NACA 63 (naca633418-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: NACA 63 (naca633418-il) Reynolds number: 500,000 Max Cl/Cd: 99.17 at α=7° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-naca633418-il-500000.txt Download as CSV file: xf-naca633418-il-500000.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 = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.500 -0.9281 0.10255 0.09878 -0.0532 1.0000 0.0242
-19.250 -0.9411 0.09683 0.09294 -0.0562 1.0000 0.0244
-19.000 -0.9484 0.09213 0.08815 -0.0586 1.0000 0.0245
-18.750 -0.9513 0.08818 0.08414 -0.0607 1.0000 0.0248
-18.500 -0.9543 0.08429 0.08020 -0.0627 1.0000 0.0250
-18.250 -0.9577 0.08036 0.07619 -0.0647 1.0000 0.0253
-18.000 -0.9613 0.07648 0.07222 -0.0666 1.0000 0.0255
-17.750 -0.9646 0.07274 0.06838 -0.0683 1.0000 0.0257
-17.500 -0.9673 0.06919 0.06473 -0.0699 1.0000 0.0259
-17.250 -0.9696 0.06572 0.06116 -0.0714 1.0000 0.0262
-17.000 -0.9700 0.06261 0.05794 -0.0726 1.0000 0.0265
-16.750 -0.9696 0.05970 0.05493 -0.0735 1.0000 0.0268
-16.500 -0.9685 0.05691 0.05203 -0.0745 1.0000 0.0271
-16.250 -0.9662 0.05433 0.04934 -0.0751 1.0000 0.0273
-16.000 -0.9631 0.05191 0.04682 -0.0757 1.0000 0.0276
-15.750 -0.9603 0.04949 0.04428 -0.0764 1.0000 0.0279
-15.500 -0.9543 0.04755 0.04227 -0.0762 1.0000 0.0282
-15.250 -0.9474 0.04580 0.04052 -0.0759 1.0000 0.0287
-15.000 -0.9401 0.04408 0.03879 -0.0759 1.0000 0.0291
-14.750 -0.9330 0.04236 0.03704 -0.0760 1.0000 0.0297
-14.500 -0.9257 0.04071 0.03535 -0.0759 1.0000 0.0302
-14.250 -0.9182 0.03911 0.03369 -0.0758 1.0000 0.0307
-14.000 -0.9102 0.03758 0.03210 -0.0756 1.0000 0.0312
-13.750 -0.9020 0.03610 0.03055 -0.0752 1.0000 0.0318
-13.500 -0.8930 0.03472 0.02911 -0.0748 1.0000 0.0322
-13.250 -0.8862 0.03326 0.02761 -0.0740 1.0000 0.0328
-13.000 -0.8797 0.03182 0.02619 -0.0732 1.0000 0.0335
-12.750 -0.8719 0.03053 0.02490 -0.0725 1.0000 0.0341
-12.500 -0.8638 0.02932 0.02367 -0.0717 1.0000 0.0348
-12.250 -0.8564 0.02816 0.02250 -0.0706 1.0000 0.0356
-12.000 -0.8433 0.02701 0.02131 -0.0705 0.9902 0.0365
-11.750 -0.8078 0.02546 0.01969 -0.0751 0.9696 0.0380
-11.500 -0.7689 0.02392 0.01814 -0.0804 0.9530 0.0399
-11.250 -0.7304 0.02275 0.01688 -0.0849 0.9333 0.0418
-11.000 -0.7070 0.02180 0.01577 -0.0862 0.9099 0.0433
-10.750 -0.6997 0.02065 0.01454 -0.0850 0.8897 0.0447
-10.500 -0.6894 0.01984 0.01366 -0.0837 0.8749 0.0464
-10.250 -0.6785 0.01912 0.01285 -0.0822 0.8626 0.0480
-10.000 -0.6669 0.01847 0.01208 -0.0806 0.8516 0.0497
-9.750 -0.6645 0.01752 0.01111 -0.0781 0.8405 0.0517
-9.250 -0.6398 0.01653 0.00997 -0.0747 0.8229 0.0564
-9.000 -0.6263 0.01587 0.00928 -0.0732 0.8150 0.0597
-8.750 -0.6070 0.01543 0.00880 -0.0723 0.8076 0.0635
-8.500 -0.5882 0.01490 0.00825 -0.0714 0.8004 0.0683
-8.250 -0.5666 0.01453 0.00782 -0.0708 0.7941 0.0737
-8.000 -0.5458 0.01399 0.00732 -0.0702 0.7871 0.0814
-7.750 -0.5238 0.01353 0.00686 -0.0697 0.7805 0.0913
-7.500 -0.5010 0.01307 0.00644 -0.0694 0.7744 0.1048
-7.250 -0.4775 0.01260 0.00603 -0.0691 0.7679 0.1232
-7.000 -0.4545 0.01205 0.00558 -0.0689 0.7618 0.1503
-6.750 -0.4309 0.01149 0.00516 -0.0687 0.7558 0.1860
-6.500 -0.4072 0.01085 0.00473 -0.0687 0.7495 0.2335
-6.250 -0.3830 0.01021 0.00431 -0.0688 0.7438 0.2890
-6.000 -0.3575 0.00971 0.00400 -0.0689 0.7382 0.3443
-5.750 -0.3302 0.00940 0.00382 -0.0691 0.7320 0.3864
-5.500 -0.3022 0.00923 0.00369 -0.0693 0.7263 0.4151
-5.250 -0.2736 0.00916 0.00358 -0.0695 0.7211 0.4360
-5.000 -0.2447 0.00907 0.00351 -0.0698 0.7152 0.4527
-4.750 -0.2159 0.00901 0.00343 -0.0700 0.7095 0.4663
-4.500 -0.1869 0.00901 0.00336 -0.0702 0.7042 0.4781
-4.250 -0.1576 0.00899 0.00331 -0.0705 0.6988 0.4896
-4.000 -0.1286 0.00895 0.00329 -0.0707 0.6933 0.4995
-3.750 -0.0993 0.00897 0.00322 -0.0710 0.6882 0.5088
-3.500 -0.0702 0.00897 0.00322 -0.0712 0.6829 0.5180
-3.250 -0.0409 0.00897 0.00319 -0.0715 0.6773 0.5268
-3.000 -0.0118 0.00898 0.00318 -0.0717 0.6723 0.5352
-2.750 0.0177 0.00905 0.00316 -0.0720 0.6676 0.5430
-2.500 0.0467 0.00901 0.00317 -0.0722 0.6624 0.5497
-2.250 0.0761 0.00903 0.00315 -0.0725 0.6572 0.5561
-2.000 0.1054 0.00905 0.00310 -0.0727 0.6523 0.5619
-1.750 0.1345 0.00904 0.00312 -0.0730 0.6474 0.5672
-1.500 0.1638 0.00905 0.00312 -0.0733 0.6424 0.5726
-1.250 0.1934 0.00909 0.00309 -0.0736 0.6377 0.5778
-1.000 0.2223 0.00911 0.00309 -0.0738 0.6331 0.5827
-0.750 0.2515 0.00910 0.00312 -0.0741 0.6283 0.5876
-0.500 0.2809 0.00912 0.00312 -0.0744 0.6232 0.5929
-0.250 0.3102 0.00915 0.00310 -0.0747 0.6187 0.5976
0.000 0.3392 0.00919 0.00315 -0.0749 0.6144 0.6023
0.250 0.3683 0.00921 0.00320 -0.0752 0.6097 0.6073
0.500 0.3976 0.00924 0.00321 -0.0755 0.6048 0.6123
0.750 0.4267 0.00928 0.00323 -0.0757 0.6004 0.6170
1.000 0.4556 0.00934 0.00330 -0.0760 0.5961 0.6219
1.250 0.4846 0.00937 0.00337 -0.0762 0.5913 0.6271
1.500 0.5138 0.00942 0.00339 -0.0765 0.5866 0.6320
1.750 0.5426 0.00947 0.00345 -0.0767 0.5822 0.6368
2.000 0.5713 0.00953 0.00355 -0.0769 0.5776 0.6420
2.250 0.6002 0.00957 0.00362 -0.0772 0.5726 0.6475
2.500 0.6290 0.00963 0.00366 -0.0774 0.5678 0.6524
2.750 0.6576 0.00973 0.00376 -0.0776 0.5631 0.6572
3.000 0.6860 0.00976 0.00387 -0.0777 0.5584 0.6626
3.250 0.7147 0.00983 0.00395 -0.0779 0.5533 0.6683
3.500 0.7429 0.00990 0.00403 -0.0781 0.5484 0.6734
3.750 0.7711 0.00999 0.00416 -0.0782 0.5435 0.6786
4.000 0.7993 0.01004 0.00427 -0.0783 0.5381 0.6843
4.250 0.8274 0.01012 0.00434 -0.0784 0.5323 0.6897
4.500 0.8548 0.01020 0.00447 -0.0784 0.5260 0.6950
4.750 0.8823 0.01025 0.00458 -0.0784 0.5191 0.7010
5.000 0.9100 0.01038 0.00468 -0.0784 0.5130 0.7067
5.250 0.9370 0.01042 0.00482 -0.0783 0.5063 0.7119
5.500 0.9635 0.01051 0.00492 -0.0781 0.4977 0.7177
5.750 0.9899 0.01060 0.00504 -0.0779 0.4870 0.7240
6.000 1.0152 0.01072 0.00517 -0.0775 0.4771 0.7297
6.250 1.0416 0.01080 0.00534 -0.0773 0.4681 0.7357
6.500 1.0673 0.01098 0.00550 -0.0771 0.4591 0.7420
6.750 1.0923 0.01109 0.00568 -0.0766 0.4483 0.7478
7.000 1.1167 0.01126 0.00588 -0.0761 0.4358 0.7543
7.500 1.1620 0.01172 0.00635 -0.0746 0.4040 0.7673
7.750 1.1827 0.01204 0.00664 -0.0735 0.3840 0.7742
8.000 1.2003 0.01247 0.00700 -0.0720 0.3594 0.7812
8.250 1.2138 0.01302 0.00746 -0.0698 0.3297 0.7886
8.500 1.2239 0.01372 0.00801 -0.0672 0.2984 0.7968
8.750 1.2274 0.01440 0.00861 -0.0633 0.2701 0.8049
9.000 1.2291 0.01528 0.00937 -0.0595 0.2426 0.8146
9.250 1.2291 0.01624 0.01026 -0.0556 0.2169 0.8247
9.500 1.2300 0.01729 0.01124 -0.0522 0.1925 0.8362
9.750 1.2298 0.01850 0.01237 -0.0490 0.1709 0.8495
10.000 1.2305 0.01971 0.01356 -0.0460 0.1517 0.8651
10.250 1.2302 0.02098 0.01484 -0.0430 0.1342 0.8851
10.500 1.2281 0.02226 0.01614 -0.0398 0.1190 0.9196
10.750 1.2339 0.02380 0.01766 -0.0388 0.1032 1.0000
11.000 1.2386 0.02548 0.01927 -0.0376 0.0911 1.0000
11.250 1.2439 0.02715 0.02090 -0.0365 0.0817 1.0000
11.500 1.2492 0.02885 0.02258 -0.0354 0.0743 1.0000
11.750 1.2522 0.03079 0.02448 -0.0343 0.0682 1.0000
12.000 1.2597 0.03241 0.02613 -0.0336 0.0636 1.0000
12.250 1.2613 0.03456 0.02826 -0.0327 0.0592 1.0000
12.500 1.2693 0.03623 0.02998 -0.0321 0.0559 1.0000
12.750 1.2723 0.03839 0.03214 -0.0314 0.0529 1.0000
13.000 1.2769 0.04047 0.03426 -0.0309 0.0502 1.0000
13.250 1.2831 0.04247 0.03631 -0.0305 0.0479 1.0000
13.500 1.2854 0.04490 0.03875 -0.0302 0.0459 1.0000
13.750 1.2882 0.04734 0.04123 -0.0299 0.0440 1.0000
14.000 1.2947 0.04947 0.04343 -0.0298 0.0423 1.0000
14.250 1.2991 0.05186 0.04586 -0.0298 0.0407 1.0000
14.500 1.3000 0.05468 0.04870 -0.0298 0.0395 1.0000
14.750 1.3013 0.05753 0.05161 -0.0299 0.0383 1.0000
15.000 1.3079 0.05984 0.05400 -0.0301 0.0371 1.0000
15.250 1.3129 0.06238 0.05659 -0.0304 0.0359 1.0000
15.500 1.3161 0.06517 0.05942 -0.0308 0.0348 1.0000
15.750 1.3158 0.06840 0.06268 -0.0313 0.0339 1.0000
16.000 1.3174 0.07148 0.06582 -0.0318 0.0331 1.0000
16.250 1.3225 0.07419 0.06862 -0.0323 0.0323 1.0000
16.500 1.3265 0.07706 0.07157 -0.0330 0.0315 1.0000
16.750 1.3298 0.08006 0.07463 -0.0337 0.0307 1.0000
17.000 1.3325 0.08318 0.07780 -0.0345 0.0300 1.0000
17.250 1.3333 0.08658 0.08123 -0.0355 0.0294 1.0000
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