NASA SC(2)-0606 AIRFOIL (sc20606-il) Xfoil prediction polar at RE=100,000 Ncrit=9
| Details | Polar file |
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Airfoil: NASA SC(2)-0606 AIRFOIL (sc20606-il) Reynolds number: 100,000 Max Cl/Cd: 31.74 at α=2° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-sc20606-il-100000.txt Download as CSV file: xf-sc20606-il-100000.csv |
XFOIL Version 6.96
Calculated polar for: NASA SC(2)-0606 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.100 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-9.500 -0.4937 0.09040 0.08555 -0.0131 1.0000 0.1056
-9.250 -0.5067 0.08640 0.08163 -0.0162 1.0000 0.1095
-9.000 -0.5320 0.08234 0.07768 -0.0213 1.0000 0.1106
-8.750 -0.6051 0.08949 0.08454 -0.0106 1.0000 0.1030
-8.500 -0.6076 0.08543 0.08054 -0.0143 1.0000 0.1076
-8.250 -0.6237 0.07780 0.07275 -0.0339 1.0000 0.1113
-8.000 -0.6034 0.07523 0.07039 -0.0238 1.0000 0.1158
-7.750 -0.6057 0.06893 0.06380 -0.0364 1.0000 0.1254
-7.500 -0.5908 0.06595 0.06103 -0.0308 1.0000 0.1300
-7.250 -0.5816 0.06106 0.05600 -0.0354 1.0000 0.1416
-7.000 -0.5682 0.05700 0.05183 -0.0378 1.0000 0.1552
-6.750 -0.5535 0.05377 0.04855 -0.0377 1.0000 0.1713
-6.500 -0.5385 0.05072 0.04546 -0.0383 1.0000 0.1983
-6.250 -0.4674 0.03650 0.02875 -0.0530 1.0000 0.0833
-6.000 -0.4354 0.03091 0.02257 -0.0541 1.0000 0.0689
-5.750 -0.4058 0.02717 0.01846 -0.0549 1.0000 0.0659
-5.500 -0.3755 0.02438 0.01521 -0.0552 1.0000 0.0649
-5.250 -0.3461 0.02238 0.01281 -0.0550 1.0000 0.0677
-5.000 -0.3185 0.02041 0.01072 -0.0550 1.0000 0.0742
-4.750 -0.2910 0.01885 0.00906 -0.0545 1.0000 0.0807
-4.500 -0.2633 0.01737 0.00760 -0.0544 1.0000 0.0955
-4.250 -0.2336 0.01585 0.00627 -0.0549 1.0000 0.1237
-4.000 -0.1986 0.01241 0.00552 -0.0574 1.0000 0.6201
-3.750 -0.1842 0.01277 0.00599 -0.0526 1.0000 0.7214
-3.500 -0.1694 0.01308 0.00624 -0.0483 1.0000 0.7678
-3.250 -0.1601 0.01329 0.00642 -0.0427 1.0000 0.8027
-3.000 -0.1506 0.01336 0.00645 -0.0374 1.0000 0.8346
-2.750 -0.1447 0.01325 0.00633 -0.0313 1.0000 0.8673
-2.500 -0.1416 0.01288 0.00596 -0.0247 1.0000 0.8996
-2.250 -0.1342 0.01233 0.00537 -0.0196 1.0000 0.9332
-2.000 -0.1158 0.01165 0.00463 -0.0172 1.0000 0.9673
-1.750 -0.0795 0.01126 0.00414 -0.0193 1.0000 1.0000
-1.500 -0.0501 0.01117 0.00396 -0.0208 1.0000 1.0000
-1.250 -0.0181 0.01114 0.00385 -0.0228 1.0000 1.0000
-1.000 0.0152 0.01115 0.00381 -0.0249 1.0000 1.0000
-0.750 0.0489 0.01119 0.00381 -0.0271 1.0000 1.0000
-0.500 0.0827 0.01126 0.00387 -0.0291 1.0000 1.0000
-0.250 0.1163 0.01135 0.00397 -0.0311 1.0000 1.0000
0.000 0.1497 0.01146 0.00413 -0.0330 1.0000 1.0000
0.250 0.1826 0.01159 0.00433 -0.0347 1.0000 1.0000
0.500 0.2150 0.01175 0.00456 -0.0363 1.0000 1.0000
0.750 0.2469 0.01192 0.00485 -0.0378 1.0000 1.0000
1.000 0.2784 0.01212 0.00522 -0.0392 1.0000 1.0000
1.250 0.3092 0.01234 0.00561 -0.0404 1.0000 1.0000
1.500 0.3396 0.01259 0.00606 -0.0415 1.0000 1.0000
1.750 0.3694 0.01287 0.00660 -0.0425 1.0000 1.0000
2.000 0.4786 0.01508 0.00585 -0.0535 0.1546 1.0000
2.250 0.5042 0.01684 0.00723 -0.0532 0.1049 1.0000
2.500 0.5322 0.01841 0.00873 -0.0530 0.0859 1.0000
2.750 0.5617 0.02015 0.01041 -0.0531 0.0742 1.0000
3.000 0.5928 0.02204 0.01244 -0.0532 0.0691 1.0000
3.250 0.6233 0.02492 0.01537 -0.0535 0.0657 1.0000
3.500 0.6534 0.02670 0.01767 -0.0532 0.0621 1.0000
3.750 0.6827 0.02973 0.02112 -0.0528 0.0631 1.0000
4.000 0.7109 0.03325 0.02493 -0.0524 0.0662 1.0000
4.500 0.7867 0.04912 0.04399 -0.0507 0.2064 1.0000
5.250 0.8308 0.05957 0.05486 -0.0496 0.1408 1.0000
5.500 0.8434 0.06346 0.05890 -0.0497 0.1267 1.0000
5.750 0.8608 0.06794 0.06320 -0.0486 0.1207 1.0000
6.000 0.8652 0.07199 0.06771 -0.0505 0.1100 1.0000
6.250 0.8843 0.07796 0.07334 -0.0488 0.1063 1.0000
6.500 0.8743 0.08199 0.07800 -0.0538 0.0991 1.0000
6.750 0.8841 0.08597 0.08198 -0.0530 0.0946 1.0000
7.000 0.8976 0.09257 0.08840 -0.0511 0.0920 1.0000
7.250 0.8778 0.09714 0.09329 -0.0589 0.0901 1.0000
7.500 0.7305 0.09435 0.09070 -0.0515 0.1017 1.0000
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Polar data table (+)
Polar graphs
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