NACA 63(3)-618 (naca633618-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 63(3)-618 (naca633618-il) Reynolds number: 200,000 Max Cl/Cd: 73.37 at α=7.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-naca633618-il-200000-n5.txt Download as CSV file: xf-naca633618-il-200000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NACA 63(3)-618
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-17.250 -0.6652 0.10265 0.09802 -0.0671 1.0000 0.0263
-17.000 -0.7052 0.09128 0.08638 -0.0739 1.0000 0.0264
-16.750 -0.7357 0.08237 0.07720 -0.0793 1.0000 0.0266
-16.500 -0.7434 0.07779 0.07254 -0.0818 1.0000 0.0269
-16.250 -0.7495 0.07362 0.06829 -0.0839 1.0000 0.0271
-16.000 -0.7526 0.07003 0.06465 -0.0857 1.0000 0.0275
-15.750 -0.7578 0.06626 0.06080 -0.0875 1.0000 0.0279
-15.500 -0.7630 0.06265 0.05709 -0.0892 1.0000 0.0283
-15.250 -0.7680 0.05923 0.05354 -0.0905 1.0000 0.0287
-15.000 -0.7730 0.05598 0.05016 -0.0917 1.0000 0.0294
-14.750 -0.7783 0.05287 0.04688 -0.0925 1.0000 0.0301
-14.500 -0.7827 0.05002 0.04383 -0.0929 1.0000 0.0307
-14.250 -0.7807 0.04803 0.04183 -0.0929 1.0000 0.0312
-14.000 -0.7782 0.04620 0.03998 -0.0927 1.0000 0.0317
-13.750 -0.7763 0.04442 0.03817 -0.0923 1.0000 0.0322
-13.500 -0.7749 0.04271 0.03641 -0.0917 1.0000 0.0329
-13.250 -0.7750 0.04109 0.03472 -0.0908 1.0000 0.0337
-12.750 -0.7509 0.03745 0.03085 -0.0929 0.9834 0.0357
-12.500 -0.7275 0.03582 0.02920 -0.0957 0.9718 0.0368
-12.250 -0.7022 0.03422 0.02751 -0.0987 0.9605 0.0381
-12.000 -0.6753 0.03267 0.02581 -0.1016 0.9492 0.0397
-11.750 -0.6466 0.03120 0.02424 -0.1046 0.9387 0.0412
-11.500 -0.6189 0.02989 0.02287 -0.1074 0.9265 0.0427
-11.250 -0.5923 0.02870 0.02157 -0.1096 0.9143 0.0444
-11.000 -0.5668 0.02764 0.02033 -0.1112 0.9025 0.0461
-10.750 -0.5471 0.02657 0.01924 -0.1119 0.8899 0.0475
-10.500 -0.5302 0.02567 0.01828 -0.1119 0.8777 0.0491
-10.250 -0.5133 0.02484 0.01734 -0.1117 0.8669 0.0509
-10.000 -0.4986 0.02409 0.01647 -0.1108 0.8558 0.0523
-9.750 -0.4870 0.02322 0.01556 -0.1097 0.8460 0.0539
-9.500 -0.4762 0.02248 0.01477 -0.1083 0.8361 0.0554
-9.250 -0.4656 0.02184 0.01406 -0.1067 0.8274 0.0571
-9.000 -0.4517 0.02122 0.01334 -0.1056 0.8187 0.0590
-8.750 -0.4366 0.02054 0.01258 -0.1046 0.8116 0.0608
-8.500 -0.4210 0.01991 0.01193 -0.1037 0.8035 0.0630
-8.250 -0.4023 0.01938 0.01131 -0.1030 0.7966 0.0659
-8.000 -0.3832 0.01883 0.01071 -0.1023 0.7899 0.0691
-7.750 -0.3636 0.01828 0.01013 -0.1018 0.7828 0.0729
-7.500 -0.3417 0.01780 0.00958 -0.1014 0.7769 0.0778
-7.250 -0.3201 0.01728 0.00906 -0.1010 0.7706 0.0847
-7.000 -0.2977 0.01678 0.00856 -0.1008 0.7639 0.0941
-6.750 -0.2742 0.01629 0.00807 -0.1007 0.7583 0.1080
-6.500 -0.2502 0.01582 0.00763 -0.1006 0.7526 0.1266
-6.250 -0.2261 0.01530 0.00720 -0.1007 0.7463 0.1524
-6.000 -0.2013 0.01475 0.00675 -0.1009 0.7407 0.1858
-5.750 -0.1761 0.01415 0.00632 -0.1013 0.7354 0.2319
-5.500 -0.1504 0.01359 0.00597 -0.1017 0.7293 0.2861
-5.250 -0.1236 0.01315 0.00573 -0.1021 0.7238 0.3424
-5.000 -0.0954 0.01293 0.00559 -0.1024 0.7192 0.3883
-4.750 -0.0675 0.01282 0.00555 -0.1026 0.7130 0.4208
-4.500 -0.0390 0.01277 0.00549 -0.1029 0.7075 0.4479
-4.250 -0.0101 0.01276 0.00544 -0.1031 0.7028 0.4695
-4.000 0.0187 0.01277 0.00542 -0.1033 0.6975 0.4865
-3.750 0.0471 0.01279 0.00542 -0.1034 0.6917 0.4999
-3.500 0.0758 0.01280 0.00538 -0.1035 0.6867 0.5100
-3.250 0.1053 0.01283 0.00529 -0.1038 0.6824 0.5212
-3.000 0.1331 0.01287 0.00537 -0.1038 0.6768 0.5313
-2.750 0.1622 0.01290 0.00532 -0.1041 0.6715 0.5413
-2.500 0.1907 0.01291 0.00529 -0.1041 0.6668 0.5469
-2.250 0.2196 0.01293 0.00526 -0.1043 0.6621 0.5534
-2.000 0.2485 0.01294 0.00522 -0.1046 0.6569 0.5599
-1.750 0.2768 0.01296 0.00523 -0.1047 0.6521 0.5648
-1.500 0.3059 0.01299 0.00519 -0.1049 0.6479 0.5707
-1.250 0.3349 0.01302 0.00517 -0.1052 0.6428 0.5769
-1.000 0.3629 0.01304 0.00521 -0.1053 0.6376 0.5816
-0.750 0.3914 0.01307 0.00522 -0.1054 0.6332 0.5864
-0.500 0.4207 0.01312 0.00520 -0.1058 0.6294 0.5920
-0.250 0.4495 0.01317 0.00523 -0.1061 0.6246 0.5975
0.000 0.4772 0.01320 0.00531 -0.1061 0.6195 0.6014
0.250 0.5057 0.01325 0.00534 -0.1062 0.6150 0.6062
0.500 0.5349 0.01332 0.00534 -0.1065 0.6112 0.6120
0.750 0.5632 0.01339 0.00544 -0.1068 0.6066 0.6172
1.000 0.5908 0.01346 0.00556 -0.1068 0.6019 0.6214
1.250 0.6191 0.01353 0.00563 -0.1069 0.5976 0.6263
1.500 0.6482 0.01361 0.00566 -0.1072 0.5937 0.6319
1.750 0.6759 0.01370 0.00580 -0.1073 0.5890 0.6372
2.000 0.7032 0.01380 0.00596 -0.1073 0.5844 0.6421
2.250 0.7313 0.01389 0.00607 -0.1074 0.5801 0.6476
2.500 0.7603 0.01400 0.00612 -0.1078 0.5762 0.6534
2.750 0.7872 0.01411 0.00632 -0.1077 0.5715 0.6581
3.000 0.8141 0.01423 0.00651 -0.1076 0.5666 0.6634
3.250 0.8419 0.01434 0.00663 -0.1077 0.5620 0.6698
3.750 0.8961 0.01460 0.00699 -0.1076 0.5528 0.6806
4.000 0.9228 0.01474 0.00719 -0.1076 0.5477 0.6866
4.250 0.9507 0.01487 0.00733 -0.1077 0.5432 0.6933
4.500 0.9772 0.01502 0.00753 -0.1075 0.5388 0.6986
4.750 1.0027 0.01518 0.00780 -0.1072 0.5334 0.7050
5.000 1.0294 0.01534 0.00800 -0.1072 0.5281 0.7118
5.250 1.0559 0.01548 0.00816 -0.1070 0.5234 0.7173
5.500 1.0799 0.01565 0.00847 -0.1065 0.5169 0.7240
5.750 1.1052 0.01581 0.00867 -0.1061 0.5101 0.7313
6.000 1.1291 0.01596 0.00888 -0.1055 0.5031 0.7371
6.250 1.1521 0.01613 0.00914 -0.1048 0.4946 0.7442
6.500 1.1763 0.01631 0.00934 -0.1042 0.4873 0.7513
6.750 1.1974 0.01650 0.00966 -0.1032 0.4785 0.7582
7.000 1.2201 0.01671 0.00988 -0.1024 0.4699 0.7660
7.250 1.2398 0.01692 0.01022 -0.1011 0.4601 0.7729
7.500 1.2597 0.01717 0.01052 -0.0999 0.4506 0.7810
7.750 1.2774 0.01744 0.01083 -0.0983 0.4389 0.7890
8.000 1.2915 0.01775 0.01120 -0.0961 0.4240 0.7975
8.250 1.3004 0.01813 0.01157 -0.0931 0.4061 0.8066
8.500 1.3061 0.01864 0.01207 -0.0896 0.3858 0.8165
8.750 1.3111 0.01929 0.01270 -0.0863 0.3634 0.8272
9.000 1.3142 0.02012 0.01349 -0.0829 0.3415 0.8393
9.250 1.3147 0.02110 0.01443 -0.0794 0.3210 0.8525
9.500 1.3145 0.02220 0.01551 -0.0760 0.3004 0.8680
9.750 1.3120 0.02347 0.01676 -0.0726 0.2802 0.8882
10.000 1.3073 0.02482 0.01810 -0.0690 0.2609 0.9232
10.250 1.3039 0.02645 0.01968 -0.0664 0.2412 1.0000
10.500 1.3048 0.02839 0.02155 -0.0648 0.2208 1.0000
10.750 1.3048 0.03049 0.02357 -0.0633 0.2015 1.0000
11.000 1.3049 0.03267 0.02568 -0.0620 0.1842 1.0000
11.250 1.3048 0.03496 0.02791 -0.0608 0.1679 1.0000
11.500 1.3051 0.03728 0.03019 -0.0598 0.1533 1.0000
11.750 1.3059 0.03966 0.03253 -0.0590 0.1399 1.0000
12.000 1.3070 0.04209 0.03495 -0.0583 0.1277 1.0000
12.250 1.3080 0.04462 0.03746 -0.0577 0.1162 1.0000
12.500 1.3090 0.04724 0.04006 -0.0572 0.1059 1.0000
12.750 1.3097 0.04997 0.04277 -0.0568 0.0961 1.0000
13.000 1.3117 0.05263 0.04543 -0.0566 0.0872 1.0000
13.250 1.3136 0.05539 0.04820 -0.0565 0.0793 1.0000
13.500 1.3151 0.05825 0.05108 -0.0564 0.0729 1.0000
13.750 1.3165 0.06119 0.05404 -0.0565 0.0674 1.0000
14.000 1.3192 0.06405 0.05695 -0.0566 0.0626 1.0000
14.500 1.3229 0.07014 0.06312 -0.0572 0.0550 1.0000
14.750 1.3233 0.07345 0.06646 -0.0577 0.0520 1.0000
15.000 1.3260 0.07652 0.06961 -0.0581 0.0492 1.0000
15.250 1.3277 0.07977 0.07292 -0.0587 0.0467 1.0000
15.500 1.3278 0.08330 0.07648 -0.0594 0.0447 1.0000
15.750 1.3315 0.08638 0.07966 -0.0601 0.0425 1.0000
16.000 1.3327 0.08984 0.08317 -0.0610 0.0407 1.0000
16.250 1.3320 0.09361 0.08697 -0.0620 0.0393 1.0000
16.500 1.3353 0.09685 0.09034 -0.0628 0.0378 1.0000
16.750 1.3374 0.10029 0.09386 -0.0639 0.0365 1.0000
17.000 1.3384 0.10392 0.09757 -0.0650 0.0354 1.0000
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