NASA SC(2)-0012 AIRFOIL (sc20012-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: NASA SC(2)-0012 AIRFOIL (sc20012-il) Reynolds number: 1,000,000 Max Cl/Cd: 72.91 at α=9.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-sc20012-il-1000000-n5.txt Download as CSV file: xf-sc20012-il-1000000-n5.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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.250 -1.2070 0.12258 0.11982 0.0093 1.0000 0.0123
-19.000 -1.2854 0.10350 0.10048 -0.0013 1.0000 0.0122
-18.750 -1.3482 0.08747 0.08419 -0.0102 1.0000 0.0121
-18.500 -1.3879 0.07610 0.07260 -0.0168 1.0000 0.0121
-18.250 -1.4136 0.06778 0.06410 -0.0215 1.0000 0.0121
-18.000 -1.4317 0.06135 0.05750 -0.0248 1.0000 0.0121
-17.750 -1.4449 0.05614 0.05215 -0.0269 1.0000 0.0121
-17.500 -1.4544 0.05185 0.04773 -0.0283 1.0000 0.0122
-17.250 -1.4614 0.04812 0.04388 -0.0290 1.0000 0.0122
-17.000 -1.4655 0.04490 0.04054 -0.0294 1.0000 0.0123
-16.750 -1.4673 0.04207 0.03760 -0.0294 1.0000 0.0123
-16.500 -1.4671 0.03955 0.03497 -0.0293 1.0000 0.0124
-16.250 -1.4652 0.03728 0.03260 -0.0289 1.0000 0.0125
-16.000 -1.4617 0.03525 0.03047 -0.0283 1.0000 0.0125
-15.750 -1.4568 0.03341 0.02854 -0.0275 1.0000 0.0126
-15.500 -1.4506 0.03176 0.02679 -0.0267 1.0000 0.0127
-15.250 -1.4433 0.03026 0.02520 -0.0256 1.0000 0.0127
-15.000 -1.4349 0.02891 0.02377 -0.0245 1.0000 0.0128
-14.750 -1.4256 0.02768 0.02245 -0.0232 1.0000 0.0129
-14.500 -1.4155 0.02657 0.02126 -0.0219 1.0000 0.0129
-14.250 -1.4044 0.02557 0.02018 -0.0204 1.0000 0.0130
-14.000 -1.3945 0.02453 0.01906 -0.0186 1.0000 0.0131
-13.750 -1.3843 0.02355 0.01802 -0.0167 1.0000 0.0133
-13.500 -1.3730 0.02271 0.01711 -0.0147 1.0000 0.0135
-13.250 -1.3602 0.02196 0.01631 -0.0127 1.0000 0.0137
-13.000 -1.3440 0.02126 0.01556 -0.0113 1.0000 0.0139
-12.750 -1.3262 0.02061 0.01485 -0.0101 1.0000 0.0141
-12.500 -1.3074 0.01999 0.01419 -0.0091 1.0000 0.0143
-12.250 -1.2876 0.01940 0.01356 -0.0081 1.0000 0.0145
-12.000 -1.2671 0.01884 0.01295 -0.0072 1.0000 0.0148
-11.750 -1.2460 0.01831 0.01238 -0.0064 1.0000 0.0150
-11.500 -1.2242 0.01781 0.01183 -0.0057 1.0000 0.0153
-11.250 -1.2020 0.01733 0.01131 -0.0050 1.0000 0.0156
-11.000 -1.1792 0.01687 0.01082 -0.0044 1.0000 0.0158
-10.750 -1.1568 0.01636 0.01028 -0.0038 1.0000 0.0163
-10.500 -1.1337 0.01589 0.00979 -0.0032 1.0000 0.0168
-10.250 -1.1102 0.01546 0.00934 -0.0027 1.0000 0.0174
-10.000 -1.0863 0.01505 0.00892 -0.0022 1.0000 0.0181
-9.750 -1.0620 0.01468 0.00852 -0.0018 1.0000 0.0188
-9.500 -1.0378 0.01428 0.00811 -0.0013 1.0000 0.0198
-9.250 -1.0133 0.01390 0.00774 -0.0009 1.0000 0.0209
-9.000 -0.9844 0.01355 0.00737 -0.0014 0.9880 0.0221
-8.750 -0.9544 0.01319 0.00701 -0.0022 0.9713 0.0235
-8.500 -0.9271 0.01289 0.00669 -0.0022 0.9500 0.0252
-8.250 -0.9030 0.01266 0.00639 -0.0015 0.9250 0.0266
-8.000 -0.8795 0.01242 0.00611 -0.0007 0.9016 0.0284
-7.750 -0.8547 0.01223 0.00584 -0.0001 0.8810 0.0301
-7.500 -0.8293 0.01202 0.00557 0.0004 0.8628 0.0317
-7.250 -0.8034 0.01181 0.00532 0.0007 0.8469 0.0336
-7.000 -0.7770 0.01163 0.00508 0.0009 0.8338 0.0352
-6.750 -0.7504 0.01143 0.00484 0.0011 0.8229 0.0369
-6.500 -0.7236 0.01123 0.00462 0.0012 0.8133 0.0388
-6.250 -0.6965 0.01106 0.00441 0.0013 0.8052 0.0407
-6.000 -0.6692 0.01087 0.00420 0.0014 0.7979 0.0425
-5.750 -0.6420 0.01068 0.00401 0.0014 0.7911 0.0447
-5.500 -0.6144 0.01052 0.00382 0.0014 0.7856 0.0466
-5.250 -0.5867 0.01035 0.00364 0.0014 0.7804 0.0487
-5.000 -0.5591 0.01016 0.00346 0.0014 0.7754 0.0520
-4.750 -0.5313 0.01002 0.00331 0.0014 0.7708 0.0548
-4.500 -0.5034 0.00984 0.00313 0.0014 0.7671 0.0580
-4.250 -0.4753 0.00967 0.00298 0.0013 0.7635 0.0614
-4.000 -0.4472 0.00951 0.00283 0.0012 0.7599 0.0655
-3.750 -0.4192 0.00935 0.00269 0.0012 0.7562 0.0713
-3.500 -0.3911 0.00919 0.00256 0.0011 0.7524 0.0797
-3.250 -0.3631 0.00901 0.00243 0.0010 0.7489 0.0916
-3.000 -0.3348 0.00883 0.00231 0.0009 0.7457 0.1058
-2.750 -0.3065 0.00866 0.00220 0.0008 0.7423 0.1202
-2.500 -0.2783 0.00849 0.00210 0.0007 0.7384 0.1370
-2.250 -0.2504 0.00829 0.00198 0.0006 0.7333 0.1646
-2.000 -0.2224 0.00805 0.00188 0.0005 0.7282 0.1984
-1.750 -0.1943 0.00781 0.00177 0.0004 0.7226 0.2351
-1.500 -0.1665 0.00755 0.00167 0.0003 0.7177 0.2832
-1.250 -0.1390 0.00723 0.00156 0.0002 0.7125 0.3463
-1.000 -0.1114 0.00686 0.00145 0.0001 0.7070 0.4164
-0.750 -0.0842 0.00645 0.00133 0.0001 0.6997 0.5035
-0.500 -0.0577 0.00600 0.00128 0.0002 0.6923 0.6143
-0.250 -0.0290 0.00591 0.00130 0.0001 0.6845 0.6532
0.000 0.0000 0.00590 0.00131 0.0000 0.6741 0.6743
0.250 0.0290 0.00591 0.00130 -0.0001 0.6527 0.6844
0.500 0.0577 0.00600 0.00128 -0.0002 0.6153 0.6924
0.750 0.0842 0.00645 0.00133 -0.0001 0.5024 0.6998
1.000 0.1114 0.00686 0.00145 -0.0001 0.4168 0.7069
1.250 0.1390 0.00723 0.00156 -0.0002 0.3463 0.7127
1.500 0.1665 0.00755 0.00167 -0.0003 0.2831 0.7178
1.750 0.1943 0.00781 0.00177 -0.0004 0.2347 0.7226
2.000 0.2224 0.00805 0.00188 -0.0005 0.1986 0.7283
2.250 0.2503 0.00829 0.00198 -0.0006 0.1644 0.7336
2.500 0.2782 0.00849 0.00210 -0.0007 0.1367 0.7384
2.750 0.3065 0.00866 0.00220 -0.0008 0.1202 0.7423
3.000 0.3348 0.00883 0.00231 -0.0009 0.1058 0.7457
3.250 0.3631 0.00901 0.00243 -0.0010 0.0917 0.7488
3.500 0.3911 0.00919 0.00256 -0.0011 0.0797 0.7523
3.750 0.4192 0.00935 0.00269 -0.0012 0.0712 0.7562
4.000 0.4472 0.00951 0.00283 -0.0012 0.0655 0.7599
4.250 0.4753 0.00967 0.00298 -0.0013 0.0614 0.7635
4.500 0.5034 0.00984 0.00313 -0.0014 0.0580 0.7670
4.750 0.5313 0.01002 0.00331 -0.0014 0.0548 0.7708
5.000 0.5591 0.01016 0.00346 -0.0014 0.0521 0.7753
5.250 0.5867 0.01035 0.00364 -0.0014 0.0487 0.7804
5.500 0.6144 0.01052 0.00382 -0.0014 0.0466 0.7856
5.750 0.6420 0.01068 0.00401 -0.0014 0.0447 0.7911
6.000 0.6692 0.01087 0.00420 -0.0014 0.0425 0.7979
6.250 0.6965 0.01106 0.00441 -0.0013 0.0406 0.8052
6.500 0.7236 0.01123 0.00462 -0.0012 0.0388 0.8133
6.750 0.7504 0.01143 0.00484 -0.0011 0.0369 0.8229
7.000 0.7770 0.01163 0.00508 -0.0009 0.0352 0.8337
7.250 0.8034 0.01181 0.00532 -0.0007 0.0336 0.8468
7.500 0.8293 0.01202 0.00557 -0.0004 0.0317 0.8627
7.750 0.8547 0.01223 0.00584 0.0001 0.0301 0.8809
8.000 0.8795 0.01242 0.00611 0.0007 0.0284 0.9016
8.250 0.9031 0.01266 0.00639 0.0015 0.0266 0.9250
8.500 0.9271 0.01289 0.00669 0.0022 0.0252 0.9500
8.750 0.9545 0.01319 0.00701 0.0022 0.0236 0.9713
9.000 0.9845 0.01355 0.00737 0.0014 0.0221 0.9881
9.250 1.0134 0.01390 0.00774 0.0009 0.0209 1.0000
9.500 1.0379 0.01428 0.00811 0.0013 0.0197 1.0000
9.750 1.0621 0.01468 0.00852 0.0018 0.0188 1.0000
10.000 1.0864 0.01505 0.00892 0.0022 0.0181 1.0000
10.250 1.1103 0.01545 0.00934 0.0027 0.0174 1.0000
10.500 1.1338 0.01589 0.00979 0.0032 0.0168 1.0000
10.750 1.1568 0.01636 0.01028 0.0038 0.0163 1.0000
11.000 1.1793 0.01687 0.01082 0.0044 0.0158 1.0000
11.250 1.2021 0.01733 0.01131 0.0050 0.0156 1.0000
11.500 1.2244 0.01781 0.01183 0.0057 0.0153 1.0000
11.750 1.2461 0.01831 0.01238 0.0064 0.0150 1.0000
12.000 1.2673 0.01884 0.01295 0.0072 0.0148 1.0000
12.250 1.2878 0.01940 0.01355 0.0081 0.0145 1.0000
12.500 1.3076 0.01998 0.01418 0.0090 0.0143 1.0000
12.750 1.3265 0.02061 0.01485 0.0101 0.0141 1.0000
13.000 1.3444 0.02126 0.01556 0.0112 0.0139 1.0000
13.250 1.3607 0.02196 0.01630 0.0126 0.0137 1.0000
13.500 1.3736 0.02270 0.01710 0.0146 0.0135 1.0000
13.750 1.3848 0.02356 0.01802 0.0166 0.0133 1.0000
14.000 1.3950 0.02454 0.01907 0.0185 0.0131 1.0000
14.250 1.4051 0.02557 0.02018 0.0203 0.0130 1.0000
14.500 1.4163 0.02657 0.02126 0.0217 0.0129 1.0000
14.750 1.4266 0.02767 0.02244 0.0231 0.0129 1.0000
15.000 1.4359 0.02890 0.02375 0.0243 0.0128 1.0000
15.250 1.4444 0.03024 0.02518 0.0255 0.0127 1.0000
15.500 1.4519 0.03173 0.02676 0.0265 0.0127 1.0000
15.750 1.4580 0.03338 0.02851 0.0274 0.0126 1.0000
16.000 1.4630 0.03522 0.03044 0.0281 0.0125 1.0000
16.250 1.4667 0.03723 0.03256 0.0287 0.0125 1.0000
16.500 1.4688 0.03949 0.03491 0.0290 0.0124 1.0000
16.750 1.4689 0.04203 0.03756 0.0292 0.0123 1.0000
17.000 1.4674 0.04482 0.04046 0.0292 0.0123 1.0000
17.250 1.4632 0.04807 0.04383 0.0288 0.0122 1.0000
17.500 1.4566 0.05175 0.04763 0.0280 0.0122 1.0000
17.750 1.4472 0.05604 0.05205 0.0267 0.0121 1.0000
18.000 1.4340 0.06124 0.05740 0.0245 0.0121 1.0000
18.250 1.4164 0.06759 0.06391 0.0213 0.0121 1.0000
18.500 1.3911 0.07585 0.07235 0.0167 0.0121 1.0000
18.750 1.3515 0.08722 0.08394 0.0100 0.0121 1.0000
19.000 1.2890 0.10321 0.10019 0.0011 0.0122 1.0000
19.250 1.2099 0.12241 0.11965 -0.0095 0.0123 1.0000
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