NACA 65(3)-618 (naca653618-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: NACA 65(3)-618 (naca653618-il) Reynolds number: 1,000,000 Max Cl/Cd: 138.34 at α=5.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-naca653618-il-1000000.txt Download as CSV file: xf-naca653618-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: NACA 65(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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.250 -0.7754 0.08819 0.08570 -0.0859 1.0000 0.0164
-18.000 -0.8085 0.07866 0.07598 -0.0916 1.0000 0.0165
-17.750 -0.8300 0.07174 0.06890 -0.0955 1.0000 0.0165
-17.500 -0.8435 0.06639 0.06343 -0.0984 1.0000 0.0167
-17.250 -0.8559 0.06156 0.05847 -0.1007 1.0000 0.0168
-17.000 -0.8645 0.05754 0.05434 -0.1024 1.0000 0.0169
-16.750 -0.8739 0.05369 0.05036 -0.1037 1.0000 0.0170
-16.500 -0.8767 0.05084 0.04743 -0.1044 1.0000 0.0172
-16.250 -0.8799 0.04818 0.04466 -0.1048 1.0000 0.0175
-16.000 -0.8848 0.04558 0.04197 -0.1047 1.0000 0.0176
-15.750 -0.8882 0.04349 0.03979 -0.1041 1.0000 0.0177
-15.250 -0.8658 0.03807 0.03410 -0.1094 0.9869 0.0181
-15.000 -0.8551 0.03541 0.03133 -0.1117 0.9790 0.0185
-14.750 -0.8331 0.03357 0.02943 -0.1148 0.9716 0.0188
-14.500 -0.8040 0.03209 0.02791 -0.1188 0.9646 0.0191
-14.250 -0.7704 0.03053 0.02628 -0.1237 0.9588 0.0195
-14.000 -0.7357 0.02892 0.02455 -0.1288 0.9512 0.0198
-13.750 -0.7006 0.02758 0.02308 -0.1336 0.9405 0.0204
-13.500 -0.6739 0.02638 0.02173 -0.1363 0.9250 0.0208
-13.250 -0.6566 0.02550 0.02070 -0.1367 0.9082 0.0211
-13.000 -0.6440 0.02478 0.01985 -0.1361 0.8933 0.0214
-12.750 -0.6325 0.02368 0.01859 -0.1349 0.8815 0.0217
-12.500 -0.6201 0.02273 0.01756 -0.1338 0.8706 0.0221
-12.250 -0.6067 0.02201 0.01680 -0.1327 0.8610 0.0225
-12.000 -0.5930 0.02140 0.01611 -0.1317 0.8518 0.0228
-11.750 -0.5786 0.02080 0.01547 -0.1306 0.8432 0.0231
-11.500 -0.5643 0.02028 0.01486 -0.1295 0.8348 0.0235
-11.250 -0.5491 0.01968 0.01420 -0.1285 0.8272 0.0239
-11.000 -0.5339 0.01919 0.01362 -0.1273 0.8193 0.0244
-10.750 -0.5177 0.01865 0.01302 -0.1263 0.8127 0.0248
-10.500 -0.5016 0.01811 0.01241 -0.1251 0.8059 0.0250
-10.250 -0.4852 0.01766 0.01188 -0.1240 0.7996 0.0253
-10.000 -0.4699 0.01697 0.01114 -0.1227 0.7934 0.0257
-9.750 -0.4580 0.01620 0.01033 -0.1209 0.7869 0.0263
-9.500 -0.4441 0.01567 0.00976 -0.1193 0.7810 0.0267
-9.250 -0.4296 0.01523 0.00930 -0.1177 0.7748 0.0272
-9.000 -0.4179 0.01487 0.00889 -0.1156 0.7686 0.0276
-8.750 -0.4027 0.01449 0.00846 -0.1140 0.7634 0.0281
-8.500 -0.3840 0.01412 0.00805 -0.1130 0.7580 0.0286
-8.250 -0.3650 0.01376 0.00764 -0.1120 0.7529 0.0290
-8.000 -0.3439 0.01348 0.00730 -0.1112 0.7481 0.0295
-7.750 -0.3211 0.01322 0.00701 -0.1107 0.7436 0.0299
-7.500 -0.3048 0.01257 0.00631 -0.1094 0.7385 0.0308
-7.250 -0.2837 0.01222 0.00591 -0.1087 0.7337 0.0315
-7.000 -0.2601 0.01192 0.00560 -0.1084 0.7295 0.0322
-6.750 -0.2360 0.01164 0.00530 -0.1081 0.7251 0.0330
-6.500 -0.2114 0.01140 0.00502 -0.1078 0.7209 0.0338
-6.250 -0.1864 0.01121 0.00477 -0.1077 0.7165 0.0346
-6.000 -0.1614 0.01090 0.00444 -0.1075 0.7131 0.0357
-5.750 -0.1360 0.01061 0.00415 -0.1075 0.7093 0.0374
-5.500 -0.1098 0.01041 0.00392 -0.1075 0.7054 0.0389
-5.250 -0.0833 0.01025 0.00372 -0.1075 0.7014 0.0405
-5.000 -0.0569 0.01002 0.00348 -0.1076 0.6977 0.0436
-4.750 -0.0296 0.00982 0.00329 -0.1078 0.6944 0.0474
-4.500 -0.0028 0.00954 0.00307 -0.1080 0.6909 0.0602
-4.250 0.0224 0.00898 0.00278 -0.1082 0.6875 0.1258
-4.000 0.0475 0.00825 0.00245 -0.1087 0.6839 0.2398
-3.750 0.0738 0.00727 0.00206 -0.1097 0.6809 0.4023
-3.500 0.1025 0.00680 0.00194 -0.1105 0.6780 0.5052
-3.250 0.1319 0.00673 0.00192 -0.1110 0.6749 0.5341
-3.000 0.1612 0.00672 0.00190 -0.1115 0.6716 0.5513
-2.750 0.1905 0.00675 0.00190 -0.1119 0.6684 0.5641
-2.500 0.2199 0.00678 0.00193 -0.1124 0.6653 0.5766
-2.250 0.2494 0.00679 0.00196 -0.1128 0.6630 0.5888
-2.000 0.2789 0.00683 0.00200 -0.1133 0.6603 0.6015
-1.750 0.3083 0.00690 0.00207 -0.1137 0.6576 0.6130
-1.500 0.3374 0.00693 0.00211 -0.1140 0.6547 0.6208
-1.250 0.3665 0.00698 0.00212 -0.1144 0.6518 0.6239
-1.000 0.3958 0.00704 0.00214 -0.1149 0.6487 0.6266
-0.750 0.4252 0.00704 0.00214 -0.1154 0.6467 0.6292
-0.500 0.4547 0.00706 0.00215 -0.1159 0.6443 0.6314
-0.250 0.4840 0.00708 0.00216 -0.1163 0.6418 0.6337
0.000 0.5130 0.00708 0.00216 -0.1167 0.6393 0.6368
0.250 0.5419 0.00711 0.00219 -0.1171 0.6366 0.6394
0.500 0.5710 0.00718 0.00224 -0.1176 0.6337 0.6418
0.750 0.6003 0.00723 0.00228 -0.1180 0.6316 0.6444
1.000 0.6294 0.00725 0.00232 -0.1185 0.6295 0.6471
1.250 0.6586 0.00729 0.00236 -0.1189 0.6272 0.6496
1.500 0.6875 0.00731 0.00240 -0.1193 0.6247 0.6522
1.750 0.7163 0.00733 0.00244 -0.1197 0.6223 0.6552
2.000 0.7450 0.00738 0.00250 -0.1201 0.6199 0.6580
2.250 0.7741 0.00748 0.00259 -0.1206 0.6170 0.6608
2.500 0.8029 0.00753 0.00267 -0.1210 0.6148 0.6638
2.750 0.8314 0.00756 0.00273 -0.1213 0.6123 0.6668
3.000 0.8596 0.00759 0.00278 -0.1216 0.6089 0.6695
3.250 0.8875 0.00761 0.00283 -0.1218 0.6051 0.6730
3.500 0.9155 0.00770 0.00292 -0.1220 0.6012 0.6762
3.750 0.9435 0.00775 0.00301 -0.1222 0.5978 0.6794
4.000 0.9709 0.00777 0.00307 -0.1224 0.5935 0.6826
4.250 0.9976 0.00782 0.00312 -0.1223 0.5873 0.6857
4.500 1.0238 0.00787 0.00320 -0.1222 0.5805 0.6896
4.750 1.0501 0.00790 0.00327 -0.1221 0.5734 0.6935
5.000 1.0751 0.00798 0.00336 -0.1217 0.5641 0.6973
5.250 1.1000 0.00808 0.00345 -0.1213 0.5539 0.7010
5.500 1.1253 0.00817 0.00356 -0.1210 0.5439 0.7044
5.750 1.1482 0.00830 0.00369 -0.1203 0.5300 0.7088
6.000 1.1701 0.00847 0.00385 -0.1193 0.5138 0.7130
6.250 1.1898 0.00872 0.00405 -0.1180 0.4931 0.7174
6.500 1.2028 0.00915 0.00434 -0.1154 0.4605 0.7218
6.750 1.2019 0.00981 0.00481 -0.1102 0.4141 0.7270
7.000 1.1968 0.01077 0.00552 -0.1044 0.3637 0.7323
7.250 1.1930 0.01178 0.00631 -0.0992 0.3185 0.7378
7.500 1.1893 0.01287 0.00720 -0.0943 0.2759 0.7432
7.750 1.1856 0.01404 0.00820 -0.0897 0.2357 0.7490
8.000 1.1830 0.01530 0.00929 -0.0855 0.1998 0.7551
8.250 1.1808 0.01665 0.01048 -0.0817 0.1648 0.7611
8.500 1.1796 0.01804 0.01175 -0.0782 0.1340 0.7677
8.750 1.1783 0.01957 0.01313 -0.0749 0.1048 0.7745
9.000 1.1773 0.02115 0.01460 -0.0719 0.0787 0.7815
9.250 1.1786 0.02270 0.01605 -0.0693 0.0571 0.7890
9.500 1.1819 0.02420 0.01748 -0.0670 0.0414 0.7962
9.750 1.1899 0.02544 0.01873 -0.0653 0.0346 0.8040
10.000 1.1991 0.02666 0.01996 -0.0639 0.0308 0.8117
10.250 1.2099 0.02777 0.02112 -0.0626 0.0283 0.8202
10.500 1.2189 0.02908 0.02246 -0.0612 0.0262 0.8289
10.750 1.2312 0.03013 0.02359 -0.0602 0.0248 0.8385
11.000 1.2409 0.03141 0.02491 -0.0589 0.0234 0.8487
11.250 1.2491 0.03282 0.02638 -0.0576 0.0221 0.8604
11.500 1.2599 0.03401 0.02767 -0.0565 0.0213 0.8738
11.750 1.2703 0.03519 0.02893 -0.0554 0.0204 0.8897
12.000 1.2775 0.03657 0.03040 -0.0539 0.0197 0.9112
12.250 1.2819 0.03807 0.03203 -0.0522 0.0188 0.9558
12.500 1.2926 0.03958 0.03361 -0.0518 0.0183 1.0000
12.750 1.3053 0.04094 0.03500 -0.0514 0.0176 1.0000
13.000 1.3154 0.04255 0.03665 -0.0508 0.0171 1.0000
13.250 1.3261 0.04412 0.03825 -0.0504 0.0167 1.0000
13.500 1.3351 0.04586 0.04002 -0.0499 0.0162 1.0000
13.750 1.3393 0.04811 0.04231 -0.0492 0.0156 1.0000
14.000 1.3449 0.05028 0.04454 -0.0487 0.0153 1.0000
14.250 1.3547 0.05205 0.04636 -0.0484 0.0151 1.0000
14.500 1.3638 0.05392 0.04829 -0.0481 0.0148 1.0000
14.750 1.3715 0.05596 0.05039 -0.0479 0.0145 1.0000
15.000 1.3797 0.05796 0.05243 -0.0477 0.0142 1.0000
15.250 1.3869 0.06014 0.05466 -0.0476 0.0140 1.0000
15.500 1.3938 0.06235 0.05692 -0.0475 0.0137 1.0000
15.750 1.3993 0.06479 0.05942 -0.0474 0.0135 1.0000
16.000 1.4051 0.06720 0.06188 -0.0474 0.0133 1.0000
16.250 1.4080 0.07001 0.06474 -0.0475 0.0131 1.0000
16.500 1.4079 0.07321 0.06801 -0.0476 0.0128 1.0000
16.750 1.4058 0.07675 0.07163 -0.0478 0.0127 1.0000
17.000 1.4083 0.07977 0.07472 -0.0481 0.0125 1.0000
17.250 1.4132 0.08251 0.07754 -0.0485 0.0124 1.0000
17.500 1.4173 0.08539 0.08049 -0.0490 0.0123 1.0000
17.750 1.4205 0.08843 0.08360 -0.0496 0.0122 1.0000
18.000 1.4238 0.09148 0.08673 -0.0502 0.0121 1.0000
18.250 1.4264 0.09468 0.09001 -0.0510 0.0120 1.0000
18.500 1.4288 0.09794 0.09335 -0.0518 0.0119 1.0000
18.750 1.4316 0.10115 0.09664 -0.0528 0.0117 1.0000
19.000 1.4330 0.10460 0.10016 -0.0538 0.0116 1.0000
19.250 1.4348 0.10800 0.10364 -0.0549 0.0115 1.0000
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