NACA 64(3)-618 (naca643618-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 64(3)-618 (naca643618-il) Reynolds number: 1,000,000 Max Cl/Cd: 124.87 at α=5.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-naca643618-il-1000000-n5.txt Download as CSV file: xf-naca643618-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NACA 64(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 -1.0048 0.08347 0.08007 -0.0766 1.0000 0.0146
-19.500 -1.0176 0.07810 0.07460 -0.0795 1.0000 0.0146
-19.250 -1.0269 0.07327 0.06968 -0.0821 1.0000 0.0148
-19.000 -1.0348 0.06885 0.06516 -0.0843 1.0000 0.0149
-18.750 -1.0388 0.06507 0.06130 -0.0861 1.0000 0.0151
-18.500 -1.0417 0.06154 0.05769 -0.0878 1.0000 0.0152
-18.250 -1.0436 0.05822 0.05430 -0.0892 1.0000 0.0154
-18.000 -1.0455 0.05505 0.05104 -0.0905 1.0000 0.0155
-17.750 -1.0417 0.05260 0.04852 -0.0914 1.0000 0.0159
-17.500 -1.0418 0.04978 0.04563 -0.0924 1.0000 0.0159
-17.250 -1.0380 0.04748 0.04326 -0.0931 1.0000 0.0161
-17.000 -1.0339 0.04526 0.04097 -0.0936 1.0000 0.0162
-16.750 -1.0308 0.04304 0.03868 -0.0941 1.0000 0.0163
-16.500 -1.0293 0.04073 0.03632 -0.0944 1.0000 0.0166
-16.250 -1.0263 0.03869 0.03423 -0.0946 1.0000 0.0168
-16.000 -1.0210 0.03695 0.03246 -0.0946 1.0000 0.0170
-15.750 -1.0155 0.03533 0.03080 -0.0943 1.0000 0.0173
-15.500 -1.0077 0.03367 0.02911 -0.0942 0.9930 0.0175
-15.250 -0.9872 0.03204 0.02742 -0.0965 0.9789 0.0177
-15.000 -0.9557 0.03045 0.02576 -0.1008 0.9648 0.0181
-14.750 -0.9152 0.02885 0.02408 -0.1069 0.9549 0.0185
-14.500 -0.8687 0.02737 0.02250 -0.1138 0.9436 0.0190
-14.250 -0.8246 0.02605 0.02105 -0.1200 0.9262 0.0193
-14.000 -0.8019 0.02479 0.01965 -0.1223 0.9004 0.0197
-13.750 -0.7897 0.02381 0.01857 -0.1219 0.8796 0.0200
-13.500 -0.7783 0.02294 0.01759 -0.1211 0.8640 0.0203
-13.250 -0.7661 0.02216 0.01673 -0.1202 0.8499 0.0207
-13.000 -0.7542 0.02136 0.01585 -0.1193 0.8371 0.0210
-12.750 -0.7415 0.02061 0.01503 -0.1184 0.8271 0.0214
-12.500 -0.7294 0.01987 0.01421 -0.1173 0.8161 0.0217
-12.250 -0.7161 0.01916 0.01343 -0.1163 0.8067 0.0220
-12.000 -0.7025 0.01854 0.01272 -0.1152 0.7972 0.0223
-11.750 -0.6877 0.01795 0.01207 -0.1143 0.7887 0.0226
-11.500 -0.6777 0.01719 0.01125 -0.1127 0.7784 0.0230
-11.250 -0.6652 0.01656 0.01057 -0.1114 0.7704 0.0234
-11.000 -0.6541 0.01598 0.00993 -0.1097 0.7613 0.0238
-10.750 -0.6446 0.01550 0.00940 -0.1076 0.7538 0.0241
-10.500 -0.6295 0.01505 0.00891 -0.1063 0.7465 0.0246
-10.250 -0.6110 0.01468 0.00846 -0.1055 0.7398 0.0251
-10.000 -0.5904 0.01433 0.00807 -0.1048 0.7335 0.0256
-9.750 -0.5691 0.01401 0.00769 -0.1042 0.7262 0.0260
-9.500 -0.5473 0.01368 0.00732 -0.1037 0.7198 0.0266
-9.250 -0.5248 0.01333 0.00694 -0.1033 0.7134 0.0273
-9.000 -0.5016 0.01304 0.00661 -0.1029 0.7070 0.0280
-8.750 -0.4773 0.01276 0.00630 -0.1027 0.7015 0.0288
-8.500 -0.4523 0.01251 0.00601 -0.1026 0.6957 0.0296
-8.250 -0.4271 0.01228 0.00574 -0.1024 0.6896 0.0303
-8.000 -0.4020 0.01201 0.00544 -0.1023 0.6842 0.0313
-7.750 -0.3760 0.01176 0.00517 -0.1023 0.6788 0.0324
-7.500 -0.3498 0.01154 0.00492 -0.1023 0.6729 0.0336
-7.250 -0.3234 0.01136 0.00469 -0.1023 0.6675 0.0347
-7.000 -0.2965 0.01113 0.00446 -0.1025 0.6625 0.0363
-6.750 -0.2695 0.01093 0.00424 -0.1026 0.6568 0.0384
-6.500 -0.2424 0.01077 0.00404 -0.1027 0.6511 0.0402
-6.250 -0.2149 0.01057 0.00384 -0.1029 0.6461 0.0431
-6.000 -0.1871 0.01040 0.00366 -0.1031 0.6404 0.0462
-5.750 -0.1596 0.01023 0.00348 -0.1033 0.6346 0.0508
-5.500 -0.1316 0.01006 0.00331 -0.1036 0.6300 0.0564
-5.250 -0.1034 0.00987 0.00314 -0.1039 0.6252 0.0644
-5.000 -0.0753 0.00969 0.00299 -0.1042 0.6202 0.0749
-4.750 -0.0473 0.00952 0.00284 -0.1045 0.6153 0.0878
-4.500 -0.0186 0.00930 0.00268 -0.1049 0.6112 0.1047
-4.250 0.0101 0.00908 0.00254 -0.1054 0.6067 0.1283
-4.000 0.0386 0.00881 0.00238 -0.1059 0.6020 0.1617
-3.500 0.0965 0.00807 0.00201 -0.1073 0.5939 0.2733
-3.250 0.1261 0.00764 0.00181 -0.1082 0.5898 0.3471
-3.000 0.1557 0.00730 0.00171 -0.1090 0.5855 0.4210
-2.750 0.1851 0.00724 0.00170 -0.1095 0.5813 0.4507
-2.500 0.2147 0.00721 0.00169 -0.1099 0.5779 0.4688
-2.250 0.2444 0.00719 0.00168 -0.1104 0.5744 0.4807
-2.000 0.2739 0.00718 0.00169 -0.1108 0.5706 0.4942
-1.750 0.3033 0.00720 0.00171 -0.1111 0.5666 0.5087
-1.250 0.3619 0.00724 0.00173 -0.1119 0.5595 0.5197
-1.000 0.3914 0.00726 0.00174 -0.1122 0.5561 0.5233
-0.750 0.4208 0.00729 0.00175 -0.1126 0.5528 0.5264
-0.500 0.4500 0.00731 0.00176 -0.1129 0.5495 0.5295
-0.250 0.4790 0.00736 0.00179 -0.1132 0.5462 0.5322
0.000 0.5082 0.00739 0.00182 -0.1136 0.5436 0.5352
0.250 0.5377 0.00741 0.00185 -0.1140 0.5411 0.5383
0.500 0.5670 0.00745 0.00188 -0.1143 0.5383 0.5410
0.750 0.5961 0.00749 0.00192 -0.1146 0.5355 0.5433
1.000 0.6251 0.00753 0.00196 -0.1150 0.5328 0.5464
1.250 0.6539 0.00758 0.00202 -0.1153 0.5300 0.5496
1.500 0.6826 0.00765 0.00208 -0.1155 0.5273 0.5529
1.750 0.7118 0.00768 0.00213 -0.1159 0.5252 0.5563
2.000 0.7409 0.00772 0.00219 -0.1162 0.5222 0.5595
2.500 0.7982 0.00784 0.00233 -0.1167 0.5153 0.5662
2.750 0.8263 0.00792 0.00241 -0.1169 0.5118 0.5701
3.000 0.8549 0.00798 0.00249 -0.1172 0.5088 0.5741
3.250 0.8837 0.00803 0.00258 -0.1175 0.5063 0.5779
3.500 0.9122 0.00809 0.00266 -0.1177 0.5034 0.5817
3.750 0.9403 0.00816 0.00276 -0.1179 0.4991 0.5864
4.000 0.9673 0.00828 0.00287 -0.1179 0.4926 0.5914
4.250 0.9955 0.00835 0.00297 -0.1181 0.4864 0.5960
4.750 1.0493 0.00858 0.00320 -0.1180 0.4691 0.6048
5.000 1.0754 0.00873 0.00334 -0.1178 0.4606 0.6099
5.250 1.1026 0.00883 0.00347 -0.1179 0.4531 0.6150
5.500 1.1274 0.00904 0.00363 -0.1175 0.4373 0.6194
5.750 1.1485 0.00940 0.00388 -0.1165 0.4030 0.6247
6.000 1.1603 0.01022 0.00440 -0.1139 0.3473 0.6302
6.250 1.1734 0.01094 0.00492 -0.1116 0.3047 0.6355
6.500 1.1865 0.01160 0.00541 -0.1093 0.2694 0.6404
6.750 1.1958 0.01223 0.00591 -0.1062 0.2379 0.6463
7.000 1.2039 0.01286 0.00643 -0.1030 0.2115 0.6524
7.500 1.2194 0.01428 0.00765 -0.0968 0.1633 0.6641
7.750 1.2247 0.01514 0.00840 -0.0936 0.1399 0.6708
8.250 1.2374 0.01694 0.01007 -0.0880 0.1022 0.6845
8.500 1.2447 0.01790 0.01097 -0.0855 0.0881 0.6920
8.750 1.2528 0.01887 0.01192 -0.0833 0.0760 0.6989
9.000 1.2613 0.01988 0.01291 -0.0813 0.0658 0.7067
9.250 1.2710 0.02089 0.01391 -0.0795 0.0586 0.7138
9.500 1.2805 0.02194 0.01497 -0.0779 0.0520 0.7209
9.750 1.2899 0.02305 0.01609 -0.0763 0.0462 0.7288
10.000 1.2999 0.02418 0.01723 -0.0748 0.0413 0.7358
10.250 1.3101 0.02532 0.01840 -0.0735 0.0375 0.7438
10.500 1.3196 0.02655 0.01967 -0.0722 0.0342 0.7515
10.750 1.3297 0.02778 0.02094 -0.0710 0.0314 0.7596
11.000 1.3395 0.02907 0.02226 -0.0699 0.0291 0.7682
11.250 1.3492 0.03039 0.02363 -0.0688 0.0274 0.7773
11.500 1.3587 0.03176 0.02505 -0.0678 0.0256 0.7874
11.750 1.3684 0.03315 0.02651 -0.0669 0.0243 0.7986
12.000 1.3773 0.03465 0.02806 -0.0660 0.0230 0.8094
12.250 1.3868 0.03611 0.02959 -0.0651 0.0219 0.8225
12.500 1.3958 0.03765 0.03120 -0.0643 0.0209 0.8369
12.750 1.4042 0.03923 0.03287 -0.0635 0.0198 0.8534
13.250 1.4175 0.04234 0.03622 -0.0613 0.0182 0.9217
13.750 1.4333 0.04590 0.03991 -0.0602 0.0165 1.0000
14.000 1.4414 0.04783 0.04188 -0.0599 0.0157 1.0000
14.250 1.4499 0.04974 0.04382 -0.0596 0.0150 1.0000
14.500 1.4573 0.05179 0.04591 -0.0594 0.0143 1.0000
14.750 1.4645 0.05390 0.04805 -0.0592 0.0137 1.0000
15.000 1.4718 0.05605 0.05024 -0.0591 0.0131 1.0000
15.250 1.4794 0.05818 0.05242 -0.0591 0.0126 1.0000
15.500 1.4858 0.06050 0.05478 -0.0591 0.0120 1.0000
15.750 1.4924 0.06280 0.05712 -0.0591 0.0117 1.0000
16.000 1.4974 0.06534 0.05971 -0.0592 0.0113 1.0000
16.250 1.5037 0.06775 0.06217 -0.0594 0.0110 1.0000
16.500 1.5092 0.07033 0.06480 -0.0596 0.0107 1.0000
16.750 1.5151 0.07284 0.06737 -0.0599 0.0104 1.0000
17.000 1.5193 0.07562 0.07021 -0.0603 0.0102 1.0000
17.250 1.5243 0.07832 0.07296 -0.0607 0.0100 1.0000
17.500 1.5279 0.08126 0.07596 -0.0612 0.0098 1.0000
17.750 1.5316 0.08420 0.07896 -0.0617 0.0096 1.0000
18.000 1.5341 0.08735 0.08217 -0.0624 0.0094 1.0000
18.250 1.5365 0.09053 0.08541 -0.0631 0.0093 1.0000
18.500 1.5374 0.09397 0.08891 -0.0640 0.0091 1.0000
18.750 1.5392 0.09731 0.09232 -0.0649 0.0090 1.0000
19.000 1.5411 0.10068 0.09577 -0.0658 0.0089 1.0000
19.250 1.5426 0.10412 0.09929 -0.0669 0.0088 1.0000
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