NACA 63(3)-018 (naca633018-il) Xfoil prediction polar at RE=50,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 63(3)-018 (naca633018-il) Reynolds number: 50,000 Max Cl/Cd: 20.59 at α=8° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-naca633018-il-50000-n5.txt Download as CSV file: xf-naca633018-il-50000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NACA 63(3)-018
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.050 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-15.500 -0.7527 0.12085 0.11321 -0.0104 1.0000 0.0938
-15.250 -0.8297 0.10138 0.09349 -0.0218 1.0000 0.0934
-15.000 -0.8726 0.09076 0.08259 -0.0274 1.0000 0.0937
-14.750 -0.9007 0.08330 0.07486 -0.0308 1.0000 0.0943
-14.500 -0.9214 0.07735 0.06860 -0.0331 1.0000 0.0953
-14.250 -0.9192 0.07406 0.06517 -0.0338 1.0000 0.0974
-14.000 -0.9064 0.07207 0.06317 -0.0339 1.0000 0.1002
-13.750 -0.9018 0.06917 0.06013 -0.0343 1.0000 0.1027
-13.500 -0.8979 0.06615 0.05690 -0.0348 1.0000 0.1054
-13.250 -0.8917 0.06332 0.05379 -0.0350 1.0000 0.1081
-13.000 -0.8747 0.06168 0.05212 -0.0348 1.0000 0.1118
-12.750 -0.8598 0.06010 0.05053 -0.0346 1.0000 0.1163
-12.500 -0.8484 0.05807 0.04830 -0.0345 1.0000 0.1211
-12.250 -0.8322 0.05656 0.04677 -0.0341 1.0000 0.1261
-12.000 -0.8172 0.05511 0.04533 -0.0337 1.0000 0.1318
-11.750 -0.8053 0.05334 0.04348 -0.0335 1.0000 0.1391
-11.500 -0.7943 0.05172 0.04195 -0.0331 1.0000 0.1470
-11.250 -0.7846 0.04996 0.04022 -0.0327 1.0000 0.1564
-11.000 -0.7762 0.04812 0.03841 -0.0323 1.0000 0.1679
-10.750 -0.7701 0.04625 0.03668 -0.0319 1.0000 0.1808
-10.500 -0.7657 0.04430 0.03488 -0.0313 1.0000 0.1966
-10.250 -0.7624 0.04238 0.03317 -0.0307 1.0000 0.2155
-10.000 -0.7591 0.04063 0.03166 -0.0298 1.0000 0.2382
-9.750 -0.7544 0.03915 0.03043 -0.0288 1.0000 0.2653
-9.500 -0.7462 0.03816 0.02967 -0.0276 1.0000 0.2956
-9.250 -0.7345 0.03764 0.02934 -0.0263 1.0000 0.3263
-9.000 -0.7254 0.03699 0.02875 -0.0251 1.0000 0.3544
-8.750 -0.7078 0.03731 0.02914 -0.0236 1.0000 0.3797
-8.500 -0.7114 0.03615 0.02797 -0.0217 1.0000 0.4016
-8.250 -0.7049 0.03635 0.02819 -0.0191 1.0000 0.4201
-8.000 -0.7332 0.03565 0.02755 -0.0130 1.0000 0.4319
-7.750 -0.7096 0.03627 0.02809 -0.0127 0.9839 0.4521
-7.500 -0.6623 0.03764 0.02929 -0.0146 0.9727 0.4705
-7.250 -0.6200 0.03838 0.02983 -0.0165 0.9614 0.4861
-7.000 -0.5826 0.03858 0.02984 -0.0184 0.9500 0.5006
-6.750 -0.5514 0.03839 0.02945 -0.0200 0.9383 0.5149
-6.500 -0.4989 0.03978 0.03067 -0.0215 0.9296 0.5216
-6.250 -0.4754 0.03935 0.03008 -0.0219 0.9171 0.5335
-6.000 -0.4637 0.03845 0.02903 -0.0214 0.9040 0.5466
-5.750 -0.4192 0.03924 0.02968 -0.0223 0.8953 0.5512
-5.500 -0.4149 0.03823 0.02854 -0.0207 0.8823 0.5634
-5.250 -0.3758 0.03869 0.02886 -0.0213 0.8744 0.5680
-5.000 -0.3748 0.03765 0.02771 -0.0191 0.8624 0.5797
-4.750 -0.3414 0.03798 0.02794 -0.0192 0.8537 0.5840
-4.500 -0.3396 0.03692 0.02677 -0.0170 0.8438 0.5955
-4.250 -0.3086 0.03721 0.02698 -0.0169 0.8349 0.5995
-4.000 -0.2898 0.03684 0.02650 -0.0159 0.8273 0.6071
-3.750 -0.2774 0.03642 0.02602 -0.0144 0.8173 0.6147
-3.500 -0.2513 0.03631 0.02580 -0.0139 0.8108 0.6202
-3.250 -0.2471 0.03565 0.02509 -0.0118 0.8008 0.6296
-2.750 -0.2175 0.03492 0.02421 -0.0092 0.7850 0.6444
-2.500 -0.1866 0.03499 0.02422 -0.0093 0.7792 0.6480
-2.250 -0.1660 0.03493 0.02414 -0.0086 0.7714 0.6537
-2.000 -0.1551 0.03440 0.02354 -0.0070 0.7642 0.6622
-1.750 -0.1291 0.03445 0.02356 -0.0066 0.7578 0.6666
-1.500 -0.1146 0.03424 0.02331 -0.0054 0.7501 0.6739
-1.250 -0.0934 0.03396 0.02297 -0.0046 0.7449 0.6801
-1.000 -0.0745 0.03410 0.02313 -0.0038 0.7367 0.6854
-0.750 -0.0622 0.03367 0.02264 -0.0023 0.7305 0.6942
-0.500 -0.0361 0.03381 0.02278 -0.0020 0.7248 0.6984
-0.250 -0.0190 0.03388 0.02286 -0.0009 0.7171 0.7046
0.000 0.0000 0.03359 0.02252 0.0000 0.7121 0.7121
0.250 0.0190 0.03388 0.02286 0.0009 0.7046 0.7171
0.500 0.0361 0.03381 0.02278 0.0020 0.6984 0.7247
0.750 0.0622 0.03367 0.02263 0.0023 0.6942 0.7305
1.000 0.0744 0.03410 0.02313 0.0038 0.6854 0.7368
1.250 0.0933 0.03397 0.02298 0.0046 0.6802 0.7449
1.500 0.1147 0.03424 0.02331 0.0054 0.6739 0.7501
1.750 0.1290 0.03445 0.02355 0.0066 0.6666 0.7579
2.000 0.1551 0.03441 0.02354 0.0070 0.6623 0.7642
2.250 0.1660 0.03493 0.02414 0.0086 0.6537 0.7714
2.500 0.1865 0.03499 0.02423 0.0093 0.6481 0.7792
2.750 0.2174 0.03492 0.02422 0.0092 0.6444 0.7850
3.000 0.2181 0.03564 0.02500 0.0116 0.6340 0.7948
3.250 0.2471 0.03565 0.02509 0.0118 0.6296 0.8008
3.500 0.2514 0.03630 0.02580 0.0139 0.6202 0.8108
3.750 0.2774 0.03642 0.02601 0.0144 0.6147 0.8173
4.000 0.2899 0.03683 0.02649 0.0158 0.6072 0.8273
4.250 0.3086 0.03721 0.02698 0.0169 0.5996 0.8349
4.500 0.3396 0.03693 0.02677 0.0170 0.5956 0.8438
4.750 0.3413 0.03798 0.02794 0.0192 0.5841 0.8537
5.000 0.3749 0.03765 0.02771 0.0191 0.5797 0.8624
5.250 0.3758 0.03869 0.02886 0.0213 0.5680 0.8745
5.500 0.4151 0.03822 0.02853 0.0207 0.5634 0.8823
5.750 0.4194 0.03924 0.02967 0.0223 0.5512 0.8954
6.000 0.4637 0.03845 0.02902 0.0213 0.5466 0.9041
6.250 0.4758 0.03932 0.03005 0.0219 0.5335 0.9171
6.500 0.4994 0.03976 0.03065 0.0214 0.5216 0.9296
6.750 0.5516 0.03839 0.02945 0.0199 0.5149 0.9384
7.000 0.5827 0.03859 0.02985 0.0184 0.5006 0.9501
7.250 0.6205 0.03835 0.02980 0.0165 0.4861 0.9615
7.500 0.6628 0.03763 0.02928 0.0145 0.4705 0.9728
7.750 0.7102 0.03624 0.02806 0.0126 0.4521 0.9840
8.000 0.7336 0.03563 0.02753 0.0129 0.4320 1.0000
8.250 0.7058 0.03629 0.02813 0.0191 0.4200 1.0000
8.500 0.7120 0.03613 0.02795 0.0217 0.4016 1.0000
8.750 0.7081 0.03730 0.02913 0.0236 0.3796 1.0000
9.000 0.7258 0.03698 0.02873 0.0250 0.3544 1.0000
9.250 0.7351 0.03760 0.02929 0.0263 0.3260 1.0000
9.500 0.7469 0.03813 0.02963 0.0275 0.2956 1.0000
9.750 0.7550 0.03912 0.03041 0.0287 0.2653 1.0000
10.000 0.7596 0.04061 0.03165 0.0298 0.2380 1.0000
10.250 0.7630 0.04236 0.03315 0.0306 0.2154 1.0000
10.500 0.7663 0.04428 0.03486 0.0312 0.1965 1.0000
10.750 0.7708 0.04623 0.03666 0.0318 0.1806 1.0000
11.000 0.7770 0.04809 0.03837 0.0323 0.1679 1.0000
11.250 0.7853 0.04994 0.04019 0.0326 0.1563 1.0000
11.500 0.7953 0.05168 0.04192 0.0330 0.1470 1.0000
11.750 0.8061 0.05331 0.04344 0.0334 0.1390 1.0000
12.000 0.8180 0.05508 0.04530 0.0336 0.1318 1.0000
12.250 0.8333 0.05652 0.04673 0.0340 0.1261 1.0000
12.500 0.8494 0.05803 0.04826 0.0344 0.1211 1.0000
12.750 0.8604 0.06009 0.05051 0.0344 0.1161 1.0000
13.000 0.8759 0.06163 0.05206 0.0347 0.1118 1.0000
13.250 0.8925 0.06331 0.05379 0.0349 0.1080 1.0000
13.500 0.8988 0.06613 0.05688 0.0347 0.1053 1.0000
13.750 0.9031 0.06913 0.06009 0.0342 0.1027 1.0000
14.000 0.9079 0.07199 0.06309 0.0338 0.1001 1.0000
14.250 0.9220 0.07385 0.06494 0.0338 0.0972 1.0000
14.500 0.9228 0.07731 0.06855 0.0330 0.0953 1.0000
14.750 0.9016 0.08330 0.07487 0.0307 0.0943 1.0000
15.000 0.8735 0.09076 0.08259 0.0273 0.0936 1.0000
15.250 0.8307 0.10138 0.09349 0.0216 0.0934 1.0000
15.500 0.7534 0.12092 0.11328 0.0102 0.0938 1.0000
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