NACA 0012 AIRFOILS (n0012-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: NACA 0012 AIRFOILS (n0012-il) Reynolds number: 1,000,000 Max Cl/Cd: 75.6 at α=7.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-n0012-il-1000000.txt Download as CSV file: xf-n0012-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: NACA 0012 AIRFOILS
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
------ -------- --------- --------- -------- -------- --------
-18.500 -1.2258 0.10236 0.09929 -0.0012 1.0000 0.0135
-18.250 -1.2456 0.09505 0.09187 -0.0049 1.0000 0.0136
-18.000 -1.2659 0.08782 0.08451 -0.0086 1.0000 0.0136
-17.750 -1.2852 0.08088 0.07744 -0.0121 1.0000 0.0136
-17.500 -1.3031 0.07429 0.07074 -0.0154 1.0000 0.0137
-17.250 -1.3193 0.06814 0.06446 -0.0185 1.0000 0.0137
-17.000 -1.3322 0.06256 0.05874 -0.0213 1.0000 0.0137
-16.750 -1.3427 0.05745 0.05351 -0.0238 1.0000 0.0138
-16.500 -1.3519 0.05263 0.04856 -0.0261 1.0000 0.0139
-16.250 -1.3687 0.04704 0.04283 -0.0285 1.0000 0.0140
-16.000 -1.3806 0.04234 0.03800 -0.0303 1.0000 0.0142
-15.750 -1.3868 0.03865 0.03420 -0.0313 1.0000 0.0144
-15.500 -1.3879 0.03577 0.03122 -0.0317 1.0000 0.0146
-15.250 -1.3854 0.03348 0.02885 -0.0317 1.0000 0.0148
-15.000 -1.3802 0.03160 0.02690 -0.0313 1.0000 0.0151
-14.750 -1.3739 0.02997 0.02518 -0.0305 1.0000 0.0153
-14.500 -1.3669 0.02849 0.02363 -0.0295 1.0000 0.0156
-14.250 -1.3590 0.02718 0.02223 -0.0283 1.0000 0.0159
-14.000 -1.3502 0.02602 0.02099 -0.0268 1.0000 0.0162
-13.750 -1.3399 0.02502 0.01991 -0.0252 1.0000 0.0164
-13.500 -1.3281 0.02416 0.01896 -0.0236 1.0000 0.0167
-13.250 -1.3149 0.02343 0.01816 -0.0219 1.0000 0.0169
-13.000 -1.3132 0.02207 0.01670 -0.0187 1.0000 0.0174
-12.750 -1.3004 0.02117 0.01576 -0.0169 1.0000 0.0179
-12.500 -1.2834 0.02049 0.01504 -0.0156 1.0000 0.0183
-12.250 -1.2649 0.01988 0.01438 -0.0144 1.0000 0.0188
-12.000 -1.2455 0.01931 0.01376 -0.0134 1.0000 0.0194
-11.750 -1.2250 0.01881 0.01321 -0.0124 1.0000 0.0199
-11.500 -1.2032 0.01839 0.01274 -0.0116 1.0000 0.0203
-11.250 -1.1872 0.01745 0.01175 -0.0101 1.0000 0.0213
-11.000 -1.1666 0.01690 0.01118 -0.0091 1.0000 0.0220
-10.750 -1.1449 0.01645 0.01069 -0.0082 1.0000 0.0228
-10.500 -1.1228 0.01602 0.01023 -0.0074 1.0000 0.0236
-10.250 -1.1000 0.01566 0.00982 -0.0066 1.0000 0.0242
-10.000 -1.0807 0.01499 0.00912 -0.0053 1.0000 0.0255
-9.750 -1.0591 0.01456 0.00868 -0.0043 1.0000 0.0266
-9.500 -1.0368 0.01423 0.00833 -0.0034 1.0000 0.0278
-9.250 -1.0143 0.01395 0.00801 -0.0024 1.0000 0.0288
-9.000 -0.9948 0.01341 0.00747 -0.0010 1.0000 0.0306
-8.750 -0.9735 0.01307 0.00712 0.0002 1.0000 0.0322
-8.500 -0.9517 0.01279 0.00682 0.0014 1.0000 0.0337
-8.250 -0.9313 0.01240 0.00642 0.0027 1.0000 0.0358
-8.000 -0.9104 0.01209 0.00612 0.0040 1.0000 0.0382
-7.750 -0.8888 0.01187 0.00587 0.0052 1.0000 0.0401
-7.500 -0.8687 0.01149 0.00552 0.0067 1.0000 0.0435
-7.250 -0.8475 0.01124 0.00527 0.0080 1.0000 0.0464
-7.000 -0.8268 0.01095 0.00500 0.0093 1.0000 0.0505
-6.750 -0.7975 0.01069 0.00475 0.0088 0.9992 0.0550
-6.500 -0.7634 0.01034 0.00446 0.0073 0.9975 0.0624
-6.250 -0.7289 0.01003 0.00419 0.0058 0.9959 0.0709
-6.000 -0.6939 0.00973 0.00395 0.0041 0.9944 0.0815
-5.750 -0.6601 0.00942 0.00371 0.0026 0.9924 0.0940
-5.500 -0.6268 0.00911 0.00348 0.0014 0.9897 0.1090
-5.000 -0.5571 0.00847 0.00304 -0.0019 0.9853 0.1490
-4.750 -0.5213 0.00816 0.00284 -0.0038 0.9836 0.1728
-4.500 -0.4903 0.00786 0.00266 -0.0045 0.9789 0.1984
-4.250 -0.4588 0.00756 0.00248 -0.0053 0.9738 0.2257
-4.000 -0.4276 0.00728 0.00232 -0.0061 0.9687 0.2535
-3.750 -0.4004 0.00705 0.00217 -0.0058 0.9599 0.2804
-3.500 -0.3730 0.00681 0.00204 -0.0057 0.9511 0.3089
-3.250 -0.3462 0.00659 0.00191 -0.0053 0.9409 0.3366
-3.000 -0.3201 0.00640 0.00180 -0.0048 0.9284 0.3637
-2.750 -0.2938 0.00623 0.00170 -0.0043 0.9152 0.3920
-2.500 -0.2675 0.00606 0.00160 -0.0038 0.9007 0.4195
-2.250 -0.2410 0.00593 0.00151 -0.0034 0.8848 0.4469
-2.000 -0.2144 0.00581 0.00144 -0.0030 0.8675 0.4744
-1.750 -0.1878 0.00570 0.00137 -0.0025 0.8486 0.5014
-1.500 -0.1611 0.00562 0.00131 -0.0021 0.8283 0.5286
-1.250 -0.1343 0.00556 0.00126 -0.0018 0.8072 0.5556
-1.000 -0.1075 0.00549 0.00122 -0.0014 0.7848 0.5826
-0.750 -0.0806 0.00546 0.00118 -0.0010 0.7610 0.6087
-0.500 -0.0538 0.00542 0.00116 -0.0007 0.7373 0.6352
-0.250 -0.0268 0.00541 0.00115 -0.0004 0.7123 0.6609
0.000 0.0000 0.00540 0.00114 0.0000 0.6872 0.6873
0.250 0.0269 0.00541 0.00115 0.0003 0.6611 0.7123
0.500 0.0538 0.00542 0.00116 0.0007 0.6353 0.7372
0.750 0.0806 0.00546 0.00118 0.0010 0.6088 0.7609
1.000 0.1075 0.00549 0.00122 0.0014 0.5826 0.7847
1.250 0.1344 0.00555 0.00126 0.0018 0.5560 0.8071
1.500 0.1611 0.00562 0.00131 0.0021 0.5281 0.8282
1.750 0.1878 0.00570 0.00137 0.0025 0.5018 0.8484
2.000 0.2144 0.00581 0.00144 0.0030 0.4743 0.8675
2.250 0.2410 0.00593 0.00151 0.0034 0.4468 0.8848
2.500 0.2675 0.00606 0.00160 0.0038 0.4196 0.9007
2.750 0.2938 0.00623 0.00170 0.0043 0.3917 0.9152
3.000 0.3201 0.00640 0.00180 0.0048 0.3637 0.9285
3.250 0.3462 0.00659 0.00191 0.0053 0.3366 0.9409
3.500 0.3730 0.00681 0.00204 0.0057 0.3090 0.9511
3.750 0.4004 0.00705 0.00218 0.0058 0.2803 0.9599
4.000 0.4276 0.00728 0.00232 0.0061 0.2536 0.9688
4.250 0.4588 0.00756 0.00248 0.0053 0.2255 0.9738
4.500 0.4903 0.00786 0.00265 0.0045 0.1986 0.9789
4.750 0.5213 0.00816 0.00284 0.0038 0.1728 0.9836
5.000 0.5572 0.00847 0.00304 0.0019 0.1488 0.9853
5.500 0.6268 0.00911 0.00348 -0.0014 0.1090 0.9897
5.750 0.6601 0.00942 0.00371 -0.0027 0.0939 0.9924
6.000 0.6940 0.00972 0.00395 -0.0041 0.0816 0.9944
6.250 0.7290 0.01003 0.00419 -0.0058 0.0709 0.9959
6.500 0.7635 0.01034 0.00446 -0.0074 0.0624 0.9976
6.750 0.7976 0.01069 0.00475 -0.0089 0.0550 0.9992
7.000 0.8267 0.01095 0.00499 -0.0093 0.0505 1.0000
7.250 0.8474 0.01124 0.00527 -0.0080 0.0464 1.0000
7.500 0.8686 0.01149 0.00552 -0.0067 0.0435 1.0000
7.750 0.8887 0.01186 0.00587 -0.0052 0.0401 1.0000
8.000 0.9103 0.01208 0.00612 -0.0040 0.0382 1.0000
8.250 0.9312 0.01240 0.00642 -0.0027 0.0359 1.0000
8.500 0.9516 0.01279 0.00682 -0.0013 0.0337 1.0000
8.750 0.9734 0.01307 0.00712 -0.0002 0.0322 1.0000
9.000 0.9948 0.01341 0.00747 0.0010 0.0306 1.0000
9.250 1.0143 0.01395 0.00801 0.0024 0.0288 1.0000
9.500 1.0368 0.01423 0.00832 0.0034 0.0278 1.0000
9.750 1.0591 0.01456 0.00868 0.0043 0.0266 1.0000
10.000 1.0808 0.01499 0.00912 0.0053 0.0255 1.0000
10.250 1.1001 0.01566 0.00982 0.0066 0.0242 1.0000
10.500 1.1229 0.01602 0.01023 0.0074 0.0236 1.0000
10.750 1.1450 0.01645 0.01069 0.0082 0.0228 1.0000
11.000 1.1668 0.01690 0.01118 0.0091 0.0220 1.0000
11.250 1.1874 0.01745 0.01175 0.0100 0.0213 1.0000
11.500 1.2033 0.01840 0.01274 0.0116 0.0203 1.0000
11.750 1.2251 0.01881 0.01321 0.0124 0.0199 1.0000
12.000 1.2457 0.01931 0.01376 0.0133 0.0194 1.0000
12.250 1.2651 0.01988 0.01438 0.0144 0.0188 1.0000
12.500 1.2837 0.02049 0.01504 0.0155 0.0183 1.0000
12.750 1.3008 0.02117 0.01576 0.0168 0.0179 1.0000
13.000 1.3137 0.02207 0.01670 0.0186 0.0174 1.0000
13.250 1.3157 0.02342 0.01815 0.0218 0.0169 1.0000
13.500 1.3290 0.02415 0.01895 0.0235 0.0167 1.0000
13.750 1.3406 0.02502 0.01991 0.0251 0.0164 1.0000
14.000 1.3509 0.02602 0.02099 0.0267 0.0162 1.0000
14.250 1.3600 0.02717 0.02222 0.0281 0.0159 1.0000
14.500 1.3679 0.02848 0.02361 0.0294 0.0156 1.0000
14.750 1.3750 0.02995 0.02516 0.0304 0.0153 1.0000
15.000 1.3814 0.03158 0.02687 0.0311 0.0151 1.0000
15.250 1.3864 0.03348 0.02885 0.0315 0.0148 1.0000
15.500 1.3892 0.03575 0.03121 0.0315 0.0146 1.0000
15.750 1.3881 0.03863 0.03418 0.0311 0.0144 1.0000
16.000 1.3818 0.04235 0.03800 0.0300 0.0142 1.0000
16.250 1.3702 0.04702 0.04280 0.0282 0.0140 1.0000
16.500 1.3536 0.05261 0.04854 0.0258 0.0139 1.0000
16.750 1.3451 0.05734 0.05340 0.0235 0.0138 1.0000
17.000 1.3352 0.06237 0.05856 0.0211 0.0137 1.0000
17.250 1.3218 0.06802 0.06434 0.0182 0.0137 1.0000
17.500 1.3059 0.07416 0.07060 0.0152 0.0136 1.0000
17.750 1.2880 0.08075 0.07731 0.0118 0.0136 1.0000
18.000 1.2685 0.08773 0.08442 0.0083 0.0136 1.0000
18.250 1.2485 0.09493 0.09174 0.0046 0.0136 1.0000
18.500 1.2284 0.10229 0.09922 0.0008 0.0135 1.0000
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