NASA SC(2)-0012 AIRFOIL (sc20012-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: NASA SC(2)-0012 AIRFOIL (sc20012-il) Reynolds number: 1,000,000 Max Cl/Cd: 71.76 at α=9° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-sc20012-il-1000000.txt Download as CSV file: xf-sc20012-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: NASA SC(2)-0012 AIRFOIL
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
------ -------- --------- --------- -------- -------- --------
-19.000 -1.1266 0.13239 0.12994 0.0144 1.0000 0.0158
-18.750 -1.1716 0.11888 0.11625 0.0066 1.0000 0.0157
-18.500 -1.2097 0.10714 0.10434 -0.0002 1.0000 0.0157
-18.250 -1.2439 0.09645 0.09349 -0.0063 1.0000 0.0157
-18.000 -1.2730 0.08682 0.08369 -0.0118 1.0000 0.0157
-17.750 -1.2971 0.07837 0.07507 -0.0167 1.0000 0.0157
-17.500 -1.3160 0.07112 0.06767 -0.0208 1.0000 0.0157
-17.250 -1.3317 0.06485 0.06124 -0.0241 1.0000 0.0157
-17.000 -1.3438 0.05960 0.05584 -0.0265 1.0000 0.0157
-16.750 -1.3533 0.05507 0.05118 -0.0282 1.0000 0.0158
-16.500 -1.3594 0.05128 0.04726 -0.0292 1.0000 0.0158
-16.250 -1.3622 0.04805 0.04391 -0.0299 1.0000 0.0158
-16.000 -1.3732 0.04408 0.03979 -0.0301 1.0000 0.0159
-15.750 -1.3827 0.04049 0.03606 -0.0299 1.0000 0.0161
-15.500 -1.3875 0.03754 0.03298 -0.0294 1.0000 0.0162
-15.250 -1.3882 0.03510 0.03044 -0.0286 1.0000 0.0164
-15.000 -1.3862 0.03302 0.02826 -0.0277 1.0000 0.0165
-14.750 -1.3820 0.03121 0.02636 -0.0266 1.0000 0.0166
-14.500 -1.3760 0.02963 0.02471 -0.0254 1.0000 0.0168
-14.250 -1.3684 0.02826 0.02325 -0.0240 1.0000 0.0169
-14.000 -1.3598 0.02701 0.02193 -0.0226 1.0000 0.0171
-13.750 -1.3500 0.02590 0.02075 -0.0210 1.0000 0.0172
-13.500 -1.3396 0.02490 0.01967 -0.0192 1.0000 0.0174
-13.250 -1.3286 0.02397 0.01867 -0.0173 1.0000 0.0176
-13.000 -1.3172 0.02314 0.01776 -0.0153 1.0000 0.0178
-12.750 -1.3043 0.02237 0.01693 -0.0134 1.0000 0.0180
-12.500 -1.2883 0.02163 0.01612 -0.0119 1.0000 0.0182
-12.250 -1.2707 0.02093 0.01535 -0.0107 1.0000 0.0185
-12.000 -1.2520 0.02027 0.01462 -0.0096 1.0000 0.0187
-11.750 -1.2320 0.01967 0.01396 -0.0086 1.0000 0.0189
-11.500 -1.2140 0.01886 0.01308 -0.0074 1.0000 0.0192
-11.250 -1.1955 0.01804 0.01223 -0.0063 1.0000 0.0198
-11.000 -1.1743 0.01745 0.01160 -0.0054 1.0000 0.0203
-10.750 -1.1520 0.01694 0.01107 -0.0048 1.0000 0.0208
-10.500 -1.1292 0.01646 0.01055 -0.0041 1.0000 0.0214
-10.250 -1.1059 0.01601 0.01006 -0.0036 1.0000 0.0220
-10.000 -1.0823 0.01558 0.00959 -0.0030 1.0000 0.0226
-9.750 -1.0601 0.01496 0.00897 -0.0023 1.0000 0.0238
-9.500 -1.0359 0.01457 0.00858 -0.0018 1.0000 0.0249
-9.250 -1.0111 0.01424 0.00821 -0.0015 1.0000 0.0261
-9.000 -0.9874 0.01376 0.00775 -0.0009 1.0000 0.0279
-8.750 -0.9623 0.01344 0.00744 -0.0005 1.0000 0.0297
-8.500 -0.9375 0.01310 0.00709 -0.0001 1.0000 0.0315
-8.250 -0.9127 0.01278 0.00680 0.0003 1.0000 0.0336
-8.000 -0.8872 0.01257 0.00657 0.0006 1.0000 0.0354
-7.750 -0.8633 0.01222 0.00625 0.0012 1.0000 0.0375
-7.500 -0.8329 0.01197 0.00601 0.0005 0.9965 0.0396
-7.250 -0.7983 0.01178 0.00580 -0.0011 0.9886 0.0413
-7.000 -0.7662 0.01139 0.00543 -0.0023 0.9764 0.0440
-6.750 -0.7364 0.01118 0.00521 -0.0028 0.9589 0.0460
-6.500 -0.7108 0.01105 0.00503 -0.0022 0.9366 0.0475
-6.250 -0.6872 0.01079 0.00472 -0.0013 0.9136 0.0500
-6.000 -0.6621 0.01062 0.00450 -0.0007 0.8932 0.0523
-5.750 -0.6360 0.01050 0.00431 -0.0003 0.8759 0.0543
-5.500 -0.6096 0.01033 0.00407 0.0000 0.8613 0.0565
-5.250 -0.5831 0.01010 0.00383 0.0003 0.8490 0.0599
-5.000 -0.5557 0.00996 0.00365 0.0003 0.8391 0.0629
-4.750 -0.5285 0.00976 0.00344 0.0004 0.8303 0.0674
-4.500 -0.5011 0.00958 0.00325 0.0005 0.8232 0.0721
-4.250 -0.4734 0.00937 0.00307 0.0005 0.8168 0.0791
-4.000 -0.4460 0.00917 0.00290 0.0005 0.8108 0.0901
-3.750 -0.4185 0.00894 0.00273 0.0006 0.8053 0.1078
-3.500 -0.3908 0.00870 0.00258 0.0005 0.8003 0.1290
-3.250 -0.3634 0.00842 0.00242 0.0005 0.7954 0.1600
-3.000 -0.3364 0.00810 0.00227 0.0005 0.7910 0.2044
-2.750 -0.3093 0.00776 0.00212 0.0005 0.7869 0.2569
-2.500 -0.2826 0.00728 0.00196 0.0005 0.7831 0.3343
-2.250 -0.2565 0.00672 0.00177 0.0006 0.7782 0.4353
-2.000 -0.2311 0.00612 0.00160 0.0008 0.7726 0.5541
-1.750 -0.2040 0.00585 0.00160 0.0010 0.7671 0.6334
-1.500 -0.1749 0.00581 0.00160 0.0008 0.7627 0.6611
-1.250 -0.1456 0.00580 0.00160 0.0006 0.7578 0.6768
-1.000 -0.1168 0.00580 0.00160 0.0006 0.7521 0.6879
-0.750 -0.0874 0.00579 0.00159 0.0004 0.7464 0.6976
-0.500 -0.0582 0.00577 0.00159 0.0002 0.7403 0.7081
-0.250 -0.0291 0.00579 0.00159 0.0001 0.7342 0.7173
0.000 0.0000 0.00579 0.00161 0.0000 0.7275 0.7277
0.250 0.0291 0.00579 0.00159 -0.0001 0.7172 0.7341
0.500 0.0582 0.00577 0.00160 -0.0002 0.7083 0.7404
0.750 0.0873 0.00579 0.00159 -0.0004 0.6975 0.7465
1.000 0.1168 0.00580 0.00160 -0.0006 0.6880 0.7520
1.250 0.1456 0.00580 0.00160 -0.0006 0.6769 0.7581
1.500 0.1749 0.00581 0.00160 -0.0008 0.6611 0.7627
1.750 0.2040 0.00585 0.00159 -0.0009 0.6332 0.7670
2.000 0.2311 0.00612 0.00160 -0.0008 0.5541 0.7726
2.250 0.2565 0.00672 0.00177 -0.0006 0.4347 0.7784
2.500 0.2826 0.00729 0.00196 -0.0005 0.3334 0.7831
2.750 0.3093 0.00776 0.00212 -0.0005 0.2565 0.7869
3.000 0.3364 0.00809 0.00227 -0.0005 0.2046 0.7910
3.250 0.3634 0.00842 0.00242 -0.0005 0.1602 0.7954
3.500 0.3908 0.00870 0.00258 -0.0005 0.1290 0.8002
3.750 0.4185 0.00894 0.00273 -0.0006 0.1078 0.8053
4.000 0.4460 0.00917 0.00290 -0.0005 0.0901 0.8108
4.250 0.4734 0.00937 0.00307 -0.0005 0.0791 0.8168
4.500 0.5011 0.00958 0.00325 -0.0005 0.0721 0.8232
4.750 0.5286 0.00975 0.00344 -0.0004 0.0675 0.8303
5.000 0.5557 0.00996 0.00366 -0.0003 0.0629 0.8391
5.250 0.5831 0.01010 0.00383 -0.0003 0.0599 0.8490
5.500 0.6096 0.01033 0.00407 0.0000 0.0564 0.8614
5.750 0.6360 0.01050 0.00431 0.0003 0.0543 0.8759
6.000 0.6621 0.01062 0.00450 0.0007 0.0523 0.8932
6.250 0.6872 0.01079 0.00472 0.0013 0.0500 0.9135
6.500 0.7109 0.01105 0.00503 0.0022 0.0475 0.9366
6.750 0.7364 0.01118 0.00521 0.0028 0.0460 0.9589
7.000 0.7663 0.01139 0.00543 0.0023 0.0440 0.9764
7.250 0.7984 0.01177 0.00579 0.0011 0.0413 0.9886
7.500 0.8330 0.01197 0.00601 -0.0005 0.0396 0.9965
7.750 0.8633 0.01222 0.00625 -0.0012 0.0375 1.0000
8.000 0.8872 0.01257 0.00657 -0.0006 0.0354 1.0000
8.250 0.9127 0.01278 0.00680 -0.0003 0.0336 1.0000
8.500 0.9375 0.01310 0.00709 0.0001 0.0315 1.0000
8.750 0.9624 0.01344 0.00744 0.0005 0.0297 1.0000
9.000 0.9874 0.01376 0.00775 0.0009 0.0279 1.0000
9.250 1.0111 0.01423 0.00821 0.0014 0.0261 1.0000
9.500 1.0360 0.01457 0.00858 0.0018 0.0249 1.0000
9.750 1.0602 0.01496 0.00897 0.0023 0.0238 1.0000
10.000 1.0823 0.01558 0.00959 0.0030 0.0225 1.0000
10.250 1.1060 0.01601 0.01006 0.0035 0.0220 1.0000
10.500 1.1293 0.01646 0.01055 0.0041 0.0214 1.0000
10.750 1.1522 0.01694 0.01106 0.0047 0.0208 1.0000
11.000 1.1745 0.01745 0.01160 0.0054 0.0203 1.0000
11.250 1.1956 0.01804 0.01223 0.0062 0.0198 1.0000
11.500 1.2142 0.01886 0.01308 0.0074 0.0192 1.0000
11.750 1.2322 0.01967 0.01396 0.0086 0.0189 1.0000
12.000 1.2522 0.02027 0.01463 0.0095 0.0187 1.0000
12.250 1.2710 0.02092 0.01535 0.0106 0.0185 1.0000
12.500 1.2886 0.02163 0.01612 0.0119 0.0182 1.0000
12.750 1.3047 0.02237 0.01693 0.0133 0.0180 1.0000
13.000 1.3177 0.02313 0.01776 0.0152 0.0178 1.0000
13.250 1.3292 0.02397 0.01867 0.0172 0.0176 1.0000
13.500 1.3402 0.02489 0.01966 0.0191 0.0174 1.0000
13.750 1.3507 0.02590 0.02074 0.0209 0.0172 1.0000
14.000 1.3604 0.02701 0.02193 0.0224 0.0171 1.0000
14.250 1.3692 0.02825 0.02324 0.0239 0.0169 1.0000
14.500 1.3768 0.02963 0.02470 0.0253 0.0168 1.0000
14.750 1.3829 0.03120 0.02635 0.0265 0.0166 1.0000
15.000 1.3872 0.03300 0.02824 0.0276 0.0165 1.0000
15.250 1.3893 0.03508 0.03042 0.0285 0.0164 1.0000
15.500 1.3886 0.03753 0.03297 0.0292 0.0162 1.0000
15.750 1.3841 0.04046 0.03603 0.0297 0.0161 1.0000
16.000 1.3745 0.04407 0.03978 0.0299 0.0159 1.0000
16.250 1.3647 0.04789 0.04375 0.0297 0.0158 1.0000
16.500 1.3614 0.05118 0.04716 0.0290 0.0158 1.0000
16.750 1.3548 0.05504 0.05115 0.0280 0.0158 1.0000
17.000 1.3458 0.05951 0.05575 0.0263 0.0157 1.0000
17.250 1.3332 0.06484 0.06123 0.0239 0.0157 1.0000
17.500 1.3181 0.07102 0.06757 0.0206 0.0157 1.0000
17.750 1.2991 0.07831 0.07501 0.0165 0.0157 1.0000
18.000 1.2750 0.08676 0.08363 0.0116 0.0157 1.0000
18.250 1.2464 0.09633 0.09336 0.0060 0.0157 1.0000
18.500 1.2122 0.10705 0.10425 -0.0001 0.0157 1.0000
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