NACA 63(3)-618 (naca633618-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 63(3)-618 (naca633618-il) Reynolds number: 1,000,000 Max Cl/Cd: 122.1 at α=5.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-naca633618-il-1000000-n5.txt Download as CSV file: xf-naca633618-il-1000000-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 = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -0.9806 0.09141 0.08793 -0.0668 1.0000 0.0114
-19.500 -0.9955 0.08558 0.08198 -0.0699 1.0000 0.0115
-19.250 -1.0091 0.08004 0.07635 -0.0729 1.0000 0.0115
-19.000 -1.0212 0.07486 0.07106 -0.0756 1.0000 0.0116
-18.750 -1.0319 0.07002 0.06613 -0.0781 1.0000 0.0117
-18.500 -1.0410 0.06553 0.06156 -0.0803 1.0000 0.0119
-18.250 -1.0463 0.06167 0.05762 -0.0822 1.0000 0.0120
-18.000 -1.0504 0.05805 0.05392 -0.0838 1.0000 0.0122
-17.750 -1.0533 0.05468 0.05048 -0.0853 1.0000 0.0124
-17.500 -1.0549 0.05156 0.04730 -0.0865 1.0000 0.0127
-17.250 -1.0546 0.04873 0.04439 -0.0876 1.0000 0.0127
-17.000 -1.0529 0.04615 0.04176 -0.0885 1.0000 0.0130
-16.750 -1.0504 0.04374 0.03929 -0.0892 1.0000 0.0133
-16.500 -1.0471 0.04149 0.03698 -0.0897 1.0000 0.0135
-16.250 -1.0441 0.03930 0.03473 -0.0902 1.0000 0.0136
-16.000 -1.0392 0.03741 0.03278 -0.0904 1.0000 0.0139
-15.750 -1.0353 0.03549 0.03081 -0.0905 1.0000 0.0142
-15.500 -1.0313 0.03366 0.02895 -0.0904 1.0000 0.0145
-15.250 -1.0251 0.03188 0.02713 -0.0902 0.9897 0.0148
-15.000 -0.9962 0.03002 0.02521 -0.0946 0.9672 0.0154
-14.750 -0.9531 0.02826 0.02339 -0.1014 0.9539 0.0162
-14.500 -0.9044 0.02658 0.02163 -0.1092 0.9410 0.0171
-14.250 -0.8603 0.02513 0.02008 -0.1157 0.9185 0.0182
-14.000 -0.8409 0.02411 0.01890 -0.1168 0.8898 0.0190
-13.500 -0.8200 0.02222 0.01680 -0.1152 0.8534 0.0202
-13.250 -0.8086 0.02138 0.01590 -0.1143 0.8403 0.0214
-13.000 -0.7972 0.02056 0.01500 -0.1134 0.8288 0.0220
-12.750 -0.7845 0.01981 0.01418 -0.1125 0.8179 0.0228
-12.500 -0.7725 0.01905 0.01335 -0.1114 0.8084 0.0234
-12.250 -0.7599 0.01832 0.01258 -0.1104 0.7994 0.0242
-12.000 -0.7470 0.01766 0.01186 -0.1093 0.7913 0.0250
-11.750 -0.7340 0.01703 0.01117 -0.1080 0.7830 0.0257
-11.250 -0.7127 0.01593 0.00995 -0.1046 0.7679 0.0268
-11.000 -0.6980 0.01540 0.00938 -0.1035 0.7604 0.0277
-10.750 -0.6793 0.01497 0.00890 -0.1028 0.7539 0.0284
-10.500 -0.6582 0.01461 0.00851 -0.1023 0.7472 0.0294
-10.250 -0.6363 0.01429 0.00813 -0.1019 0.7408 0.0302
-10.000 -0.6133 0.01399 0.00777 -0.1015 0.7352 0.0308
-9.750 -0.5906 0.01361 0.00737 -0.1012 0.7292 0.0318
-9.500 -0.5669 0.01330 0.00702 -0.1009 0.7225 0.0327
-9.250 -0.5423 0.01302 0.00670 -0.1008 0.7170 0.0337
-9.000 -0.5169 0.01275 0.00640 -0.1007 0.7116 0.0347
-8.750 -0.4912 0.01252 0.00612 -0.1007 0.7055 0.0354
-8.500 -0.4658 0.01223 0.00580 -0.1006 0.7000 0.0366
-8.250 -0.4395 0.01196 0.00552 -0.1007 0.6945 0.0381
-8.000 -0.4128 0.01174 0.00527 -0.1007 0.6889 0.0397
-7.500 -0.3590 0.01128 0.00476 -0.1010 0.6784 0.0430
-7.250 -0.3315 0.01107 0.00453 -0.1012 0.6727 0.0448
-7.000 -0.3040 0.01089 0.00431 -0.1013 0.6673 0.0467
-6.750 -0.2763 0.01067 0.00409 -0.1016 0.6626 0.0499
-6.500 -0.2481 0.01048 0.00389 -0.1018 0.6575 0.0538
-6.250 -0.2201 0.01028 0.00369 -0.1021 0.6520 0.0594
-6.000 -0.1921 0.01008 0.00349 -0.1024 0.6466 0.0667
-5.750 -0.1635 0.00986 0.00330 -0.1028 0.6424 0.0762
-5.500 -0.1349 0.00965 0.00312 -0.1032 0.6372 0.0884
-5.250 -0.1064 0.00942 0.00294 -0.1036 0.6318 0.1047
-5.000 -0.0777 0.00919 0.00277 -0.1040 0.6271 0.1256
-4.750 -0.0485 0.00893 0.00259 -0.1046 0.6224 0.1493
-4.500 -0.0193 0.00871 0.00244 -0.1051 0.6177 0.1732
-4.250 0.0098 0.00846 0.00228 -0.1056 0.6128 0.2054
-4.000 0.0393 0.00817 0.00212 -0.1063 0.6085 0.2447
-3.750 0.0691 0.00789 0.00197 -0.1070 0.6037 0.2864
-3.500 0.0989 0.00763 0.00185 -0.1077 0.5985 0.3300
-3.000 0.1587 0.00728 0.00172 -0.1090 0.5902 0.4098
-2.750 0.1887 0.00721 0.00169 -0.1095 0.5860 0.4320
-2.500 0.2185 0.00717 0.00167 -0.1099 0.5813 0.4480
-2.250 0.2480 0.00717 0.00166 -0.1103 0.5765 0.4573
-2.000 0.2778 0.00717 0.00166 -0.1107 0.5724 0.4664
-1.750 0.3077 0.00715 0.00166 -0.1112 0.5681 0.4772
-1.500 0.3373 0.00718 0.00166 -0.1115 0.5638 0.4859
-1.250 0.3667 0.00719 0.00168 -0.1119 0.5596 0.4927
-1.000 0.3963 0.00721 0.00169 -0.1122 0.5560 0.4983
-0.750 0.4260 0.00723 0.00170 -0.1126 0.5521 0.5031
-0.500 0.4556 0.00725 0.00172 -0.1130 0.5475 0.5088
-0.250 0.4848 0.00729 0.00175 -0.1133 0.5430 0.5146
0.000 0.5141 0.00734 0.00178 -0.1136 0.5393 0.5200
0.250 0.5438 0.00736 0.00181 -0.1140 0.5358 0.5247
0.500 0.5732 0.00739 0.00185 -0.1144 0.5316 0.5297
0.750 0.6023 0.00744 0.00190 -0.1147 0.5271 0.5346
1.000 0.6312 0.00751 0.00194 -0.1149 0.5227 0.5388
1.250 0.6607 0.00754 0.00199 -0.1153 0.5190 0.5426
1.500 0.6898 0.00759 0.00205 -0.1156 0.5141 0.5471
1.750 0.7186 0.00766 0.00211 -0.1158 0.5090 0.5520
2.000 0.7473 0.00773 0.00218 -0.1160 0.5046 0.5567
2.250 0.7764 0.00778 0.00225 -0.1164 0.5004 0.5609
2.500 0.8053 0.00784 0.00232 -0.1166 0.4958 0.5656
2.750 0.8337 0.00793 0.00241 -0.1168 0.4910 0.5703
3.000 0.8622 0.00801 0.00249 -0.1170 0.4868 0.5747
3.250 0.8910 0.00807 0.00258 -0.1173 0.4823 0.5787
3.500 0.9193 0.00816 0.00268 -0.1175 0.4768 0.5839
3.750 0.9469 0.00827 0.00279 -0.1175 0.4707 0.5894
4.000 0.9752 0.00836 0.00289 -0.1177 0.4638 0.5944
4.250 1.0021 0.00852 0.00302 -0.1177 0.4548 0.5988
4.500 1.0301 0.00861 0.00314 -0.1178 0.4472 0.6039
4.750 1.0569 0.00876 0.00328 -0.1177 0.4391 0.6090
5.000 1.0841 0.00889 0.00342 -0.1177 0.4304 0.6139
5.250 1.1099 0.00909 0.00359 -0.1175 0.4188 0.6189
5.500 1.1350 0.00933 0.00379 -0.1172 0.4032 0.6248
5.750 1.1595 0.00959 0.00400 -0.1168 0.3866 0.6306
6.000 1.1830 0.00989 0.00424 -0.1162 0.3670 0.6353
6.250 1.2032 0.01037 0.00459 -0.1151 0.3376 0.6406
6.500 1.2194 0.01102 0.00506 -0.1133 0.2990 0.6466
6.750 1.2343 0.01171 0.00556 -0.1114 0.2637 0.6524
7.000 1.2500 0.01229 0.00603 -0.1096 0.2380 0.6580
7.250 1.2648 0.01283 0.00649 -0.1076 0.2155 0.6641
7.500 1.2745 0.01340 0.00697 -0.1046 0.1948 0.6701
7.750 1.2847 0.01401 0.00750 -0.1018 0.1764 0.6760
8.000 1.2937 0.01469 0.00812 -0.0990 0.1572 0.6827
8.250 1.3024 0.01542 0.00878 -0.0963 0.1404 0.6894
8.500 1.3098 0.01625 0.00954 -0.0936 0.1239 0.6952
8.750 1.3178 0.01710 0.01035 -0.0911 0.1101 0.7022
9.000 1.3264 0.01799 0.01121 -0.0888 0.0984 0.7093
9.250 1.3344 0.01897 0.01217 -0.0866 0.0871 0.7160
9.500 1.3429 0.01998 0.01317 -0.0846 0.0775 0.7233
9.750 1.3518 0.02103 0.01421 -0.0828 0.0693 0.7301
10.000 1.3604 0.02215 0.01534 -0.0811 0.0619 0.7374
10.250 1.3684 0.02337 0.01656 -0.0794 0.0548 0.7457
10.500 1.3770 0.02460 0.01780 -0.0779 0.0492 0.7531
10.750 1.3851 0.02591 0.01913 -0.0765 0.0443 0.7612
11.250 1.4022 0.02861 0.02189 -0.0739 0.0368 0.7779
11.500 1.4103 0.03006 0.02337 -0.0728 0.0341 0.7870
11.750 1.4193 0.03147 0.02484 -0.0718 0.0319 0.7974
12.000 1.4276 0.03297 0.02640 -0.0708 0.0304 0.8076
12.250 1.4364 0.03447 0.02796 -0.0699 0.0290 0.8191
12.500 1.4449 0.03603 0.02960 -0.0691 0.0278 0.8316
12.750 1.4526 0.03768 0.03132 -0.0682 0.0267 0.8463
13.000 1.4595 0.03940 0.03312 -0.0674 0.0256 0.8646
13.250 1.4662 0.04104 0.03488 -0.0664 0.0250 0.8938
13.500 1.4715 0.04257 0.03657 -0.0652 0.0243 1.0000
13.750 1.4790 0.04451 0.03856 -0.0648 0.0235 1.0000
14.000 1.4860 0.04655 0.04063 -0.0645 0.0227 1.0000
14.250 1.4924 0.04869 0.04281 -0.0642 0.0220 1.0000
14.500 1.5001 0.05075 0.04491 -0.0640 0.0215 1.0000
14.750 1.5078 0.05282 0.04703 -0.0639 0.0210 1.0000
15.000 1.5141 0.05509 0.04935 -0.0638 0.0203 1.0000
15.250 1.5205 0.05739 0.05169 -0.0638 0.0197 1.0000
15.500 1.5254 0.05992 0.05427 -0.0639 0.0191 1.0000
15.750 1.5308 0.06241 0.05680 -0.0640 0.0185 1.0000
16.000 1.5365 0.06492 0.05937 -0.0642 0.0181 1.0000
16.250 1.5424 0.06741 0.06192 -0.0644 0.0175 1.0000
16.500 1.5467 0.07018 0.06474 -0.0647 0.0169 1.0000
16.750 1.5509 0.07296 0.06757 -0.0651 0.0163 1.0000
17.000 1.5536 0.07600 0.07066 -0.0656 0.0157 1.0000
17.250 1.5581 0.07883 0.07354 -0.0661 0.0152 1.0000
17.500 1.5614 0.08186 0.07664 -0.0667 0.0146 1.0000
17.750 1.5644 0.08496 0.07980 -0.0674 0.0140 1.0000
18.000 1.5663 0.08827 0.08316 -0.0682 0.0135 1.0000
18.250 1.5679 0.09165 0.08659 -0.0691 0.0129 1.0000
18.500 1.5699 0.09498 0.08999 -0.0700 0.0124 1.0000
18.750 1.5709 0.09851 0.09358 -0.0710 0.0119 1.0000
19.000 1.5718 0.10205 0.09719 -0.0721 0.0114 1.0000
19.250 1.5713 0.10587 0.10107 -0.0734 0.0111 1.0000
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