NACA 64(3)-418 (naca643418-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 64(3)-418 (naca643418-il) Reynolds number: 1,000,000 Max Cl/Cd: 109.15 at α=5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-naca643418-il-1000000-n5.txt Download as CSV file: xf-naca643418-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NACA 64(3)-418
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 -1.0946 0.08244 0.07873 -0.0603 1.0000 0.0150
-19.500 -1.1024 0.07794 0.07414 -0.0624 1.0000 0.0151
-19.250 -1.1059 0.07415 0.07028 -0.0641 1.0000 0.0152
-19.000 -1.1076 0.07065 0.06670 -0.0656 1.0000 0.0154
-18.750 -1.1118 0.06692 0.06289 -0.0671 1.0000 0.0155
-18.500 -1.1118 0.06380 0.05969 -0.0684 1.0000 0.0156
-18.250 -1.1121 0.06071 0.05653 -0.0695 1.0000 0.0158
-18.000 -1.1113 0.05780 0.05355 -0.0706 1.0000 0.0159
-17.750 -1.1098 0.05505 0.05072 -0.0715 1.0000 0.0160
-17.500 -1.1068 0.05252 0.04813 -0.0722 1.0000 0.0162
-17.250 -1.1025 0.05019 0.04572 -0.0729 1.0000 0.0163
-17.000 -1.0982 0.04789 0.04336 -0.0734 1.0000 0.0165
-16.750 -1.0936 0.04568 0.04108 -0.0739 1.0000 0.0166
-16.500 -1.0874 0.04369 0.03903 -0.0743 1.0000 0.0167
-16.250 -1.0825 0.04162 0.03690 -0.0746 1.0000 0.0168
-16.000 -1.0787 0.03948 0.03471 -0.0748 1.0000 0.0170
-15.750 -1.0734 0.03757 0.03275 -0.0750 1.0000 0.0172
-15.500 -1.0661 0.03592 0.03107 -0.0749 1.0000 0.0175
-15.250 -1.0586 0.03431 0.02942 -0.0748 1.0000 0.0177
-15.000 -1.0497 0.03288 0.02795 -0.0747 1.0000 0.0178
-14.500 -1.0269 0.03008 0.02508 -0.0748 0.9747 0.0184
-14.250 -0.9806 0.02852 0.02345 -0.0817 0.9587 0.0188
-14.000 -0.9343 0.02702 0.02186 -0.0886 0.9423 0.0192
-13.750 -0.8998 0.02584 0.02052 -0.0928 0.9128 0.0195
-13.500 -0.8869 0.02488 0.01941 -0.0924 0.8851 0.0196
-13.250 -0.8760 0.02398 0.01839 -0.0914 0.8666 0.0199
-13.000 -0.8673 0.02297 0.01729 -0.0903 0.8506 0.0202
-12.750 -0.8573 0.02203 0.01628 -0.0892 0.8371 0.0205
-12.500 -0.8452 0.02123 0.01541 -0.0882 0.8256 0.0209
-12.250 -0.8334 0.02045 0.01455 -0.0871 0.8147 0.0212
-12.000 -0.8207 0.01968 0.01373 -0.0861 0.8045 0.0217
-11.750 -0.8075 0.01901 0.01299 -0.0850 0.7943 0.0220
-11.500 -0.7942 0.01834 0.01225 -0.0839 0.7836 0.0224
-11.250 -0.7807 0.01770 0.01155 -0.0827 0.7748 0.0226
-11.000 -0.7671 0.01708 0.01086 -0.0814 0.7656 0.0229
-10.750 -0.7531 0.01654 0.01025 -0.0801 0.7578 0.0233
-10.500 -0.7416 0.01590 0.00957 -0.0784 0.7501 0.0238
-10.250 -0.7314 0.01536 0.00898 -0.0764 0.7420 0.0243
-10.000 -0.7208 0.01494 0.00853 -0.0742 0.7350 0.0249
-9.750 -0.7031 0.01457 0.00811 -0.0731 0.7271 0.0254
-9.500 -0.6836 0.01424 0.00772 -0.0722 0.7206 0.0262
-9.250 -0.6624 0.01392 0.00737 -0.0715 0.7139 0.0267
-9.000 -0.6411 0.01360 0.00700 -0.0708 0.7074 0.0275
-8.750 -0.6191 0.01327 0.00665 -0.0702 0.7016 0.0284
-8.500 -0.5960 0.01298 0.00633 -0.0698 0.6955 0.0294
-8.250 -0.5722 0.01272 0.00603 -0.0694 0.6893 0.0305
-8.000 -0.5476 0.01249 0.00576 -0.0692 0.6839 0.0314
-7.750 -0.5232 0.01220 0.00546 -0.0689 0.6780 0.0330
-7.500 -0.4982 0.01196 0.00520 -0.0687 0.6720 0.0348
-7.250 -0.4726 0.01174 0.00495 -0.0686 0.6667 0.0367
-7.000 -0.4468 0.01149 0.00470 -0.0686 0.6613 0.0393
-6.750 -0.4207 0.01129 0.00447 -0.0685 0.6553 0.0421
-6.500 -0.3946 0.01107 0.00425 -0.0685 0.6497 0.0460
-6.250 -0.3680 0.01085 0.00403 -0.0685 0.6441 0.0509
-6.000 -0.3413 0.01064 0.00383 -0.0686 0.6382 0.0570
-5.750 -0.3147 0.01043 0.00363 -0.0686 0.6328 0.0653
-5.500 -0.2876 0.01019 0.00343 -0.0688 0.6283 0.0760
-5.250 -0.2603 0.00996 0.00324 -0.0689 0.6232 0.0884
-5.000 -0.2332 0.00973 0.00305 -0.0691 0.6181 0.1050
-4.750 -0.2062 0.00945 0.00285 -0.0693 0.6137 0.1301
-4.500 -0.1788 0.00913 0.00265 -0.0696 0.6093 0.1608
-4.250 -0.1517 0.00876 0.00243 -0.0699 0.6046 0.2022
-4.000 -0.1247 0.00835 0.00220 -0.0702 0.5999 0.2563
-3.750 -0.0976 0.00786 0.00196 -0.0706 0.5959 0.3258
-3.500 -0.0698 0.00742 0.00176 -0.0711 0.5920 0.3916
-3.250 -0.0410 0.00721 0.00170 -0.0715 0.5877 0.4416
-3.000 -0.0119 0.00715 0.00167 -0.0719 0.5835 0.4613
-2.750 0.0173 0.00714 0.00164 -0.0722 0.5795 0.4719
-2.500 0.0469 0.00711 0.00162 -0.0726 0.5762 0.4836
-2.250 0.0763 0.00707 0.00162 -0.0730 0.5724 0.4982
-2.000 0.1057 0.00706 0.00161 -0.0733 0.5684 0.5090
-1.750 0.1349 0.00708 0.00161 -0.0737 0.5644 0.5146
-1.500 0.1644 0.00710 0.00160 -0.0740 0.5609 0.5179
-1.250 0.1941 0.00711 0.00159 -0.0744 0.5576 0.5210
-1.000 0.2235 0.00710 0.00159 -0.0748 0.5543 0.5249
-0.750 0.2529 0.00711 0.00160 -0.0752 0.5509 0.5281
-0.500 0.2821 0.00714 0.00161 -0.0755 0.5476 0.5310
-0.250 0.3114 0.00718 0.00162 -0.0758 0.5446 0.5339
0.000 0.3410 0.00719 0.00163 -0.0762 0.5422 0.5365
0.250 0.3705 0.00721 0.00165 -0.0766 0.5395 0.5389
0.500 0.3999 0.00722 0.00168 -0.0770 0.5366 0.5419
0.750 0.4292 0.00725 0.00171 -0.0773 0.5338 0.5450
1.000 0.4583 0.00729 0.00174 -0.0776 0.5310 0.5482
1.250 0.4873 0.00734 0.00179 -0.0779 0.5282 0.5513
1.500 0.5167 0.00737 0.00183 -0.0783 0.5260 0.5543
1.750 0.5460 0.00740 0.00187 -0.0787 0.5230 0.5572
2.000 0.5751 0.00742 0.00192 -0.0790 0.5195 0.5608
2.250 0.6041 0.00747 0.00198 -0.0793 0.5160 0.5645
2.500 0.6327 0.00753 0.00205 -0.0795 0.5125 0.5683
2.750 0.6616 0.00759 0.00211 -0.0798 0.5094 0.5720
3.000 0.6908 0.00762 0.00218 -0.0802 0.5069 0.5758
3.250 0.7197 0.00766 0.00225 -0.0805 0.5035 0.5803
3.500 0.7479 0.00774 0.00233 -0.0806 0.4970 0.5849
3.750 0.7762 0.00781 0.00241 -0.0808 0.4896 0.5892
4.250 0.8318 0.00800 0.00260 -0.0810 0.4713 0.5974
4.500 0.8593 0.00811 0.00270 -0.0811 0.4622 0.6023
4.750 0.8871 0.00820 0.00281 -0.0812 0.4539 0.6071
5.000 0.9136 0.00837 0.00294 -0.0811 0.4379 0.6113
5.250 0.9366 0.00871 0.00315 -0.0805 0.3982 0.6162
5.500 0.9527 0.00948 0.00361 -0.0787 0.3363 0.6215
5.750 0.9711 0.01009 0.00403 -0.0774 0.2947 0.6266
6.000 0.9880 0.01075 0.00448 -0.0758 0.2513 0.6312
6.250 1.0045 0.01137 0.00494 -0.0742 0.2151 0.6368
6.500 1.0216 0.01191 0.00536 -0.0726 0.1864 0.6426
6.750 1.0382 0.01243 0.00578 -0.0710 0.1620 0.6479
7.000 1.0521 0.01298 0.00623 -0.0689 0.1385 0.6536
7.250 1.0620 0.01349 0.00666 -0.0660 0.1184 0.6599
7.500 1.0709 0.01409 0.00718 -0.0630 0.1011 0.6664
7.750 1.0800 0.01472 0.00777 -0.0603 0.0849 0.6732
8.000 1.0900 0.01536 0.00837 -0.0578 0.0724 0.6804
8.500 1.1130 0.01666 0.00964 -0.0537 0.0560 0.6939
8.750 1.1248 0.01736 0.01034 -0.0519 0.0499 0.7011
9.000 1.1365 0.01810 0.01109 -0.0502 0.0447 0.7077
9.500 1.1608 0.01966 0.01269 -0.0471 0.0368 0.7227
9.750 1.1723 0.02053 0.01359 -0.0456 0.0337 0.7300
10.000 1.1847 0.02139 0.01448 -0.0443 0.0314 0.7382
10.250 1.1965 0.02232 0.01544 -0.0430 0.0294 0.7457
10.500 1.2085 0.02326 0.01643 -0.0418 0.0277 0.7544
10.750 1.2194 0.02431 0.01752 -0.0405 0.0261 0.7629
11.000 1.2314 0.02530 0.01857 -0.0395 0.0250 0.7732
11.250 1.2426 0.02638 0.01970 -0.0384 0.0237 0.7827
11.500 1.2530 0.02754 0.02091 -0.0373 0.0227 0.7927
11.750 1.2635 0.02872 0.02216 -0.0363 0.0218 0.8034
12.000 1.2742 0.02991 0.02342 -0.0354 0.0209 0.8157
12.250 1.2839 0.03116 0.02475 -0.0344 0.0199 0.8309
12.500 1.2927 0.03249 0.02616 -0.0334 0.0191 0.8495
12.750 1.3011 0.03384 0.02761 -0.0324 0.0183 0.8712
13.000 1.3097 0.03514 0.02901 -0.0313 0.0177 0.8949
13.250 1.3167 0.03648 0.03049 -0.0301 0.0170 0.9368
13.750 1.3376 0.03974 0.03384 -0.0300 0.0156 1.0000
14.000 1.3475 0.04135 0.03549 -0.0296 0.0150 1.0000
14.250 1.3563 0.04308 0.03726 -0.0293 0.0145 1.0000
14.500 1.3647 0.04488 0.03909 -0.0290 0.0140 1.0000
14.750 1.3729 0.04673 0.04098 -0.0288 0.0137 1.0000
15.000 1.3802 0.04872 0.04300 -0.0287 0.0133 1.0000
15.250 1.3876 0.05073 0.04506 -0.0285 0.0128 1.0000
15.500 1.3952 0.05274 0.04712 -0.0285 0.0125 1.0000
15.750 1.4026 0.05482 0.04924 -0.0285 0.0123 1.0000
16.000 1.4094 0.05699 0.05147 -0.0286 0.0120 1.0000
16.250 1.4156 0.05927 0.05379 -0.0287 0.0117 1.0000
16.500 1.4216 0.06161 0.05618 -0.0289 0.0115 1.0000
16.750 1.4269 0.06406 0.05868 -0.0292 0.0113 1.0000
17.000 1.4316 0.06661 0.06128 -0.0296 0.0111 1.0000
17.250 1.4352 0.06936 0.06409 -0.0300 0.0109 1.0000
17.500 1.4381 0.07225 0.06704 -0.0305 0.0107 1.0000
17.750 1.4422 0.07502 0.06987 -0.0311 0.0106 1.0000
18.000 1.4455 0.07792 0.07284 -0.0317 0.0105 1.0000
18.250 1.4489 0.08087 0.07585 -0.0325 0.0104 1.0000
18.500 1.4512 0.08402 0.07908 -0.0333 0.0103 1.0000
18.750 1.4536 0.08719 0.08232 -0.0342 0.0102 1.0000
19.000 1.4544 0.09062 0.08583 -0.0353 0.0101 1.0000
19.250 1.4557 0.09399 0.08927 -0.0364 0.0099 1.0000
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