NACA 63(3)-618 (naca633618-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 63(3)-618 (naca633618-il) Reynolds number: 500,000 Max Cl/Cd: 102.82 at α=6.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-naca633618-il-500000-n5.txt Download as CSV file: xf-naca633618-il-500000-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 = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -0.7984 0.12008 0.11659 -0.0532 1.0000 0.0156
-19.500 -0.8188 0.11255 0.10894 -0.0573 1.0000 0.0158
-19.250 -0.8369 0.10558 0.10185 -0.0611 1.0000 0.0159
-19.000 -0.8529 0.09914 0.09530 -0.0645 1.0000 0.0161
-18.750 -0.8673 0.09309 0.08914 -0.0678 1.0000 0.0162
-18.500 -0.8805 0.08737 0.08330 -0.0708 1.0000 0.0163
-18.250 -0.8905 0.08230 0.07813 -0.0734 1.0000 0.0165
-18.000 -0.8992 0.07750 0.07321 -0.0759 1.0000 0.0166
-17.750 -0.9078 0.07284 0.06847 -0.0783 1.0000 0.0168
-17.500 -0.9153 0.06847 0.06403 -0.0805 1.0000 0.0171
-17.250 -0.9198 0.06461 0.06009 -0.0823 1.0000 0.0173
-17.000 -0.9227 0.06108 0.05649 -0.0839 1.0000 0.0175
-16.750 -0.9246 0.05780 0.05314 -0.0853 1.0000 0.0179
-16.500 -0.9252 0.05476 0.05002 -0.0865 1.0000 0.0181
-16.250 -0.9245 0.05197 0.04716 -0.0875 1.0000 0.0185
-16.000 -0.9235 0.04933 0.04444 -0.0884 1.0000 0.0189
-15.750 -0.9212 0.04690 0.04193 -0.0890 1.0000 0.0193
-15.500 -0.9181 0.04467 0.03964 -0.0895 1.0000 0.0197
-15.250 -0.9160 0.04244 0.03737 -0.0898 1.0000 0.0201
-15.000 -0.9132 0.04039 0.03527 -0.0900 1.0000 0.0204
-14.750 -0.9083 0.03864 0.03348 -0.0899 1.0000 0.0211
-14.500 -0.9033 0.03697 0.03177 -0.0897 1.0000 0.0216
-14.250 -0.8990 0.03537 0.03011 -0.0893 1.0000 0.0222
-14.000 -0.8820 0.03366 0.02833 -0.0907 0.9845 0.0230
-13.750 -0.8554 0.03180 0.02643 -0.0947 0.9665 0.0237
-13.500 -0.8186 0.03019 0.02475 -0.1000 0.9535 0.0248
-13.250 -0.7780 0.02868 0.02312 -0.1058 0.9399 0.0261
-12.750 -0.7112 0.02596 0.02018 -0.1142 0.9034 0.0281
-12.500 -0.6933 0.02502 0.01911 -0.1147 0.8844 0.0291
-12.250 -0.6791 0.02416 0.01813 -0.1144 0.8687 0.0300
-12.000 -0.6660 0.02334 0.01718 -0.1137 0.8550 0.0307
-11.750 -0.6566 0.02233 0.01611 -0.1128 0.8428 0.0314
-11.250 -0.6333 0.02070 0.01433 -0.1108 0.8216 0.0330
-11.000 -0.6204 0.02000 0.01354 -0.1097 0.8125 0.0339
-10.750 -0.6077 0.01930 0.01277 -0.1086 0.8038 0.0347
-10.500 -0.5955 0.01866 0.01204 -0.1073 0.7953 0.0355
-10.250 -0.5883 0.01794 0.01127 -0.1053 0.7874 0.0363
-10.000 -0.5762 0.01734 0.01062 -0.1040 0.7796 0.0372
-9.750 -0.5590 0.01684 0.01005 -0.1033 0.7727 0.0382
-9.500 -0.5393 0.01641 0.00956 -0.1027 0.7658 0.0395
-9.250 -0.5184 0.01603 0.00909 -0.1021 0.7592 0.0405
-9.000 -0.4983 0.01554 0.00858 -0.1016 0.7534 0.0419
-8.750 -0.4759 0.01515 0.00816 -0.1013 0.7470 0.0435
-8.500 -0.4526 0.01481 0.00775 -0.1009 0.7406 0.0451
-8.250 -0.4287 0.01447 0.00736 -0.1007 0.7350 0.0467
-8.000 -0.4047 0.01409 0.00696 -0.1006 0.7291 0.0486
-7.750 -0.3798 0.01377 0.00660 -0.1005 0.7232 0.0507
-7.500 -0.3543 0.01350 0.00626 -0.1004 0.7177 0.0529
-7.250 -0.3286 0.01316 0.00592 -0.1005 0.7119 0.0562
-7.000 -0.3024 0.01289 0.00562 -0.1005 0.7061 0.0603
-6.750 -0.2762 0.01260 0.00531 -0.1006 0.7010 0.0660
-6.500 -0.2493 0.01229 0.00502 -0.1008 0.6956 0.0734
-6.250 -0.2223 0.01200 0.00474 -0.1010 0.6898 0.0838
-6.000 -0.1953 0.01172 0.00447 -0.1012 0.6845 0.0979
-5.750 -0.1679 0.01138 0.00421 -0.1016 0.6797 0.1179
-5.500 -0.1401 0.01106 0.00396 -0.1020 0.6743 0.1415
-5.250 -0.1123 0.01073 0.00371 -0.1024 0.6689 0.1677
-5.000 -0.0843 0.01039 0.00345 -0.1029 0.6638 0.2010
-4.750 -0.0557 0.00998 0.00321 -0.1036 0.6589 0.2457
-4.500 -0.0269 0.00958 0.00298 -0.1042 0.6538 0.2953
-4.250 0.0021 0.00927 0.00280 -0.1049 0.6488 0.3440
-4.000 0.0315 0.00908 0.00270 -0.1054 0.6440 0.3801
-3.750 0.0611 0.00895 0.00263 -0.1060 0.6388 0.4104
-3.500 0.0906 0.00885 0.00260 -0.1064 0.6339 0.4389
-3.250 0.1199 0.00883 0.00257 -0.1068 0.6294 0.4582
-3.000 0.1496 0.00880 0.00254 -0.1072 0.6250 0.4707
-2.750 0.1791 0.00879 0.00252 -0.1075 0.6199 0.4805
-2.500 0.2084 0.00880 0.00250 -0.1078 0.6148 0.4894
-2.250 0.2377 0.00882 0.00249 -0.1081 0.6104 0.5004
-2.000 0.2673 0.00882 0.00250 -0.1085 0.6062 0.5084
-1.750 0.2967 0.00883 0.00249 -0.1088 0.6016 0.5147
-1.500 0.3260 0.00886 0.00248 -0.1091 0.5971 0.5204
-1.250 0.3550 0.00889 0.00249 -0.1094 0.5927 0.5255
-1.000 0.3845 0.00890 0.00251 -0.1097 0.5882 0.5312
-0.750 0.4138 0.00893 0.00252 -0.1101 0.5835 0.5369
-0.500 0.4429 0.00898 0.00254 -0.1103 0.5793 0.5420
-0.250 0.4718 0.00902 0.00257 -0.1106 0.5754 0.5468
0.000 0.5012 0.00905 0.00261 -0.1109 0.5714 0.5518
0.250 0.5304 0.00909 0.00264 -0.1112 0.5669 0.5568
0.500 0.5592 0.00915 0.00268 -0.1115 0.5623 0.5610
0.750 0.5878 0.00921 0.00274 -0.1117 0.5582 0.5653
1.000 0.6170 0.00925 0.00280 -0.1120 0.5545 0.5702
1.250 0.6460 0.00930 0.00286 -0.1123 0.5502 0.5753
1.500 0.6747 0.00937 0.00293 -0.1125 0.5457 0.5798
1.750 0.7030 0.00945 0.00301 -0.1126 0.5414 0.5843
2.000 0.7318 0.00951 0.00309 -0.1129 0.5374 0.5891
2.250 0.7604 0.00958 0.00318 -0.1131 0.5327 0.5939
2.500 0.7887 0.00966 0.00326 -0.1133 0.5278 0.5985
2.750 0.8165 0.00977 0.00337 -0.1134 0.5233 0.6036
3.000 0.8451 0.00983 0.00348 -0.1136 0.5190 0.6092
3.250 0.8734 0.00992 0.00359 -0.1138 0.5143 0.6143
3.500 0.9011 0.01002 0.00371 -0.1138 0.5095 0.6189
3.750 0.9286 0.01014 0.00384 -0.1139 0.5051 0.6240
4.000 0.9567 0.01022 0.00398 -0.1140 0.5004 0.6294
4.250 0.9843 0.01033 0.00411 -0.1141 0.4950 0.6349
4.500 1.0109 0.01047 0.00427 -0.1140 0.4893 0.6403
4.750 1.0382 0.01057 0.00443 -0.1140 0.4825 0.6462
5.000 1.0643 0.01072 0.00458 -0.1138 0.4743 0.6518
5.250 1.0906 0.01087 0.00475 -0.1136 0.4668 0.6570
5.500 1.1165 0.01101 0.00494 -0.1134 0.4589 0.6628
5.750 1.1418 0.01119 0.00513 -0.1131 0.4506 0.6692
6.000 1.1666 0.01139 0.00533 -0.1127 0.4405 0.6751
6.250 1.1907 0.01158 0.00556 -0.1122 0.4290 0.6808
6.500 1.2133 0.01185 0.00581 -0.1114 0.4150 0.6872
7.000 1.2518 0.01260 0.00645 -0.1088 0.3734 0.6997
7.250 1.2659 0.01315 0.00690 -0.1067 0.3442 0.7064
7.500 1.2754 0.01378 0.00740 -0.1038 0.3171 0.7126
7.750 1.2840 0.01440 0.00795 -0.1007 0.2943 0.7193
8.000 1.2908 0.01517 0.00864 -0.0976 0.2709 0.7268
8.250 1.2971 0.01601 0.00939 -0.0946 0.2471 0.7337
8.500 1.3022 0.01695 0.01026 -0.0915 0.2254 0.7410
8.750 1.3079 0.01795 0.01119 -0.0888 0.2055 0.7486
9.000 1.3134 0.01900 0.01222 -0.0862 0.1872 0.7563
9.250 1.3190 0.02015 0.01332 -0.0839 0.1706 0.7649
9.500 1.3243 0.02137 0.01452 -0.0816 0.1553 0.7731
9.750 1.3291 0.02270 0.01583 -0.0795 0.1404 0.7820
10.000 1.3341 0.02408 0.01720 -0.0775 0.1271 0.7907
10.250 1.3378 0.02563 0.01873 -0.0756 0.1133 0.8009
10.500 1.3414 0.02724 0.02033 -0.0738 0.1009 0.8113
10.750 1.3454 0.02890 0.02198 -0.0722 0.0901 0.8228
11.000 1.3491 0.03060 0.02370 -0.0706 0.0803 0.8351
11.250 1.3527 0.03234 0.02547 -0.0691 0.0719 0.8490
11.500 1.3558 0.03413 0.02731 -0.0676 0.0648 0.8664
11.750 1.3574 0.03593 0.02917 -0.0659 0.0583 0.8924
12.250 1.3655 0.03954 0.03289 -0.0637 0.0486 1.0000
12.500 1.3704 0.04169 0.03504 -0.0631 0.0445 1.0000
12.750 1.3768 0.04372 0.03711 -0.0627 0.0413 1.0000
13.000 1.3826 0.04588 0.03929 -0.0623 0.0387 1.0000
13.250 1.3890 0.04804 0.04149 -0.0620 0.0366 1.0000
13.500 1.3943 0.05034 0.04381 -0.0617 0.0346 1.0000
13.750 1.4007 0.05258 0.04611 -0.0616 0.0332 1.0000
14.000 1.4068 0.05489 0.04847 -0.0615 0.0319 1.0000
14.250 1.4123 0.05731 0.05094 -0.0615 0.0307 1.0000
14.500 1.4163 0.05997 0.05364 -0.0615 0.0297 1.0000
14.750 1.4224 0.06239 0.05613 -0.0617 0.0289 1.0000
15.000 1.4276 0.06499 0.05880 -0.0619 0.0279 1.0000
15.250 1.4324 0.06768 0.06154 -0.0621 0.0271 1.0000
15.500 1.4358 0.07058 0.06451 -0.0625 0.0263 1.0000
15.750 1.4381 0.07367 0.06764 -0.0629 0.0256 1.0000
16.000 1.4430 0.07647 0.07052 -0.0634 0.0249 1.0000
16.250 1.4469 0.07943 0.07356 -0.0639 0.0242 1.0000
16.500 1.4503 0.08248 0.07668 -0.0645 0.0235 1.0000
16.750 1.4524 0.08578 0.08004 -0.0653 0.0228 1.0000
17.000 1.4539 0.08919 0.08351 -0.0661 0.0221 1.0000
17.250 1.4554 0.09263 0.08702 -0.0670 0.0216 1.0000
17.500 1.4589 0.09581 0.09029 -0.0679 0.0209 1.0000
17.750 1.4607 0.09929 0.09386 -0.0689 0.0203 1.0000
18.000 1.4624 0.10280 0.09744 -0.0700 0.0197 1.0000
18.250 1.4626 0.10659 0.10130 -0.0713 0.0192 1.0000
18.500 1.4619 0.11053 0.10530 -0.0727 0.0187 1.0000
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