NACA 63 (naca633418-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 63 (naca633418-il) Reynolds number: 1,000,000 Max Cl/Cd: 106.93 at α=5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-naca633418-il-1000000-n5.txt Download as CSV file: xf-naca633418-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NACA 63
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 -1.0901 0.08701 0.08322 -0.0531 1.0000 0.0142
-19.500 -1.0992 0.08229 0.07840 -0.0553 1.0000 0.0142
-19.250 -1.1022 0.07855 0.07458 -0.0570 1.0000 0.0145
-19.000 -1.1099 0.07419 0.07013 -0.0590 1.0000 0.0145
-18.750 -1.1139 0.07038 0.06625 -0.0606 1.0000 0.0146
-18.500 -1.1198 0.06645 0.06223 -0.0623 1.0000 0.0147
-18.250 -1.1237 0.06280 0.05853 -0.0638 1.0000 0.0150
-18.000 -1.1260 0.05945 0.05511 -0.0651 1.0000 0.0152
-17.750 -1.1261 0.05643 0.05201 -0.0662 1.0000 0.0152
-17.500 -1.1258 0.05353 0.04905 -0.0672 1.0000 0.0153
-17.250 -1.1211 0.05116 0.04665 -0.0680 1.0000 0.0159
-17.000 -1.1182 0.04863 0.04407 -0.0687 1.0000 0.0161
-16.750 -1.1166 0.04604 0.04140 -0.0694 1.0000 0.0161
-16.500 -1.1091 0.04412 0.03944 -0.0699 1.0000 0.0165
-16.250 -1.1047 0.04191 0.03717 -0.0704 1.0000 0.0166
-16.000 -1.0992 0.03988 0.03508 -0.0708 1.0000 0.0168
-15.750 -1.0919 0.03809 0.03324 -0.0710 1.0000 0.0171
-15.500 -1.0856 0.03628 0.03137 -0.0711 1.0000 0.0172
-15.250 -1.0783 0.03460 0.02963 -0.0711 1.0000 0.0173
-15.000 -1.0726 0.03282 0.02781 -0.0711 1.0000 0.0176
-14.750 -1.0658 0.03118 0.02614 -0.0710 1.0000 0.0180
-14.500 -1.0603 0.02965 0.02459 -0.0701 0.9782 0.0183
-14.250 -1.0122 0.02794 0.02282 -0.0777 0.9561 0.0190
-14.000 -0.9596 0.02638 0.02116 -0.0859 0.9314 0.0197
-13.750 -0.9352 0.02530 0.01988 -0.0880 0.8906 0.0201
-13.500 -0.9256 0.02433 0.01877 -0.0870 0.8667 0.0204
-13.000 -0.9074 0.02232 0.01658 -0.0850 0.8366 0.0213
-12.750 -0.8971 0.02139 0.01558 -0.0839 0.8250 0.0217
-12.500 -0.8862 0.02054 0.01466 -0.0828 0.8142 0.0222
-12.250 -0.8741 0.01972 0.01379 -0.0818 0.8049 0.0228
-12.000 -0.8619 0.01898 0.01297 -0.0807 0.7957 0.0234
-11.750 -0.8486 0.01827 0.01221 -0.0797 0.7877 0.0239
-11.500 -0.8369 0.01755 0.01143 -0.0783 0.7792 0.0245
-11.250 -0.8254 0.01686 0.01069 -0.0769 0.7715 0.0252
-11.000 -0.8146 0.01622 0.01001 -0.0752 0.7638 0.0260
-10.750 -0.8063 0.01570 0.00943 -0.0729 0.7569 0.0267
-10.500 -0.7910 0.01526 0.00895 -0.0716 0.7505 0.0276
-10.250 -0.7727 0.01485 0.00850 -0.0706 0.7437 0.0286
-10.000 -0.7532 0.01445 0.00807 -0.0698 0.7374 0.0299
-9.750 -0.7317 0.01410 0.00769 -0.0692 0.7311 0.0313
-9.500 -0.7092 0.01380 0.00733 -0.0687 0.7251 0.0324
-9.250 -0.6868 0.01344 0.00696 -0.0682 0.7197 0.0341
-9.000 -0.6630 0.01313 0.00663 -0.0679 0.7137 0.0360
-8.750 -0.6386 0.01287 0.00632 -0.0677 0.7074 0.0376
-8.500 -0.6144 0.01256 0.00601 -0.0674 0.7018 0.0401
-8.250 -0.5890 0.01229 0.00573 -0.0673 0.6963 0.0427
-8.000 -0.5637 0.01202 0.00543 -0.0672 0.6902 0.0457
-7.750 -0.5379 0.01178 0.00517 -0.0671 0.6846 0.0489
-7.500 -0.5118 0.01151 0.00491 -0.0671 0.6792 0.0532
-7.250 -0.4853 0.01127 0.00466 -0.0671 0.6734 0.0580
-7.000 -0.4589 0.01103 0.00442 -0.0671 0.6680 0.0639
-6.750 -0.4320 0.01077 0.00419 -0.0672 0.6626 0.0712
-6.500 -0.4050 0.01053 0.00396 -0.0673 0.6568 0.0793
-6.000 -0.3506 0.01003 0.00352 -0.0676 0.6465 0.1026
-5.750 -0.3232 0.00977 0.00331 -0.0678 0.6409 0.1183
-5.500 -0.2957 0.00952 0.00310 -0.0680 0.6354 0.1377
-5.250 -0.2682 0.00922 0.00289 -0.0683 0.6310 0.1614
-5.000 -0.2404 0.00889 0.00268 -0.0686 0.6263 0.1910
-4.750 -0.2126 0.00857 0.00247 -0.0689 0.6210 0.2255
-4.250 -0.1566 0.00790 0.00208 -0.0697 0.6114 0.3066
-4.000 -0.1280 0.00763 0.00194 -0.0701 0.6067 0.3446
-3.750 -0.0992 0.00743 0.00183 -0.0705 0.6020 0.3787
-3.500 -0.0701 0.00733 0.00176 -0.0708 0.5977 0.4021
-3.250 -0.0406 0.00724 0.00171 -0.0712 0.5935 0.4193
-3.000 -0.0111 0.00717 0.00166 -0.0716 0.5887 0.4352
-2.750 0.0182 0.00712 0.00163 -0.0719 0.5836 0.4488
-2.500 0.0476 0.00709 0.00160 -0.0723 0.5795 0.4603
-2.250 0.0773 0.00707 0.00158 -0.0727 0.5756 0.4708
-2.000 0.1069 0.00703 0.00157 -0.0730 0.5713 0.4801
-1.750 0.1364 0.00704 0.00156 -0.0734 0.5669 0.4871
-1.500 0.1658 0.00705 0.00155 -0.0737 0.5625 0.4935
-1.250 0.1955 0.00704 0.00155 -0.0741 0.5583 0.5000
-1.000 0.2252 0.00705 0.00155 -0.0744 0.5540 0.5052
-0.750 0.2546 0.00706 0.00155 -0.0747 0.5498 0.5103
-0.500 0.2839 0.00708 0.00156 -0.0751 0.5456 0.5156
-0.250 0.3136 0.00709 0.00158 -0.0754 0.5418 0.5206
0.000 0.3431 0.00712 0.00159 -0.0758 0.5373 0.5248
0.250 0.3724 0.00714 0.00162 -0.0761 0.5330 0.5294
0.500 0.4016 0.00718 0.00165 -0.0764 0.5287 0.5343
0.750 0.4312 0.00720 0.00168 -0.0767 0.5250 0.5390
1.000 0.4606 0.00724 0.00171 -0.0770 0.5203 0.5427
1.250 0.4897 0.00727 0.00175 -0.0773 0.5156 0.5474
1.500 0.5187 0.00733 0.00180 -0.0776 0.5109 0.5524
1.750 0.5481 0.00736 0.00185 -0.0779 0.5064 0.5570
2.000 0.5772 0.00741 0.00190 -0.0782 0.5012 0.5608
2.250 0.6059 0.00748 0.00196 -0.0784 0.4961 0.5654
2.500 0.6350 0.00752 0.00203 -0.0787 0.4916 0.5706
2.750 0.6640 0.00757 0.00209 -0.0790 0.4863 0.5754
3.000 0.6925 0.00765 0.00217 -0.0791 0.4805 0.5796
3.250 0.7212 0.00772 0.00225 -0.0794 0.4755 0.5843
3.500 0.7499 0.00778 0.00233 -0.0796 0.4690 0.5891
3.750 0.7778 0.00791 0.00243 -0.0797 0.4605 0.5940
4.000 0.8061 0.00799 0.00253 -0.0799 0.4516 0.5988
4.250 0.8338 0.00811 0.00264 -0.0799 0.4435 0.6041
4.500 0.8620 0.00820 0.00275 -0.0801 0.4355 0.6091
4.750 0.8891 0.00836 0.00288 -0.0800 0.4247 0.6135
5.000 0.9153 0.00856 0.00304 -0.0799 0.4066 0.6182
5.250 0.9402 0.00884 0.00324 -0.0795 0.3818 0.6238
5.500 0.9649 0.00915 0.00346 -0.0791 0.3598 0.6292
5.750 0.9891 0.00946 0.00369 -0.0787 0.3369 0.6339
6.000 1.0118 0.00986 0.00399 -0.0780 0.3117 0.6389
6.250 1.0329 0.01034 0.00434 -0.0771 0.2818 0.6441
6.500 1.0517 0.01094 0.00477 -0.0758 0.2472 0.6492
6.750 1.0696 0.01153 0.00521 -0.0745 0.2150 0.6542
7.000 1.0880 0.01206 0.00563 -0.0731 0.1890 0.6600
7.250 1.1049 0.01261 0.00608 -0.0716 0.1652 0.6654
7.500 1.1218 0.01313 0.00651 -0.0700 0.1462 0.6701
7.750 1.1369 0.01363 0.00695 -0.0681 0.1297 0.6755
8.000 1.1472 0.01413 0.00740 -0.0653 0.1147 0.6818
8.250 1.1573 0.01471 0.00792 -0.0626 0.1014 0.6872
8.500 1.1682 0.01528 0.00848 -0.0602 0.0906 0.6930
8.750 1.1792 0.01590 0.00907 -0.0579 0.0811 0.6990
9.000 1.1903 0.01656 0.00972 -0.0558 0.0732 0.7050
9.250 1.2003 0.01730 0.01046 -0.0537 0.0656 0.7111
9.750 1.2233 0.01882 0.01200 -0.0503 0.0556 0.7242
10.000 1.2339 0.01968 0.01288 -0.0486 0.0514 0.7308
10.250 1.2461 0.02051 0.01374 -0.0472 0.0481 0.7383
10.500 1.2562 0.02149 0.01474 -0.0457 0.0446 0.7453
10.750 1.2684 0.02239 0.01568 -0.0444 0.0422 0.7531
11.000 1.2788 0.02344 0.01676 -0.0431 0.0397 0.7607
11.250 1.2897 0.02447 0.01784 -0.0419 0.0378 0.7695
11.500 1.3005 0.02556 0.01898 -0.0408 0.0357 0.7786
11.750 1.3100 0.02676 0.02022 -0.0397 0.0338 0.7881
12.000 1.3201 0.02795 0.02147 -0.0386 0.0321 0.7980
12.250 1.3295 0.02920 0.02279 -0.0376 0.0306 0.8105
12.500 1.3377 0.03058 0.02422 -0.0366 0.0291 0.8237
12.750 1.3466 0.03190 0.02564 -0.0357 0.0281 0.8402
13.000 1.3545 0.03328 0.02712 -0.0346 0.0270 0.8620
13.250 1.3600 0.03466 0.02864 -0.0332 0.0259 0.9040
14.250 1.3949 0.04145 0.03567 -0.0321 0.0223 1.0000
14.500 1.4022 0.04335 0.03761 -0.0318 0.0217 1.0000
14.750 1.4079 0.04543 0.03973 -0.0315 0.0210 1.0000
15.000 1.4158 0.04736 0.04170 -0.0314 0.0206 1.0000
15.250 1.4228 0.04940 0.04380 -0.0313 0.0201 1.0000
15.500 1.4288 0.05161 0.04605 -0.0313 0.0196 1.0000
15.750 1.4350 0.05381 0.04830 -0.0313 0.0191 1.0000
16.000 1.4395 0.05626 0.05079 -0.0315 0.0186 1.0000
16.250 1.4438 0.05877 0.05334 -0.0317 0.0180 1.0000
16.500 1.4479 0.06136 0.05598 -0.0320 0.0177 1.0000
16.750 1.4532 0.06386 0.05855 -0.0323 0.0173 1.0000
17.000 1.4578 0.06645 0.06121 -0.0327 0.0170 1.0000
17.250 1.4615 0.06924 0.06405 -0.0333 0.0166 1.0000
17.500 1.4654 0.07201 0.06688 -0.0338 0.0162 1.0000
17.750 1.4674 0.07509 0.07003 -0.0345 0.0160 1.0000
18.000 1.4698 0.07815 0.07314 -0.0353 0.0156 1.0000
18.250 1.4705 0.08149 0.07653 -0.0362 0.0153 1.0000
18.500 1.4706 0.08498 0.08009 -0.0372 0.0150 1.0000
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