NACA 63(3)-018 (naca633018-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: NACA 63(3)-018 (naca633018-il) Reynolds number: 500,000 Max Cl/Cd: 72.96 at α=6.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-naca633018-il-500000.txt Download as CSV file: xf-naca633018-il-500000.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 = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.1912 0.10230 0.09809 -0.0077 1.0000 0.0263
-19.500 -1.1928 0.09821 0.09394 -0.0099 1.0000 0.0271
-19.250 -1.1929 0.09439 0.09005 -0.0118 1.0000 0.0281
-19.000 -1.1924 0.09070 0.08626 -0.0137 1.0000 0.0290
-18.750 -1.1913 0.08711 0.08254 -0.0154 1.0000 0.0298
-18.500 -1.1914 0.08358 0.07892 -0.0169 1.0000 0.0307
-18.250 -1.1915 0.08018 0.07549 -0.0182 1.0000 0.0316
-18.000 -1.1894 0.07697 0.07224 -0.0196 1.0000 0.0324
-17.750 -1.1862 0.07397 0.06918 -0.0209 1.0000 0.0332
-17.500 -1.1821 0.07115 0.06629 -0.0220 1.0000 0.0341
-17.250 -1.1777 0.06840 0.06345 -0.0230 1.0000 0.0350
-17.000 -1.1726 0.06577 0.06071 -0.0240 1.0000 0.0357
-16.750 -1.1668 0.06323 0.05806 -0.0250 1.0000 0.0362
-16.500 -1.1644 0.06071 0.05555 -0.0252 1.0000 0.0375
-16.250 -1.1593 0.05833 0.05314 -0.0258 1.0000 0.0385
-16.000 -1.1530 0.05609 0.05085 -0.0264 1.0000 0.0392
-15.750 -1.1459 0.05397 0.04868 -0.0268 1.0000 0.0401
-15.500 -1.1382 0.05197 0.04662 -0.0272 1.0000 0.0409
-15.250 -1.1298 0.05003 0.04461 -0.0276 1.0000 0.0419
-15.000 -1.1209 0.04822 0.04272 -0.0278 1.0000 0.0426
-14.750 -1.1109 0.04648 0.04090 -0.0281 1.0000 0.0433
-14.500 -1.1058 0.04455 0.03894 -0.0276 1.0000 0.0444
-14.250 -1.1004 0.04259 0.03697 -0.0275 1.0000 0.0455
-14.000 -1.0923 0.04087 0.03522 -0.0274 1.0000 0.0464
-13.750 -1.0828 0.03929 0.03361 -0.0273 1.0000 0.0475
-13.500 -1.0727 0.03781 0.03209 -0.0272 1.0000 0.0488
-13.250 -1.0621 0.03640 0.03064 -0.0270 1.0000 0.0498
-13.000 -1.0496 0.03516 0.02932 -0.0269 1.0000 0.0510
-12.750 -1.0386 0.03383 0.02794 -0.0265 1.0000 0.0518
-12.500 -1.0359 0.03194 0.02604 -0.0257 1.0000 0.0534
-12.250 -1.0292 0.03034 0.02442 -0.0251 1.0000 0.0545
-12.000 -1.0193 0.02900 0.02308 -0.0246 1.0000 0.0561
-11.750 -1.0092 0.02770 0.02174 -0.0240 1.0000 0.0572
-11.500 -0.9983 0.02647 0.02048 -0.0234 1.0000 0.0584
-11.250 -0.9866 0.02530 0.01928 -0.0229 1.0000 0.0595
-11.000 -0.9732 0.02425 0.01818 -0.0225 1.0000 0.0606
-10.750 -0.9525 0.02267 0.01654 -0.0246 0.9474 0.0628
-10.250 -0.9321 0.02060 0.01425 -0.0225 0.8862 0.0673
-10.000 -0.9235 0.01979 0.01334 -0.0206 0.8699 0.0694
-9.750 -0.9131 0.01910 0.01252 -0.0188 0.8564 0.0714
-9.500 -0.9094 0.01811 0.01148 -0.0162 0.8439 0.0752
-9.250 -0.9026 0.01730 0.01064 -0.0139 0.8324 0.0796
-9.000 -0.8943 0.01665 0.00993 -0.0114 0.8227 0.0848
-8.750 -0.8904 0.01598 0.00926 -0.0080 0.8129 0.0935
-8.500 -0.8804 0.01532 0.00865 -0.0057 0.8043 0.1083
-8.250 -0.8695 0.01457 0.00800 -0.0035 0.7963 0.1316
-8.000 -0.8560 0.01382 0.00738 -0.0018 0.7886 0.1611
-7.750 -0.8410 0.01308 0.00679 -0.0002 0.7812 0.1956
-7.500 -0.8252 0.01232 0.00622 0.0012 0.7743 0.2362
-7.250 -0.8075 0.01159 0.00569 0.0024 0.7670 0.2802
-7.000 -0.7882 0.01099 0.00524 0.0034 0.7610 0.3243
-6.750 -0.7661 0.01050 0.00492 0.0040 0.7540 0.3631
-6.500 -0.7418 0.01020 0.00467 0.0044 0.7476 0.3928
-6.250 -0.7159 0.01001 0.00449 0.0046 0.7417 0.4154
-6.000 -0.6889 0.00985 0.00434 0.0046 0.7353 0.4325
-5.750 -0.6620 0.00973 0.00419 0.0047 0.7295 0.4462
-5.500 -0.6344 0.00963 0.00407 0.0047 0.7236 0.4580
-5.250 -0.6064 0.00954 0.00395 0.0046 0.7173 0.4690
-5.000 -0.5785 0.00950 0.00384 0.0045 0.7118 0.4794
-4.750 -0.5503 0.00942 0.00376 0.0044 0.7061 0.4883
-4.500 -0.5220 0.00938 0.00370 0.0043 0.7002 0.5005
-4.250 -0.4940 0.00940 0.00365 0.0042 0.6949 0.5123
-4.000 -0.4655 0.00933 0.00360 0.0041 0.6891 0.5202
-3.750 -0.4366 0.00930 0.00353 0.0039 0.6833 0.5273
-3.500 -0.4082 0.00928 0.00347 0.0038 0.6784 0.5348
-3.250 -0.3792 0.00928 0.00345 0.0035 0.6729 0.5425
-3.000 -0.3502 0.00923 0.00337 0.0033 0.6673 0.5483
-2.750 -0.3214 0.00920 0.00331 0.0031 0.6622 0.5532
-2.500 -0.2922 0.00919 0.00327 0.0028 0.6571 0.5587
-2.250 -0.2630 0.00915 0.00320 0.0025 0.6517 0.5639
-2.000 -0.2340 0.00911 0.00316 0.0023 0.6467 0.5688
-1.750 -0.2048 0.00912 0.00313 0.0020 0.6417 0.5739
-1.500 -0.1754 0.00911 0.00308 0.0017 0.6363 0.5789
-1.250 -0.1464 0.00905 0.00305 0.0015 0.6316 0.5834
-1.000 -0.1172 0.00907 0.00303 0.0012 0.6269 0.5882
-0.750 -0.0877 0.00905 0.00301 0.0009 0.6216 0.5933
-0.500 -0.0585 0.00901 0.00298 0.0006 0.6167 0.5978
-0.250 -0.0294 0.00903 0.00298 0.0003 0.6123 0.6023
0.000 0.0000 0.00903 0.00299 0.0000 0.6074 0.6074
0.250 0.0294 0.00903 0.00298 -0.0003 0.6023 0.6123
0.500 0.0585 0.00901 0.00298 -0.0006 0.5978 0.6167
0.750 0.0877 0.00905 0.00301 -0.0009 0.5933 0.6217
1.000 0.1172 0.00907 0.00303 -0.0012 0.5882 0.6269
1.250 0.1464 0.00905 0.00305 -0.0015 0.5834 0.6316
1.500 0.1754 0.00911 0.00308 -0.0017 0.5789 0.6363
1.750 0.2048 0.00912 0.00313 -0.0020 0.5740 0.6417
2.000 0.2340 0.00911 0.00316 -0.0023 0.5687 0.6467
2.250 0.2630 0.00915 0.00320 -0.0025 0.5639 0.6517
2.500 0.2922 0.00919 0.00327 -0.0028 0.5587 0.6571
2.750 0.3214 0.00920 0.00331 -0.0031 0.5532 0.6622
3.000 0.3502 0.00923 0.00337 -0.0033 0.5482 0.6673
3.250 0.3792 0.00928 0.00345 -0.0035 0.5425 0.6729
3.500 0.4082 0.00928 0.00347 -0.0038 0.5348 0.6784
3.750 0.4366 0.00930 0.00353 -0.0039 0.5273 0.6834
4.000 0.4655 0.00933 0.00360 -0.0041 0.5203 0.6891
4.250 0.4940 0.00940 0.00365 -0.0042 0.5123 0.6949
4.500 0.5220 0.00938 0.00370 -0.0043 0.5005 0.7002
4.750 0.5503 0.00942 0.00376 -0.0044 0.4882 0.7061
5.000 0.5785 0.00950 0.00384 -0.0045 0.4794 0.7118
5.250 0.6065 0.00954 0.00396 -0.0046 0.4692 0.7173
5.500 0.6344 0.00963 0.00407 -0.0047 0.4580 0.7236
5.750 0.6620 0.00973 0.00419 -0.0047 0.4462 0.7295
6.000 0.6890 0.00985 0.00434 -0.0046 0.4325 0.7353
6.250 0.7159 0.01001 0.00449 -0.0046 0.4155 0.7417
6.500 0.7418 0.01020 0.00467 -0.0044 0.3928 0.7476
6.750 0.7661 0.01050 0.00492 -0.0040 0.3629 0.7541
7.000 0.7882 0.01100 0.00524 -0.0034 0.3242 0.7610
7.250 0.8075 0.01160 0.00569 -0.0024 0.2800 0.7670
7.500 0.8252 0.01233 0.00622 -0.0012 0.2360 0.7743
7.750 0.8410 0.01309 0.00679 0.0002 0.1953 0.7812
8.000 0.8561 0.01382 0.00738 0.0017 0.1612 0.7886
8.250 0.8695 0.01457 0.00800 0.0035 0.1315 0.7963
8.500 0.8805 0.01532 0.00865 0.0057 0.1081 0.8042
8.750 0.8905 0.01598 0.00927 0.0080 0.0934 0.8130
9.000 0.8947 0.01664 0.00992 0.0113 0.0849 0.8227
9.250 0.9027 0.01730 0.01064 0.0138 0.0795 0.8324
9.500 0.9097 0.01811 0.01147 0.0162 0.0752 0.8438
9.750 0.9134 0.01909 0.01251 0.0187 0.0714 0.8564
10.000 0.9238 0.01979 0.01333 0.0205 0.0695 0.8697
10.250 0.9326 0.02058 0.01423 0.0224 0.0673 0.8861
10.500 0.9395 0.02147 0.01522 0.0244 0.0653 0.9086
10.750 0.9531 0.02263 0.01650 0.0245 0.0629 0.9471
11.000 0.9741 0.02421 0.01813 0.0224 0.0606 1.0000
11.250 0.9869 0.02530 0.01927 0.0228 0.0596 1.0000
11.500 0.9990 0.02644 0.02046 0.0234 0.0584 1.0000
11.750 1.0100 0.02767 0.02171 0.0239 0.0572 1.0000
12.000 1.0206 0.02893 0.02300 0.0244 0.0559 1.0000
12.250 1.0299 0.03031 0.02441 0.0250 0.0550 1.0000
12.500 1.0367 0.03190 0.02599 0.0256 0.0533 1.0000
12.750 1.0399 0.03376 0.02788 0.0264 0.0520 1.0000
13.000 1.0512 0.03507 0.02924 0.0267 0.0509 1.0000
13.250 1.0623 0.03642 0.03065 0.0270 0.0501 1.0000
13.500 1.0739 0.03774 0.03202 0.0271 0.0487 1.0000
13.750 1.0839 0.03923 0.03355 0.0272 0.0475 1.0000
14.000 1.0932 0.04083 0.03518 0.0273 0.0464 1.0000
14.250 1.1012 0.04255 0.03692 0.0274 0.0454 1.0000
14.500 1.1072 0.04446 0.03885 0.0275 0.0444 1.0000
14.750 1.1124 0.04641 0.04082 0.0279 0.0432 1.0000
15.000 1.1220 0.04813 0.04262 0.0277 0.0427 1.0000
15.250 1.1311 0.04994 0.04452 0.0274 0.0419 1.0000
15.500 1.1394 0.05188 0.04653 0.0271 0.0410 1.0000
15.750 1.1473 0.05388 0.04859 0.0267 0.0401 1.0000
16.000 1.1546 0.05600 0.05076 0.0262 0.0391 1.0000
16.250 1.1608 0.05826 0.05306 0.0256 0.0383 1.0000
16.500 1.1659 0.06062 0.05545 0.0251 0.0375 1.0000
16.750 1.1686 0.06310 0.05793 0.0248 0.0363 1.0000
17.000 1.1745 0.06567 0.06062 0.0238 0.0356 1.0000
17.250 1.1795 0.06826 0.06331 0.0230 0.0350 1.0000
17.500 1.1839 0.07103 0.06617 0.0219 0.0341 1.0000
17.750 1.1883 0.07385 0.06905 0.0207 0.0331 1.0000
18.000 1.1915 0.07685 0.07211 0.0194 0.0323 1.0000
18.250 1.1935 0.08004 0.07536 0.0181 0.0315 1.0000
18.500 1.1930 0.08346 0.07878 0.0168 0.0306 1.0000
18.750 1.1935 0.08694 0.08237 0.0152 0.0298 1.0000
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