NACA 63(3)-018 (naca633018-il) Xfoil prediction polar at RE=200,000 Ncrit=9
| Details | Polar file |
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Airfoil: NACA 63(3)-018 (naca633018-il) Reynolds number: 200,000 Max Cl/Cd: 53.25 at α=7.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-naca633018-il-200000.txt Download as CSV file: xf-naca633018-il-200000.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 = 0.200 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-17.750 -1.0786 0.09164 0.08685 -0.0227 1.0000 0.0476
-17.500 -1.0941 0.08604 0.08106 -0.0255 1.0000 0.0484
-17.250 -1.1099 0.08066 0.07546 -0.0279 1.0000 0.0492
-17.000 -1.1254 0.07570 0.07027 -0.0299 1.0000 0.0501
-16.750 -1.1405 0.07116 0.06548 -0.0316 1.0000 0.0509
-16.500 -1.1550 0.06715 0.06122 -0.0329 1.0000 0.0515
-16.250 -1.1434 0.06453 0.05861 -0.0329 1.0000 0.0534
-16.000 -1.1369 0.06256 0.05665 -0.0333 1.0000 0.0550
-15.750 -1.1360 0.06002 0.05401 -0.0337 1.0000 0.0562
-15.500 -1.1357 0.05754 0.05139 -0.0341 1.0000 0.0576
-15.250 -1.1379 0.05501 0.04870 -0.0343 1.0000 0.0590
-15.000 -1.1412 0.05256 0.04605 -0.0343 1.0000 0.0602
-14.500 -1.1195 0.04860 0.04200 -0.0340 1.0000 0.0640
-14.250 -1.1102 0.04702 0.04038 -0.0338 1.0000 0.0658
-14.000 -1.1028 0.04535 0.03860 -0.0335 1.0000 0.0676
-13.750 -1.0934 0.04373 0.03687 -0.0332 1.0000 0.0692
-13.500 -1.0843 0.04214 0.03512 -0.0327 1.0000 0.0706
-13.250 -1.0746 0.04067 0.03348 -0.0322 1.0000 0.0716
-13.000 -1.0427 0.03944 0.03233 -0.0320 1.0000 0.0744
-12.750 -1.0253 0.03832 0.03121 -0.0317 1.0000 0.0764
-12.500 -1.0088 0.03718 0.03004 -0.0313 1.0000 0.0783
-12.250 -0.9919 0.03607 0.02887 -0.0308 1.0000 0.0802
-12.000 -0.9764 0.03495 0.02765 -0.0303 1.0000 0.0821
-11.750 -0.9575 0.03393 0.02661 -0.0297 1.0000 0.0845
-11.500 -0.9406 0.03285 0.02561 -0.0291 1.0000 0.0874
-11.250 -0.9264 0.03172 0.02450 -0.0285 1.0000 0.0901
-11.000 -0.9121 0.03062 0.02337 -0.0280 1.0000 0.0932
-10.750 -0.8977 0.02954 0.02223 -0.0274 1.0000 0.0963
-10.500 -0.8890 0.02807 0.02090 -0.0266 1.0000 0.1007
-10.250 -0.8778 0.02681 0.01966 -0.0260 1.0000 0.1057
-10.000 -0.8681 0.02545 0.01832 -0.0255 1.0000 0.1119
-9.750 -0.8603 0.02400 0.01696 -0.0250 1.0000 0.1198
-9.500 -0.8550 0.02249 0.01556 -0.0244 1.0000 0.1304
-9.250 -0.8396 0.02071 0.01391 -0.0263 0.9681 0.1535
-9.000 -0.8302 0.01882 0.01224 -0.0269 0.9406 0.1898
-8.750 -0.8375 0.01779 0.01136 -0.0226 0.9178 0.2245
-8.500 -0.8422 0.01691 0.01066 -0.0181 0.9009 0.2656
-8.250 -0.8411 0.01615 0.01011 -0.0143 0.8877 0.3119
-8.000 -0.8328 0.01565 0.00976 -0.0114 0.8768 0.3560
-7.750 -0.8174 0.01535 0.00955 -0.0095 0.8663 0.3910
-7.500 -0.7995 0.01522 0.00937 -0.0078 0.8580 0.4176
-7.250 -0.7782 0.01514 0.00928 -0.0067 0.8486 0.4382
-7.000 -0.7565 0.01513 0.00921 -0.0055 0.8413 0.4562
-6.750 -0.7328 0.01513 0.00917 -0.0048 0.8327 0.4720
-6.500 -0.7097 0.01516 0.00909 -0.0037 0.8261 0.4855
-6.250 -0.6849 0.01517 0.00900 -0.0033 0.8176 0.4984
-6.000 -0.6597 0.01525 0.00904 -0.0025 0.8115 0.5092
-5.750 -0.6333 0.01535 0.00912 -0.0022 0.8037 0.5205
-5.500 -0.6083 0.01551 0.00922 -0.0014 0.7970 0.5336
-5.250 -0.5830 0.01571 0.00933 -0.0008 0.7904 0.5466
-5.000 -0.5545 0.01587 0.00955 -0.0006 0.7835 0.5545
-4.750 -0.5294 0.01584 0.00936 0.0000 0.7782 0.5634
-4.500 -0.5003 0.01599 0.00957 0.0000 0.7708 0.5703
-4.250 -0.4747 0.01598 0.00943 0.0004 0.7646 0.5796
-4.000 -0.4461 0.01610 0.00957 0.0007 0.7593 0.5854
-3.750 -0.4189 0.01606 0.00947 0.0006 0.7523 0.5925
-3.500 -0.3915 0.01598 0.00933 0.0008 0.7469 0.5979
-3.250 -0.3633 0.01602 0.00935 0.0008 0.7412 0.6030
-3.000 -0.3363 0.01593 0.00918 0.0008 0.7345 0.6098
-2.750 -0.3083 0.01586 0.00907 0.0009 0.7296 0.6145
-2.500 -0.2800 0.01590 0.00910 0.0009 0.7241 0.6194
-2.250 -0.2526 0.01581 0.00896 0.0007 0.7177 0.6257
-2.000 -0.2248 0.01572 0.00881 0.0008 0.7128 0.6304
-1.750 -0.1964 0.01575 0.00886 0.0007 0.7075 0.6348
-1.500 -0.1685 0.01572 0.00880 0.0005 0.7014 0.6405
-1.250 -0.1408 0.01561 0.00862 0.0005 0.6966 0.6459
-1.000 -0.1124 0.01564 0.00866 0.0005 0.6916 0.6499
-0.750 -0.0843 0.01564 0.00868 0.0003 0.6855 0.6552
-0.500 -0.0565 0.01556 0.00851 0.0001 0.6808 0.6614
-0.250 -0.0280 0.01557 0.00853 0.0002 0.6766 0.6652
0.000 0.0000 0.01561 0.00864 0.0000 0.6701 0.6701
0.250 0.0280 0.01557 0.00853 -0.0002 0.6652 0.6766
0.500 0.0565 0.01555 0.00851 -0.0001 0.6614 0.6808
0.750 0.0843 0.01564 0.00868 -0.0003 0.6552 0.6855
1.000 0.1124 0.01564 0.00866 -0.0005 0.6499 0.6917
1.250 0.1408 0.01561 0.00862 -0.0005 0.6459 0.6966
1.500 0.1685 0.01572 0.00880 -0.0005 0.6405 0.7014
1.750 0.1964 0.01575 0.00886 -0.0007 0.6348 0.7075
2.000 0.2248 0.01572 0.00882 -0.0008 0.6304 0.7128
2.250 0.2526 0.01581 0.00896 -0.0007 0.6256 0.7177
2.500 0.2800 0.01589 0.00910 -0.0009 0.6194 0.7241
2.750 0.3083 0.01586 0.00907 -0.0009 0.6145 0.7296
3.000 0.3363 0.01593 0.00918 -0.0008 0.6098 0.7345
3.250 0.3633 0.01601 0.00935 -0.0008 0.6030 0.7412
3.500 0.3915 0.01599 0.00933 -0.0008 0.5979 0.7469
3.750 0.4189 0.01606 0.00947 -0.0006 0.5925 0.7523
4.000 0.4461 0.01610 0.00957 -0.0007 0.5854 0.7593
4.250 0.4747 0.01598 0.00943 -0.0004 0.5796 0.7646
4.500 0.5003 0.01599 0.00957 0.0000 0.5703 0.7708
4.750 0.5294 0.01584 0.00936 0.0000 0.5634 0.7782
5.000 0.5545 0.01587 0.00955 0.0006 0.5546 0.7835
5.250 0.5831 0.01571 0.00933 0.0008 0.5467 0.7904
5.500 0.6083 0.01551 0.00922 0.0014 0.5336 0.7970
5.750 0.6333 0.01535 0.00912 0.0022 0.5204 0.8037
6.000 0.6598 0.01525 0.00904 0.0025 0.5091 0.8115
6.250 0.6849 0.01517 0.00900 0.0033 0.4984 0.8176
6.500 0.7097 0.01516 0.00909 0.0037 0.4855 0.8261
6.750 0.7329 0.01513 0.00917 0.0047 0.4719 0.8327
7.000 0.7566 0.01513 0.00922 0.0055 0.4563 0.8413
7.250 0.7783 0.01514 0.00928 0.0067 0.4383 0.8486
7.500 0.7995 0.01522 0.00937 0.0078 0.4176 0.8580
7.750 0.8174 0.01535 0.00955 0.0095 0.3909 0.8663
8.000 0.8329 0.01565 0.00975 0.0114 0.3560 0.8768
8.250 0.8412 0.01615 0.01011 0.0143 0.3119 0.8877
8.500 0.8423 0.01691 0.01066 0.0181 0.2656 0.9009
8.750 0.8375 0.01780 0.01136 0.0226 0.2241 0.9177
9.000 0.8305 0.01882 0.01223 0.0269 0.1900 0.9406
9.250 0.8398 0.02072 0.01392 0.0263 0.1533 0.9682
9.500 0.8554 0.02248 0.01555 0.0243 0.1305 1.0000
9.750 0.8608 0.02398 0.01694 0.0249 0.1199 1.0000
10.000 0.8685 0.02544 0.01831 0.0254 0.1118 1.0000
10.250 0.8784 0.02679 0.01964 0.0260 0.1057 1.0000
10.500 0.8896 0.02805 0.02088 0.0265 0.1005 1.0000
10.750 0.8983 0.02952 0.02222 0.0274 0.0963 1.0000
11.000 0.9128 0.03060 0.02335 0.0279 0.0932 1.0000
11.250 0.9271 0.03170 0.02448 0.0284 0.0901 1.0000
11.500 0.9414 0.03282 0.02559 0.0290 0.0874 1.0000
11.750 0.9582 0.03391 0.02659 0.0297 0.0845 1.0000
12.000 0.9773 0.03493 0.02762 0.0302 0.0822 1.0000
12.250 0.9926 0.03605 0.02884 0.0307 0.0802 1.0000
12.500 1.0095 0.03716 0.03001 0.0312 0.0783 1.0000
12.750 1.0259 0.03830 0.03119 0.0316 0.0763 1.0000
13.000 1.0432 0.03942 0.03230 0.0319 0.0743 1.0000
13.250 1.0756 0.04065 0.03347 0.0322 0.0716 1.0000
13.500 1.0846 0.04212 0.03510 0.0327 0.0706 1.0000
13.750 1.0941 0.04370 0.03684 0.0331 0.0692 1.0000
14.000 1.1035 0.04532 0.03858 0.0334 0.0676 1.0000
14.250 1.1111 0.04700 0.04035 0.0337 0.0657 1.0000
14.500 1.1200 0.04854 0.04192 0.0339 0.0639 1.0000
14.750 1.1456 0.05032 0.04360 0.0339 0.0610 1.0000
15.000 1.1414 0.05253 0.04602 0.0342 0.0602 1.0000
15.250 1.1385 0.05498 0.04867 0.0341 0.0590 1.0000
15.500 1.1370 0.05751 0.05136 0.0340 0.0576 1.0000
15.750 1.1372 0.05998 0.05396 0.0337 0.0562 1.0000
16.000 1.1383 0.06236 0.05642 0.0332 0.0548 1.0000
16.250 1.1460 0.06428 0.05833 0.0328 0.0532 1.0000
16.500 1.1548 0.06714 0.06122 0.0327 0.0514 1.0000
16.750 1.1412 0.07112 0.06544 0.0315 0.0508 1.0000
17.000 1.1258 0.07566 0.07023 0.0298 0.0500 1.0000
17.250 1.1109 0.08062 0.07541 0.0278 0.0492 1.0000
17.500 1.0954 0.08594 0.08094 0.0254 0.0483 1.0000
17.750 1.0809 0.09138 0.08658 0.0227 0.0475 1.0000
18.000 1.0715 0.09625 0.09156 0.0201 0.0464 1.0000
18.250 1.0604 0.10158 0.09701 0.0172 0.0456 1.0000
18.500 1.0850 0.10127 0.09650 0.0182 0.0435 1.0000
18.750 0.9950 0.12104 0.11696 0.0057 0.0452 1.0000
19.000 0.9822 0.12760 0.12360 0.0016 0.0444 1.0000
19.250 0.9647 0.13527 0.13134 -0.0030 0.0436 1.0000
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