NACA 0012-64 (naca001264-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 0012-64 (naca001264-il) Reynolds number: 1,000,000 Max Cl/Cd: 67.75 at α=10.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-naca001264-il-1000000-n5.txt Download as CSV file: xf-naca001264-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NACA 0012-64
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
------ -------- --------- --------- -------- -------- --------
-19.750 -1.2592 0.09990 0.09704 -0.0213 1.0000 0.0094
-19.500 -1.3207 0.08465 0.08153 -0.0298 1.0000 0.0091
-19.250 -1.3584 0.07423 0.07089 -0.0357 1.0000 0.0091
-19.000 -1.3837 0.06642 0.06291 -0.0399 1.0000 0.0091
-18.750 -1.4021 0.06021 0.05655 -0.0429 1.0000 0.0092
-18.500 -1.4152 0.05511 0.05131 -0.0450 1.0000 0.0093
-18.250 -1.4247 0.05081 0.04689 -0.0464 1.0000 0.0094
-18.000 -1.4313 0.04716 0.04312 -0.0473 1.0000 0.0096
-17.750 -1.4353 0.04401 0.03986 -0.0477 1.0000 0.0098
-17.500 -1.4372 0.04126 0.03700 -0.0477 1.0000 0.0100
-17.250 -1.4371 0.03884 0.03447 -0.0474 1.0000 0.0102
-17.000 -1.4353 0.03669 0.03222 -0.0468 1.0000 0.0105
-16.750 -1.4318 0.03479 0.03022 -0.0461 1.0000 0.0107
-16.500 -1.4275 0.03305 0.02838 -0.0452 1.0000 0.0109
-16.250 -1.4226 0.03140 0.02666 -0.0441 1.0000 0.0114
-16.000 -1.4158 0.02998 0.02517 -0.0429 1.0000 0.0118
-15.750 -1.4076 0.02871 0.02384 -0.0416 1.0000 0.0122
-15.500 -1.3983 0.02756 0.02262 -0.0403 1.0000 0.0127
-15.250 -1.3881 0.02651 0.02150 -0.0389 1.0000 0.0131
-15.000 -1.3771 0.02554 0.02045 -0.0375 1.0000 0.0135
-14.750 -1.3654 0.02466 0.01949 -0.0360 1.0000 0.0138
-14.500 -1.3531 0.02381 0.01859 -0.0345 1.0000 0.0144
-14.250 -1.3394 0.02308 0.01783 -0.0331 1.0000 0.0149
-14.000 -1.3250 0.02242 0.01713 -0.0316 1.0000 0.0155
-13.750 -1.3100 0.02180 0.01647 -0.0302 1.0000 0.0161
-13.500 -1.2949 0.02123 0.01583 -0.0287 1.0000 0.0166
-13.250 -1.2796 0.02068 0.01523 -0.0271 1.0000 0.0171
-13.000 -1.2646 0.02015 0.01464 -0.0253 1.0000 0.0175
-12.750 -1.2500 0.01963 0.01409 -0.0235 1.0000 0.0181
-12.500 -1.2352 0.01920 0.01364 -0.0215 1.0000 0.0186
-12.250 -1.2217 0.01882 0.01323 -0.0192 1.0000 0.0191
-12.000 -1.2091 0.01847 0.01284 -0.0166 1.0000 0.0195
-11.750 -1.1951 0.01812 0.01246 -0.0142 1.0000 0.0200
-11.500 -1.1811 0.01780 0.01210 -0.0119 1.0000 0.0205
-11.250 -1.1675 0.01751 0.01176 -0.0093 1.0000 0.0209
-11.000 -1.1479 0.01719 0.01140 -0.0081 0.9995 0.0213
-10.750 -1.1208 0.01676 0.01091 -0.0085 0.9981 0.0216
-10.500 -1.0948 0.01618 0.01031 -0.0087 0.9966 0.0224
-10.250 -1.0670 0.01576 0.00987 -0.0093 0.9953 0.0230
-10.000 -1.0382 0.01537 0.00947 -0.0100 0.9942 0.0237
-9.750 -1.0106 0.01501 0.00908 -0.0104 0.9926 0.0242
-9.500 -0.9832 0.01466 0.00870 -0.0107 0.9906 0.0248
-9.250 -0.9549 0.01432 0.00833 -0.0112 0.9888 0.0254
-9.000 -0.9258 0.01399 0.00797 -0.0118 0.9872 0.0259
-8.750 -0.8963 0.01368 0.00762 -0.0125 0.9857 0.0263
-8.500 -0.8670 0.01333 0.00724 -0.0132 0.9843 0.0266
-8.250 -0.8415 0.01287 0.00676 -0.0131 0.9813 0.0275
-8.000 -0.8152 0.01251 0.00639 -0.0130 0.9779 0.0282
-7.750 -0.7877 0.01219 0.00604 -0.0133 0.9751 0.0288
-7.500 -0.7592 0.01188 0.00572 -0.0137 0.9728 0.0294
-7.250 -0.7336 0.01161 0.00544 -0.0134 0.9687 0.0300
-7.000 -0.7078 0.01136 0.00517 -0.0131 0.9644 0.0307
-6.750 -0.6807 0.01111 0.00490 -0.0131 0.9609 0.0314
-6.500 -0.6546 0.01088 0.00465 -0.0129 0.9569 0.0319
-6.250 -0.6292 0.01067 0.00442 -0.0125 0.9518 0.0323
-6.000 -0.6035 0.01041 0.00415 -0.0121 0.9471 0.0336
-5.750 -0.5777 0.01018 0.00391 -0.0118 0.9427 0.0351
-5.500 -0.5523 0.00997 0.00371 -0.0114 0.9371 0.0366
-5.250 -0.5262 0.00978 0.00351 -0.0110 0.9320 0.0383
-5.000 -0.5002 0.00958 0.00331 -0.0107 0.9270 0.0415
-4.750 -0.4746 0.00937 0.00313 -0.0103 0.9209 0.0469
-4.500 -0.4489 0.00915 0.00294 -0.0099 0.9151 0.0562
-4.250 -0.4230 0.00895 0.00279 -0.0096 0.9094 0.0664
-4.000 -0.3970 0.00876 0.00263 -0.0093 0.9028 0.0756
-3.750 -0.3706 0.00860 0.00248 -0.0090 0.8969 0.0841
-3.500 -0.3442 0.00843 0.00235 -0.0088 0.8901 0.0944
-3.250 -0.3182 0.00824 0.00221 -0.0084 0.8833 0.1101
-3.000 -0.2924 0.00803 0.00208 -0.0081 0.8764 0.1324
-2.750 -0.2665 0.00782 0.00195 -0.0078 0.8689 0.1572
-2.500 -0.2410 0.00758 0.00183 -0.0074 0.8618 0.1913
-2.250 -0.2160 0.00730 0.00171 -0.0069 0.8538 0.2342
-2.000 -0.1916 0.00698 0.00157 -0.0063 0.8462 0.2911
-1.750 -0.1682 0.00658 0.00144 -0.0056 0.8377 0.3647
-1.500 -0.1445 0.00623 0.00132 -0.0049 0.8296 0.4357
-1.250 -0.1207 0.00591 0.00123 -0.0041 0.8208 0.5026
-1.000 -0.0968 0.00563 0.00115 -0.0033 0.8110 0.5658
-0.750 -0.0729 0.00542 0.00110 -0.0025 0.7973 0.6191
-0.500 -0.0485 0.00529 0.00106 -0.0017 0.7789 0.6616
0.000 0.0000 0.00521 0.00102 0.0000 0.7268 0.7267
0.500 0.0485 0.00529 0.00106 0.0017 0.6611 0.7788
0.750 0.0730 0.00542 0.00110 0.0025 0.6196 0.7974
1.000 0.0969 0.00562 0.00115 0.0033 0.5666 0.8110
1.250 0.1205 0.00593 0.00123 0.0041 0.4994 0.8208
1.500 0.1446 0.00623 0.00132 0.0048 0.4367 0.8296
1.750 0.1683 0.00658 0.00144 0.0055 0.3653 0.8377
2.000 0.1916 0.00698 0.00158 0.0063 0.2899 0.8462
2.250 0.2162 0.00730 0.00170 0.0069 0.2350 0.8538
2.500 0.2411 0.00758 0.00183 0.0073 0.1909 0.8617
2.750 0.2666 0.00782 0.00195 0.0077 0.1568 0.8689
3.000 0.2925 0.00803 0.00208 0.0081 0.1325 0.8763
3.250 0.3184 0.00824 0.00221 0.0084 0.1101 0.8833
3.500 0.3444 0.00843 0.00235 0.0087 0.0944 0.8901
3.750 0.3707 0.00860 0.00248 0.0090 0.0842 0.8969
4.000 0.3971 0.00876 0.00263 0.0093 0.0756 0.9028
4.250 0.4231 0.00895 0.00279 0.0096 0.0665 0.9094
4.500 0.4490 0.00915 0.00294 0.0099 0.0562 0.9151
4.750 0.4747 0.00938 0.00313 0.0103 0.0469 0.9209
5.000 0.5003 0.00959 0.00331 0.0107 0.0415 0.9269
5.250 0.5264 0.00978 0.00351 0.0110 0.0383 0.9319
5.500 0.5524 0.00997 0.00371 0.0113 0.0366 0.9371
5.750 0.5778 0.01018 0.00392 0.0117 0.0351 0.9427
6.000 0.6036 0.01041 0.00415 0.0121 0.0336 0.9471
6.250 0.6294 0.01067 0.00442 0.0124 0.0323 0.9517
6.500 0.6547 0.01088 0.00465 0.0128 0.0319 0.9569
6.750 0.6809 0.01111 0.00490 0.0131 0.0314 0.9609
7.000 0.7080 0.01136 0.00518 0.0131 0.0307 0.9644
7.250 0.7338 0.01161 0.00544 0.0133 0.0300 0.9687
7.500 0.7593 0.01188 0.00572 0.0136 0.0294 0.9727
7.750 0.7878 0.01219 0.00604 0.0132 0.0288 0.9751
8.000 0.8153 0.01251 0.00639 0.0130 0.0282 0.9779
8.250 0.8415 0.01287 0.00676 0.0131 0.0275 0.9813
8.500 0.8670 0.01333 0.00724 0.0132 0.0266 0.9843
8.750 0.8963 0.01368 0.00762 0.0125 0.0263 0.9857
9.000 0.9259 0.01399 0.00797 0.0118 0.0259 0.9873
9.250 0.9550 0.01431 0.00833 0.0112 0.0254 0.9888
9.500 0.9833 0.01466 0.00870 0.0106 0.0248 0.9907
9.750 1.0108 0.01501 0.00907 0.0103 0.0242 0.9927
10.000 1.0383 0.01537 0.00947 0.0099 0.0237 0.9942
10.250 1.0671 0.01575 0.00987 0.0093 0.0230 0.9953
10.500 1.0949 0.01618 0.01031 0.0087 0.0223 0.9966
10.750 1.1210 0.01675 0.01091 0.0085 0.0216 0.9981
11.000 1.1481 0.01718 0.01139 0.0081 0.0213 0.9995
11.250 1.1674 0.01751 0.01176 0.0094 0.0209 1.0000
11.500 1.1811 0.01780 0.01210 0.0119 0.0205 1.0000
11.750 1.1951 0.01812 0.01246 0.0142 0.0200 1.0000
12.000 1.2093 0.01846 0.01284 0.0165 0.0195 1.0000
12.250 1.2220 0.01882 0.01323 0.0191 0.0191 1.0000
12.500 1.2357 0.01920 0.01364 0.0214 0.0186 1.0000
12.750 1.2505 0.01963 0.01409 0.0234 0.0181 1.0000
13.000 1.2652 0.02015 0.01464 0.0252 0.0175 1.0000
13.250 1.2803 0.02068 0.01522 0.0269 0.0171 1.0000
13.500 1.2958 0.02122 0.01582 0.0285 0.0166 1.0000
13.750 1.3110 0.02179 0.01646 0.0300 0.0160 1.0000
14.000 1.3260 0.02241 0.01712 0.0315 0.0155 1.0000
14.250 1.3404 0.02307 0.01782 0.0329 0.0149 1.0000
14.500 1.3542 0.02380 0.01859 0.0343 0.0143 1.0000
14.750 1.3665 0.02465 0.01948 0.0358 0.0138 1.0000
15.000 1.3784 0.02554 0.02044 0.0373 0.0135 1.0000
15.250 1.3894 0.02650 0.02149 0.0387 0.0131 1.0000
15.500 1.3997 0.02755 0.02261 0.0401 0.0127 1.0000
15.750 1.4091 0.02870 0.02382 0.0414 0.0122 1.0000
16.000 1.4174 0.02996 0.02515 0.0426 0.0118 1.0000
16.250 1.4243 0.03138 0.02664 0.0438 0.0114 1.0000
16.500 1.4294 0.03302 0.02836 0.0448 0.0110 1.0000
16.750 1.4338 0.03477 0.03020 0.0458 0.0107 1.0000
17.000 1.4374 0.03666 0.03219 0.0465 0.0105 1.0000
17.250 1.4393 0.03880 0.03443 0.0470 0.0102 1.0000
17.500 1.4395 0.04121 0.03695 0.0473 0.0100 1.0000
17.750 1.4377 0.04396 0.03981 0.0473 0.0098 1.0000
18.000 1.4339 0.04710 0.04306 0.0469 0.0096 1.0000
18.250 1.4273 0.05075 0.04682 0.0461 0.0094 1.0000
18.500 1.4180 0.05502 0.05123 0.0446 0.0093 1.0000
18.750 1.4049 0.06013 0.05647 0.0425 0.0092 1.0000
19.000 1.3867 0.06634 0.06283 0.0395 0.0091 1.0000
19.250 1.3615 0.07414 0.07081 0.0352 0.0091 1.0000
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