505 0.9482
8.750 0.5500 0.01856 0.01111 0.0769 0.0467 0.9494
9.000 0.5729 0.01901 0.01158 0.0770 0.0445 0.9506
9.250 0.5947 0.01945 0.01206 0.0774 0.0425 0.9521
9.500 0.6150 0.01992 0.01254 0.0780 0.0407 0.9538
9.750 0.6328 0.02042 0.01305 0.0791 0.0389 0.9561
10.000 0.6424 0.02079 0.01344 0.0821 0.0379 0.9605
10.250 0.6657 0.02130 0.01401 0.0819 0.0369 0.9613
10.500 0.6882 0.02184 0.01460 0.0819 0.0357 0.9621
10.750 0.7100 0.02241 0.01520 0.0819 0.0345 0.9630
11.000 0.7313 0.02302 0.01583 0.0820 0.0334 0.9640
11.250 0.7508 0.02374 0.01658 0.0824 0.0322 0.9653
11.500 0.7697 0.02443 0.01732 0.0828 0.0313 0.9667
11.750 0.7885 0.02503 0.01797 0.0834 0.0306 0.9684
12.000 0.8014 0.02556 0.01856 0.0852 0.0298 0.9714
12.250 0.8175 0.02616 0.01921 0.0863 0.0289 0.9732
12.500 0.8389 0.02689 0.01999 0.0860 0.0280 0.9738
12.750 0.8593 0.02770 0.02084 0.0858 0.0272 0.9744
13.000 0.8766 0.02872 0.02188 0.0859 0.0263 0.9750
13.250 0.8966 0.02950 0.02274 0.0858 0.0256 0.9757
13.500 0.9158 0.03028 0.02360 0.0857 0.0248 0.9765
13.750 0.9335 0.03114 0.02454 0.0859 0.0240 0.9774
14.000 0.9502 0.03201 0.02547 0.0862 0.0233 0.9786
14.250 0.9661 0.03290 0.02641 0.0866 0.0225 0.9799
14.500 0.9785 0.03392 0.02747 0.0875 0.0219 0.9818
14.750 0.9870 0.03504 0.02864 0.0891 0.0213 0.9841
15.000 1.0037 0.03610 0.02981 0.0889 0.0207 0.9845
15.250 1.0193 0.03724 0.03104 0.0889 0.0200 0.9851
15.500 1.0338 0.03846 0.03235 0.0889 0.0193 0.9857
15.750 1.0477 0.03972 0.03369 0.0889 0.0187 0.9864
16.000 1.0602 0.04109 0.03512 0.0889 0.0181 0.9871
16.250 1.0714 0.04262 0.03671 0.0890 0.0176 0.9880
16.500 1.0803 0.04436 0.03853 0.0891 0.0171 0.9890
16.750 1.0895 0.04608 0.04037 0.0893 0.0167 0.9901
17.000 1.0974 0.04789 0.04228 0.0894 0.0161 0.9912
17.250 1.1041 0.04979 0.04429 0.0896 0.0157 0.9923
17.500 1.1097 0.05182 0.04641 0.0899 0.0152 0.9934
17.750 1.1150 0.05405 0.04872 0.0897 0.0148 0.9941
18.000 1.1199 0.05657 0.05134 0.0890 0.0144 0.9946
18.250 1.1222 0.05945 0.05431 0.0882 0.0141 0.9951
18.500 1.1210 0.06283 0.05778 0.0873 0.0138 0.9957
18.750 1.1200 0.06622 0.06132 0.0863 0.0136 0.9963
19.000 1.1169 0.06996 0.06521 0.0850 0.0134 0.9969
19.250 1.1120 0.07406 0.06945 0.0835 0.0132 0.9975
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