NACA 16-018 (naca16018-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: NACA 16-018 (naca16018-il) Reynolds number: 1,000,000 Max Cl/Cd: 47.06 at α=4° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-naca16018-il-1000000.txt Download as CSV file: xf-naca16018-il-1000000.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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.2050 0.07124 0.06729 -0.0784 0.9993 0.0132
-19.500 -1.2069 0.06749 0.06343 -0.0798 0.9988 0.0134
-19.250 -1.2068 0.06414 0.05998 -0.0810 0.9983 0.0136
-19.000 -1.2049 0.06110 0.05684 -0.0820 0.9978 0.0139
-18.750 -1.2017 0.05827 0.05392 -0.0828 0.9973 0.0141
-18.500 -1.1964 0.05575 0.05130 -0.0835 0.9967 0.0144
-18.250 -1.1902 0.05339 0.04883 -0.0841 0.9962 0.0146
-18.000 -1.1821 0.05126 0.04660 -0.0847 0.9957 0.0148
-17.750 -1.1874 0.04792 0.04316 -0.0845 0.9952 0.0152
-17.500 -1.1820 0.04563 0.04079 -0.0847 0.9947 0.0155
-17.250 -1.1720 0.04380 0.03890 -0.0850 0.9943 0.0159
-17.000 -1.1593 0.04225 0.03730 -0.0854 0.9940 0.0162
-16.750 -1.1487 0.04080 0.03579 -0.0851 0.9932 0.0166
-16.500 -1.1390 0.03942 0.03435 -0.0844 0.9918 0.0169
-16.250 -1.1268 0.03815 0.03300 -0.0841 0.9907 0.0174
-16.000 -1.1135 0.03693 0.03170 -0.0838 0.9897 0.0177
-15.750 -1.0969 0.03591 0.03060 -0.0839 0.9887 0.0180
-15.500 -1.0909 0.03407 0.02869 -0.0830 0.9879 0.0186
-15.250 -1.0772 0.03282 0.02740 -0.0828 0.9871 0.0191
-15.000 -1.0588 0.03192 0.02647 -0.0830 0.9864 0.0197
-14.750 -1.0397 0.03107 0.02558 -0.0833 0.9858 0.0202
-14.500 -1.0204 0.03022 0.02468 -0.0835 0.9853 0.0208
-14.250 -1.0000 0.02943 0.02383 -0.0839 0.9849 0.0214
-14.000 -0.9781 0.02874 0.02308 -0.0844 0.9845 0.0218
-13.750 -0.9657 0.02737 0.02164 -0.0838 0.9840 0.0226
-13.500 -0.9460 0.02647 0.02073 -0.0841 0.9837 0.0233
-13.250 -0.9232 0.02578 0.02001 -0.0847 0.9833 0.0240
-13.000 -0.9150 0.02525 0.01944 -0.0819 0.9795 0.0246
-12.750 -0.8955 0.02465 0.01881 -0.0816 0.9781 0.0253
-12.500 -0.8736 0.02409 0.01820 -0.0817 0.9771 0.0259
-12.250 -0.8520 0.02344 0.01750 -0.0818 0.9762 0.0265
-12.000 -0.8355 0.02238 0.01640 -0.0813 0.9755 0.0276
-11.750 -0.8122 0.02173 0.01574 -0.0818 0.9749 0.0285
-11.500 -0.7873 0.02117 0.01516 -0.0825 0.9744 0.0295
-11.250 -0.7628 0.02063 0.01458 -0.0830 0.9738 0.0304
-11.000 -0.7381 0.02012 0.01404 -0.0835 0.9733 0.0311
-10.750 -0.7154 0.01950 0.01338 -0.0837 0.9726 0.0319
-10.500 -0.6939 0.01880 0.01266 -0.0837 0.9719 0.0334
-10.250 -0.6703 0.01830 0.01215 -0.0839 0.9710 0.0347
-10.000 -0.6602 0.01797 0.01180 -0.0809 0.9668 0.0356
-9.750 -0.6394 0.01757 0.01137 -0.0803 0.9649 0.0366
-9.500 -0.6165 0.01721 0.01097 -0.0801 0.9634 0.0374
-9.250 -0.5966 0.01661 0.01037 -0.0794 0.9619 0.0398
-9.000 -0.5736 0.01615 0.00991 -0.0792 0.9607 0.0418
-8.750 -0.5498 0.01576 0.00949 -0.0792 0.9595 0.0437
-8.500 -0.5278 0.01534 0.00907 -0.0788 0.9581 0.0471
-8.250 -0.5126 0.01505 0.00880 -0.0768 0.9551 0.0510
-8.000 -0.4952 0.01468 0.00846 -0.0752 0.9522 0.0576
-7.750 -0.4761 0.01425 0.00809 -0.0741 0.9500 0.0690
-7.500 -0.4559 0.01381 0.00771 -0.0732 0.9481 0.0844
-7.250 -0.4358 0.01336 0.00735 -0.0724 0.9465 0.1028
-7.000 -0.4154 0.01294 0.00702 -0.0715 0.9448 0.1235
-6.750 -0.3992 0.01260 0.00678 -0.0697 0.9422 0.1462
-6.500 -0.3842 0.01223 0.00652 -0.0676 0.9389 0.1735
-6.250 -0.3692 0.01174 0.00619 -0.0656 0.9362 0.2102
-6.000 -0.3549 0.01117 0.00583 -0.0634 0.9338 0.2597
-5.750 -0.3423 0.01052 0.00542 -0.0609 0.9315 0.3221
-5.500 -0.3348 0.00991 0.00508 -0.0573 0.9284 0.3879
-5.250 -0.3331 0.00933 0.00477 -0.0523 0.9241 0.4533
-5.000 -0.3313 0.00866 0.00436 -0.0472 0.9204 0.5199
-4.750 -0.3311 0.00796 0.00391 -0.0416 0.9171 0.5866
-4.500 -0.3345 0.00749 0.00365 -0.0350 0.9130 0.6404
-4.250 -0.3348 0.00721 0.00351 -0.0289 0.9085 0.6801
-4.000 -0.3267 0.00694 0.00334 -0.0247 0.9052 0.7128
-3.750 -0.3128 0.00672 0.00319 -0.0217 0.9027 0.7407
-3.500 -0.2961 0.00660 0.00309 -0.0193 0.9004 0.7609
-3.250 -0.2903 0.00661 0.00315 -0.0144 0.8964 0.7746
-3.000 -0.2792 0.00660 0.00317 -0.0106 0.8928 0.7873
-2.750 -0.2620 0.00657 0.00313 -0.0083 0.8902 0.7971
-2.500 -0.2408 0.00652 0.00307 -0.0070 0.8881 0.8046
-2.250 -0.2141 0.00650 0.00305 -0.0069 0.8864 0.8128
-2.000 -0.2067 0.00656 0.00311 -0.0022 0.8828 0.8223
-1.750 -0.1873 0.00666 0.00325 -0.0003 0.8797 0.8321
-1.500 -0.1703 0.00671 0.00331 0.0021 0.8767 0.8421
-1.250 -0.1373 0.00679 0.00341 0.0008 0.8750 0.8477
-1.000 -0.1123 0.00678 0.00337 0.0012 0.8730 0.8524
-0.750 -0.0830 0.00676 0.00333 0.0007 0.8713 0.8559
-0.500 -0.0449 0.00680 0.00337 -0.0020 0.8698 0.8580
-0.250 -0.0237 0.00688 0.00347 -0.0007 0.8667 0.8608
0.000 0.0000 0.00690 0.00351 0.0000 0.8636 0.8636
0.250 0.0238 0.00688 0.00347 0.0007 0.8608 0.8667
0.500 0.0449 0.00680 0.00337 0.0020 0.8580 0.8698
0.750 0.0830 0.00676 0.00333 -0.0007 0.8559 0.8713
1.000 0.1123 0.00678 0.00337 -0.0012 0.8524 0.8730
1.250 0.1373 0.00679 0.00341 -0.0008 0.8477 0.8750
1.500 0.1703 0.00672 0.00331 -0.0021 0.8421 0.8767
1.750 0.1874 0.00666 0.00325 0.0003 0.8321 0.8797
2.000 0.2066 0.00656 0.00311 0.0023 0.8222 0.8828
2.250 0.2142 0.00650 0.00305 0.0069 0.8128 0.8864
2.500 0.2412 0.00652 0.00307 0.0069 0.8047 0.8881
2.750 0.2621 0.00657 0.00313 0.0083 0.7971 0.8902
3.000 0.2801 0.00660 0.00317 0.0104 0.7877 0.8927
3.250 0.2923 0.00662 0.00316 0.0139 0.7755 0.8962
3.500 0.2965 0.00660 0.00309 0.0192 0.7611 0.9003
3.750 0.3129 0.00672 0.00319 0.0216 0.7406 0.9027
4.000 0.3266 0.00694 0.00334 0.0247 0.7125 0.9052
4.250 0.3349 0.00721 0.00351 0.0289 0.6799 0.9085
4.500 0.3345 0.00750 0.00365 0.0350 0.6400 0.9130
4.750 0.3311 0.00796 0.00391 0.0416 0.5862 0.9171
5.000 0.3317 0.00866 0.00436 0.0471 0.5200 0.9204
5.250 0.3335 0.00933 0.00476 0.0522 0.4534 0.9241
5.500 0.3350 0.00992 0.00508 0.0573 0.3870 0.9284
6.000 0.3552 0.01117 0.00582 0.0634 0.2592 0.9338
6.250 0.3696 0.01174 0.00619 0.0655 0.2100 0.9362
6.500 0.3846 0.01223 0.00651 0.0675 0.1732 0.9389
6.750 0.3997 0.01260 0.00678 0.0696 0.1461 0.9421
7.000 0.4161 0.01294 0.00702 0.0714 0.1235 0.9448
7.250 0.4364 0.01335 0.00734 0.0722 0.1026 0.9465
7.500 0.4566 0.01380 0.00771 0.0731 0.0840 0.9481
7.750 0.4768 0.01424 0.00808 0.0740 0.0690 0.9500
8.000 0.4959 0.01467 0.00845 0.0751 0.0576 0.9522
8.250 0.5134 0.01504 0.00879 0.0766 0.0509 0.9551
8.500 0.5286 0.01534 0.00906 0.0786 0.0470 0.9581
8.750 0.5507 0.01575 0.00948 0.0790 0.0437 0.9595
9.000 0.5745 0.01614 0.00990 0.0791 0.0417 0.9607
9.250 0.5974 0.01660 0.01036 0.0792 0.0398 0.9619
9.500 0.6172 0.01720 0.01096 0.0799 0.0374 0.9634
9.750 0.6403 0.01756 0.01135 0.0801 0.0366 0.9649
10.000 0.6610 0.01796 0.01178 0.0807 0.0355 0.9669
10.250 0.6710 0.01828 0.01213 0.0837 0.0346 0.9711
10.500 0.6950 0.01879 0.01264 0.0834 0.0334 0.9719
10.750 0.7165 0.01950 0.01337 0.0835 0.0319 0.9727
11.000 0.7393 0.02011 0.01402 0.0833 0.0311 0.9733
11.250 0.7642 0.02060 0.01455 0.0828 0.0303 0.9739
11.500 0.7886 0.02114 0.01513 0.0822 0.0294 0.9745
11.750 0.8135 0.02170 0.01570 0.0816 0.0284 0.9750
12.000 0.8367 0.02236 0.01638 0.0811 0.0276 0.9755
12.250 0.8531 0.02343 0.01749 0.0816 0.0264 0.9763
12.500 0.8749 0.02407 0.01818 0.0814 0.0259 0.9772
12.750 0.8966 0.02463 0.01879 0.0813 0.0253 0.9783
13.000 0.9164 0.02519 0.01939 0.0816 0.0246 0.9798
13.250 0.9252 0.02575 0.01997 0.0843 0.0240 0.9834
13.500 0.9480 0.02644 0.02069 0.0837 0.0233 0.9837
13.750 0.9676 0.02734 0.02161 0.0834 0.0225 0.9841
14.000 0.9804 0.02869 0.02302 0.0840 0.0218 0.9845
14.250 1.0024 0.02938 0.02378 0.0835 0.0214 0.9849
14.500 1.0228 0.03017 0.02462 0.0831 0.0208 0.9854
14.750 1.0419 0.03103 0.02555 0.0829 0.0202 0.9859
15.000 1.0611 0.03188 0.02643 0.0826 0.0197 0.9865
15.250 1.0791 0.03280 0.02739 0.0824 0.0191 0.9872
15.500 1.0932 0.03403 0.02864 0.0826 0.0186 0.9880
15.750 1.0999 0.03581 0.03050 0.0835 0.0180 0.9889
16.000 1.1159 0.03687 0.03164 0.0834 0.0177 0.9898
16.250 1.1296 0.03806 0.03291 0.0836 0.0173 0.9909
16.500 1.1417 0.03933 0.03425 0.0840 0.0169 0.9921
16.750 1.1508 0.04071 0.03570 0.0849 0.0166 0.9935
17.000 1.1632 0.04213 0.03717 0.0848 0.0162 0.9941
17.250 1.1756 0.04370 0.03881 0.0844 0.0158 0.9944
17.500 1.1856 0.04554 0.04070 0.0841 0.0155 0.9948
17.750 1.1908 0.04786 0.04309 0.0839 0.0151 0.9953
18.000 1.1849 0.05125 0.04659 0.0841 0.0147 0.9958
18.250 1.1943 0.05325 0.04869 0.0835 0.0146 0.9963
18.500 1.2016 0.05550 0.05104 0.0829 0.0143 0.9969
18.750 1.2067 0.05805 0.05369 0.0822 0.0141 0.9974
19.000 1.2092 0.06094 0.05668 0.0814 0.0139 0.9980
19.250 1.2117 0.06392 0.05976 0.0804 0.0136 0.9985
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