NACA 0012 AIRFOILS (n0012-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 0012 AIRFOILS (n0012-il) Reynolds number: 1,000,000 Max Cl/Cd: 75.44 at α=8.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-n0012-il-1000000-n5.txt Download as CSV file: xf-n0012-il-1000000-n5.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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.250 -1.2322 0.11416 0.11116 0.0052 1.0000 0.0103
-19.000 -1.2711 0.10336 0.10020 -0.0004 1.0000 0.0103
-18.750 -1.3084 0.09309 0.08977 -0.0057 1.0000 0.0103
-18.500 -1.3433 0.08350 0.08002 -0.0106 1.0000 0.0102
-18.250 -1.3730 0.07497 0.07133 -0.0150 1.0000 0.0102
-18.000 -1.3978 0.06745 0.06366 -0.0188 1.0000 0.0102
-17.750 -1.4170 0.06096 0.05702 -0.0221 1.0000 0.0103
-17.500 -1.4317 0.05530 0.05123 -0.0249 1.0000 0.0103
-17.250 -1.4420 0.05042 0.04621 -0.0272 1.0000 0.0104
-17.000 -1.4487 0.04625 0.04192 -0.0289 1.0000 0.0105
-16.750 -1.4524 0.04263 0.03818 -0.0303 1.0000 0.0106
-16.500 -1.4536 0.03953 0.03497 -0.0312 1.0000 0.0107
-16.250 -1.4526 0.03684 0.03218 -0.0316 1.0000 0.0109
-16.000 -1.4496 0.03454 0.02978 -0.0317 1.0000 0.0110
-15.750 -1.4453 0.03254 0.02768 -0.0314 1.0000 0.0111
-15.500 -1.4413 0.03064 0.02568 -0.0308 1.0000 0.0113
-15.250 -1.4375 0.02886 0.02382 -0.0298 1.0000 0.0115
-15.000 -1.4313 0.02740 0.02228 -0.0286 1.0000 0.0117
-14.750 -1.4233 0.02616 0.02097 -0.0272 1.0000 0.0119
-14.500 -1.4140 0.02508 0.01983 -0.0257 1.0000 0.0122
-14.250 -1.4035 0.02413 0.01881 -0.0240 1.0000 0.0124
-14.000 -1.3922 0.02328 0.01790 -0.0222 1.0000 0.0127
-13.750 -1.3800 0.02252 0.01708 -0.0204 1.0000 0.0129
-13.500 -1.3670 0.02183 0.01633 -0.0185 1.0000 0.0132
-13.250 -1.3515 0.02118 0.01561 -0.0170 1.0000 0.0135
-13.000 -1.3339 0.02057 0.01494 -0.0158 1.0000 0.0137
-12.750 -1.3161 0.01993 0.01424 -0.0145 1.0000 0.0140
-12.500 -1.2980 0.01928 0.01355 -0.0134 1.0000 0.0144
-12.250 -1.2785 0.01870 0.01294 -0.0123 1.0000 0.0149
-12.000 -1.2583 0.01817 0.01238 -0.0114 1.0000 0.0154
-11.750 -1.2374 0.01768 0.01184 -0.0105 1.0000 0.0160
-11.500 -1.2159 0.01721 0.01134 -0.0096 1.0000 0.0165
-11.250 -1.1940 0.01678 0.01086 -0.0088 1.0000 0.0168
-11.000 -1.1728 0.01627 0.01032 -0.0079 1.0000 0.0175
-10.750 -1.1510 0.01581 0.00984 -0.0071 1.0000 0.0182
-10.500 -1.1288 0.01539 0.00940 -0.0062 1.0000 0.0189
-10.250 -1.1063 0.01501 0.00899 -0.0054 1.0000 0.0196
-10.000 -1.0836 0.01466 0.00860 -0.0046 1.0000 0.0202
-9.750 -1.0617 0.01426 0.00819 -0.0037 1.0000 0.0212
-9.500 -1.0398 0.01389 0.00782 -0.0027 1.0000 0.0223
-9.250 -1.0178 0.01357 0.00748 -0.0016 1.0000 0.0233
-9.000 -0.9958 0.01328 0.00716 -0.0006 1.0000 0.0242
-8.750 -0.9743 0.01294 0.00682 0.0006 1.0000 0.0255
-8.500 -0.9529 0.01263 0.00651 0.0018 1.0000 0.0269
-8.250 -0.9313 0.01236 0.00623 0.0029 1.0000 0.0283
-8.000 -0.9005 0.01203 0.00590 0.0021 0.9984 0.0303
-7.750 -0.8690 0.01171 0.00559 0.0011 0.9965 0.0326
-7.500 -0.8368 0.01143 0.00530 0.0000 0.9948 0.0347
-7.250 -0.8051 0.01112 0.00501 -0.0010 0.9929 0.0379
-7.000 -0.7742 0.01085 0.00475 -0.0017 0.9900 0.0410
-6.750 -0.7427 0.01055 0.00448 -0.0027 0.9870 0.0451
-6.500 -0.7107 0.01029 0.00424 -0.0037 0.9840 0.0492
-6.250 -0.6808 0.01003 0.00400 -0.0042 0.9793 0.0545
-6.000 -0.6509 0.00976 0.00377 -0.0047 0.9739 0.0606
-5.750 -0.6204 0.00952 0.00355 -0.0053 0.9686 0.0672
-5.250 -0.5637 0.00904 0.00315 -0.0055 0.9523 0.0847
-5.000 -0.5365 0.00881 0.00296 -0.0054 0.9419 0.0960
-4.750 -0.5098 0.00859 0.00278 -0.0051 0.9300 0.1079
-4.500 -0.4834 0.00838 0.00260 -0.0047 0.9169 0.1219
-4.250 -0.4572 0.00818 0.00243 -0.0043 0.9023 0.1376
-4.000 -0.4309 0.00800 0.00228 -0.0038 0.8864 0.1545
-3.750 -0.4047 0.00782 0.00212 -0.0034 0.8691 0.1731
-3.500 -0.3784 0.00765 0.00198 -0.0031 0.8504 0.1944
-3.250 -0.3519 0.00750 0.00185 -0.0027 0.8303 0.2158
-3.000 -0.3254 0.00736 0.00173 -0.0023 0.8095 0.2384
-2.750 -0.2987 0.00724 0.00162 -0.0021 0.7881 0.2625
-2.500 -0.2720 0.00712 0.00153 -0.0018 0.7656 0.2864
-2.250 -0.2451 0.00703 0.00144 -0.0015 0.7430 0.3111
-2.000 -0.2182 0.00693 0.00137 -0.0013 0.7204 0.3359
-1.750 -0.1910 0.00687 0.00130 -0.0011 0.6968 0.3603
-1.500 -0.1640 0.00680 0.00125 -0.0009 0.6734 0.3859
-1.000 -0.1095 0.00670 0.00116 -0.0006 0.6261 0.4352
-0.750 -0.0821 0.00667 0.00114 -0.0004 0.6023 0.4588
-0.500 -0.0548 0.00664 0.00112 -0.0003 0.5787 0.4830
-0.250 -0.0274 0.00663 0.00110 -0.0001 0.5554 0.5071
0.000 0.0000 0.00662 0.00110 0.0000 0.5313 0.5314
0.250 0.0274 0.00663 0.00110 0.0001 0.5074 0.5554
0.500 0.0548 0.00664 0.00112 0.0003 0.4831 0.5785
0.750 0.0821 0.00667 0.00114 0.0004 0.4590 0.6023
1.000 0.1096 0.00670 0.00116 0.0006 0.4351 0.6261
1.250 0.1367 0.00675 0.00120 0.0007 0.4103 0.6495
1.500 0.1640 0.00680 0.00125 0.0009 0.3850 0.6733
1.750 0.1911 0.00687 0.00130 0.0011 0.3607 0.6966
2.000 0.2182 0.00693 0.00137 0.0013 0.3357 0.7205
2.250 0.2451 0.00703 0.00144 0.0015 0.3111 0.7429
2.500 0.2720 0.00712 0.00153 0.0018 0.2866 0.7657
2.750 0.2987 0.00724 0.00162 0.0021 0.2622 0.7881
3.000 0.3254 0.00736 0.00173 0.0024 0.2384 0.8097
3.250 0.3519 0.00751 0.00185 0.0027 0.2157 0.8303
3.500 0.3784 0.00765 0.00198 0.0031 0.1946 0.8502
3.750 0.4047 0.00782 0.00212 0.0034 0.1730 0.8690
4.000 0.4309 0.00800 0.00228 0.0038 0.1545 0.8865
4.250 0.4572 0.00818 0.00243 0.0043 0.1373 0.9024
4.500 0.4835 0.00838 0.00260 0.0047 0.1222 0.9169
4.750 0.5098 0.00859 0.00278 0.0050 0.1078 0.9299
5.000 0.5365 0.00881 0.00296 0.0054 0.0959 0.9419
5.250 0.5637 0.00904 0.00315 0.0055 0.0847 0.9524
5.750 0.6204 0.00952 0.00356 0.0053 0.0671 0.9686
6.000 0.6509 0.00976 0.00377 0.0047 0.0606 0.9739
6.250 0.6809 0.01003 0.00400 0.0042 0.0545 0.9794
6.500 0.7108 0.01029 0.00424 0.0036 0.0492 0.9840
6.750 0.7428 0.01055 0.00448 0.0026 0.0451 0.9870
7.000 0.7743 0.01085 0.00475 0.0017 0.0410 0.9900
7.250 0.8051 0.01112 0.00501 0.0010 0.0379 0.9929
7.500 0.8369 0.01143 0.00530 -0.0001 0.0347 0.9948
7.750 0.8691 0.01171 0.00559 -0.0012 0.0326 0.9966
8.000 0.9006 0.01203 0.00590 -0.0021 0.0303 0.9985
8.250 0.9312 0.01236 0.00623 -0.0029 0.0283 1.0000
8.500 0.9528 0.01263 0.00651 -0.0017 0.0269 1.0000
8.750 0.9743 0.01294 0.00682 -0.0006 0.0255 1.0000
9.000 0.9957 0.01328 0.00716 0.0006 0.0242 1.0000
9.250 1.0178 0.01357 0.00748 0.0016 0.0233 1.0000
9.500 1.0398 0.01389 0.00782 0.0027 0.0223 1.0000
9.750 1.0617 0.01426 0.00819 0.0036 0.0212 1.0000
10.000 1.0836 0.01466 0.00860 0.0046 0.0202 1.0000
10.250 1.1063 0.01501 0.00899 0.0054 0.0196 1.0000
10.500 1.1288 0.01539 0.00940 0.0062 0.0189 1.0000
10.750 1.1511 0.01581 0.00984 0.0071 0.0182 1.0000
11.000 1.1729 0.01627 0.01031 0.0079 0.0175 1.0000
11.250 1.1942 0.01678 0.01085 0.0088 0.0168 1.0000
11.500 1.2161 0.01721 0.01134 0.0096 0.0165 1.0000
11.750 1.2375 0.01768 0.01185 0.0104 0.0160 1.0000
12.000 1.2585 0.01817 0.01238 0.0113 0.0154 1.0000
12.250 1.2788 0.01870 0.01294 0.0123 0.0149 1.0000
12.500 1.2982 0.01928 0.01355 0.0133 0.0144 1.0000
12.750 1.3164 0.01993 0.01424 0.0145 0.0140 1.0000
13.000 1.3343 0.02057 0.01494 0.0157 0.0137 1.0000
13.250 1.3519 0.02118 0.01561 0.0169 0.0134 1.0000
13.500 1.3675 0.02183 0.01632 0.0184 0.0132 1.0000
13.750 1.3806 0.02252 0.01708 0.0203 0.0129 1.0000
14.000 1.3928 0.02328 0.01790 0.0221 0.0127 1.0000
14.250 1.4043 0.02412 0.01881 0.0239 0.0124 1.0000
14.500 1.4148 0.02507 0.01982 0.0255 0.0122 1.0000
14.750 1.4241 0.02615 0.02096 0.0271 0.0119 1.0000
15.000 1.4322 0.02739 0.02227 0.0284 0.0117 1.0000
15.250 1.4385 0.02885 0.02381 0.0297 0.0115 1.0000
15.500 1.4424 0.03062 0.02566 0.0306 0.0113 1.0000
15.750 1.4465 0.03252 0.02766 0.0312 0.0111 1.0000
16.000 1.4511 0.03450 0.02973 0.0315 0.0110 1.0000
16.250 1.4540 0.03682 0.03215 0.0314 0.0109 1.0000
16.500 1.4551 0.03948 0.03492 0.0309 0.0107 1.0000
16.750 1.4542 0.04256 0.03811 0.0301 0.0106 1.0000
17.000 1.4508 0.04615 0.04182 0.0287 0.0105 1.0000
17.250 1.4442 0.05033 0.04612 0.0270 0.0104 1.0000
17.500 1.4341 0.05518 0.05110 0.0247 0.0103 1.0000
17.750 1.4197 0.06081 0.05687 0.0219 0.0103 1.0000
18.000 1.4004 0.06732 0.06353 0.0186 0.0102 1.0000
18.250 1.3762 0.07477 0.07113 0.0148 0.0102 1.0000
18.500 1.3466 0.08329 0.07981 0.0104 0.0102 1.0000
18.750 1.3115 0.09292 0.08959 0.0054 0.0102 1.0000
19.000 1.2739 0.10324 0.10008 0.0001 0.0103 1.0000
19.250 1.2349 0.11407 0.11107 -0.0055 0.0103 1.0000
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