N-12 (n12-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: N-12 (n12-il) Reynolds number: 1,000,000 Max Cl/Cd: 73.73 at α=9° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-n12-il-1000000-n5.txt Download as CSV file: xf-n12-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: N-12
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
------ -------- --------- --------- -------- -------- --------
-18.500 -1.0807 0.11303 0.11069 -0.0093 1.0000 0.0060
-18.250 -1.1361 0.09825 0.09571 -0.0171 1.0000 0.0058
-18.000 -1.1754 0.08706 0.08436 -0.0232 1.0000 0.0058
-17.750 -1.2157 0.07623 0.07334 -0.0293 1.0000 0.0057
-17.500 -1.2430 0.06798 0.06492 -0.0339 1.0000 0.0056
-17.250 -1.2665 0.06047 0.05725 -0.0382 1.0000 0.0056
-17.000 -1.2845 0.05408 0.05070 -0.0418 1.0000 0.0056
-16.750 -1.2969 0.04902 0.04551 -0.0443 1.0000 0.0057
-16.500 -1.3079 0.04458 0.04093 -0.0461 1.0000 0.0057
-16.250 -1.3158 0.04093 0.03716 -0.0470 1.0000 0.0058
-16.000 -1.3188 0.03813 0.03426 -0.0471 1.0000 0.0060
-15.750 -1.3213 0.03561 0.03163 -0.0468 1.0000 0.0061
-15.500 -1.3239 0.03328 0.02919 -0.0459 1.0000 0.0062
-15.250 -1.3233 0.03142 0.02722 -0.0447 1.0000 0.0064
-15.000 -1.3203 0.02989 0.02560 -0.0432 1.0000 0.0065
-14.750 -1.3178 0.02842 0.02403 -0.0413 1.0000 0.0068
-14.500 -1.3136 0.02717 0.02268 -0.0393 1.0000 0.0069
-14.250 -1.3089 0.02603 0.02144 -0.0369 1.0000 0.0071
-14.000 -1.3031 0.02506 0.02037 -0.0345 1.0000 0.0072
-13.750 -1.2967 0.02417 0.01940 -0.0318 1.0000 0.0073
-13.500 -1.2904 0.02336 0.01849 -0.0288 1.0000 0.0074
-13.250 -1.2851 0.02256 0.01763 -0.0256 1.0000 0.0077
-13.000 -1.2791 0.02188 0.01689 -0.0221 1.0000 0.0081
-12.750 -1.2711 0.02123 0.01618 -0.0190 1.0000 0.0083
-12.500 -1.2586 0.02058 0.01547 -0.0166 1.0000 0.0086
-12.250 -1.2449 0.01997 0.01481 -0.0145 1.0000 0.0090
-12.000 -1.2306 0.01939 0.01416 -0.0123 1.0000 0.0094
-11.750 -1.2158 0.01882 0.01352 -0.0102 1.0000 0.0098
-11.500 -1.2000 0.01828 0.01292 -0.0083 1.0000 0.0102
-11.250 -1.1828 0.01783 0.01245 -0.0066 1.0000 0.0109
-11.000 -1.1641 0.01747 0.01208 -0.0051 1.0000 0.0117
-10.750 -1.1459 0.01707 0.01164 -0.0035 1.0000 0.0123
-10.500 -1.1275 0.01666 0.01119 -0.0018 1.0000 0.0128
-10.250 -1.1092 0.01624 0.01072 -0.0002 1.0000 0.0133
-10.000 -1.0890 0.01595 0.01041 0.0011 1.0000 0.0140
-9.750 -1.0678 0.01574 0.01022 0.0023 1.0000 0.0147
-9.500 -1.0461 0.01557 0.01004 0.0034 1.0000 0.0154
-9.250 -1.0249 0.01535 0.00981 0.0046 1.0000 0.0161
-9.000 -1.0045 0.01507 0.00949 0.0059 1.0000 0.0167
-8.750 -0.9847 0.01473 0.00911 0.0074 1.0000 0.0171
-8.500 -0.9632 0.01455 0.00888 0.0086 1.0000 0.0175
-8.250 -0.9427 0.01412 0.00842 0.0098 0.9999 0.0180
-8.000 -0.9123 0.01383 0.00814 0.0090 0.9989 0.0187
-7.750 -0.8816 0.01358 0.00788 0.0081 0.9977 0.0192
-7.500 -0.8501 0.01339 0.00768 0.0071 0.9964 0.0199
-7.250 -0.8186 0.01314 0.00741 0.0061 0.9950 0.0206
-7.000 -0.7873 0.01284 0.00710 0.0051 0.9935 0.0212
-6.750 -0.7558 0.01252 0.00675 0.0041 0.9908 0.0219
-6.500 -0.7219 0.01224 0.00645 0.0026 0.9879 0.0224
-6.250 -0.6877 0.01197 0.00616 0.0011 0.9857 0.0228
-6.000 -0.6602 0.01166 0.00583 0.0010 0.9817 0.0230
-5.750 -0.6315 0.01139 0.00554 0.0007 0.9773 0.0232
-5.500 -0.6065 0.01085 0.00496 0.0012 0.9718 0.0239
-5.000 -0.5570 0.01009 0.00414 0.0024 0.9517 0.0248
-4.750 -0.5200 0.00971 0.00374 0.0003 0.9404 0.0254
-4.500 -0.4739 0.00937 0.00338 -0.0039 0.9322 0.0263
-4.250 -0.4217 0.00907 0.00307 -0.0095 0.9245 0.0271
-4.000 -0.3692 0.00880 0.00274 -0.0152 0.9103 0.0280
-3.750 -0.3288 0.00868 0.00249 -0.0180 0.8794 0.0286
-3.500 -0.3028 0.00863 0.00233 -0.0176 0.8516 0.0289
-3.250 -0.2791 0.00858 0.00218 -0.0166 0.8245 0.0293
-3.000 -0.2555 0.00853 0.00205 -0.0156 0.8017 0.0297
-2.750 -0.2318 0.00848 0.00192 -0.0146 0.7793 0.0301
-2.500 -0.2090 0.00847 0.00180 -0.0134 0.7483 0.0304
-2.250 -0.1869 0.00851 0.00169 -0.0121 0.7076 0.0307
-2.000 -0.1659 0.00861 0.00159 -0.0105 0.6515 0.0321
-1.750 -0.1433 0.00868 0.00151 -0.0094 0.6088 0.0341
-1.500 -0.1193 0.00867 0.00144 -0.0085 0.5823 0.0386
-1.250 -0.0976 0.00845 0.00133 -0.0073 0.5563 0.0991
-1.000 -0.0737 0.00844 0.00128 -0.0065 0.5289 0.1115
-0.750 -0.0497 0.00842 0.00124 -0.0056 0.5009 0.1268
-0.500 -0.0273 0.00833 0.00118 -0.0045 0.4692 0.1648
-0.250 -0.0124 0.00773 0.00106 -0.0021 0.4355 0.3333
0.000 0.0070 0.00795 0.00109 -0.0005 0.3482 0.3709
0.250 0.0296 0.00805 0.00112 0.0005 0.3046 0.3950
0.500 0.0525 0.00803 0.00112 0.0015 0.2797 0.4293
0.750 0.0749 0.00792 0.00112 0.0026 0.2627 0.4764
1.000 0.0955 0.00771 0.00112 0.0041 0.2478 0.5523
1.250 0.1152 0.00750 0.00115 0.0058 0.2353 0.6343
1.500 0.1361 0.00736 0.00118 0.0074 0.2265 0.6947
1.750 0.1582 0.00731 0.00123 0.0087 0.2163 0.7323
2.000 0.1815 0.00734 0.00130 0.0097 0.2015 0.7567
2.250 0.2019 0.00755 0.00140 0.0113 0.1423 0.7855
2.500 0.2225 0.00771 0.00156 0.0129 0.1124 0.8186
2.750 0.2463 0.00779 0.00167 0.0139 0.1045 0.8414
3.000 0.2715 0.00785 0.00177 0.0145 0.0999 0.8563
3.250 0.2969 0.00796 0.00188 0.0151 0.0934 0.8676
3.500 0.3226 0.00806 0.00199 0.0156 0.0807 0.8802
3.750 0.3468 0.00839 0.00217 0.0162 0.0417 0.8935
4.000 0.3808 0.00853 0.00237 0.0148 0.0365 0.9140
4.250 0.4220 0.00871 0.00259 0.0118 0.0342 0.9267
4.500 0.4622 0.00892 0.00282 0.0089 0.0332 0.9346
4.750 0.5041 0.00914 0.00306 0.0057 0.0321 0.9392
5.000 0.5441 0.00939 0.00332 0.0029 0.0308 0.9451
5.250 0.5792 0.00966 0.00359 0.0011 0.0297 0.9509
5.500 0.6113 0.00994 0.00389 0.0001 0.0286 0.9562
6.000 0.6661 0.01061 0.00462 0.0002 0.0262 0.9699
6.250 0.6925 0.01084 0.00486 0.0004 0.0259 0.9757
6.500 0.7227 0.01107 0.00511 -0.0002 0.0254 0.9791
6.750 0.7489 0.01133 0.00539 0.0000 0.0248 0.9841
7.000 0.7811 0.01159 0.00567 -0.0011 0.0238 0.9865
7.250 0.8126 0.01185 0.00595 -0.0021 0.0228 0.9885
7.500 0.8428 0.01212 0.00622 -0.0028 0.0217 0.9908
7.750 0.8713 0.01244 0.00655 -0.0032 0.0207 0.9929
8.000 0.8992 0.01285 0.00699 -0.0035 0.0196 0.9947
8.250 0.9303 0.01307 0.00723 -0.0044 0.0190 0.9960
8.500 0.9618 0.01333 0.00753 -0.0055 0.0180 0.9975
8.750 0.9940 0.01359 0.00779 -0.0067 0.0166 0.9990
9.000 1.0248 0.01390 0.00807 -0.0077 0.0153 1.0000
9.250 1.0435 0.01424 0.00844 -0.0060 0.0145 1.0000
9.500 1.0625 0.01457 0.00881 -0.0044 0.0137 1.0000
9.750 1.0813 0.01492 0.00919 -0.0028 0.0130 1.0000
10.000 1.0999 0.01528 0.00955 -0.0012 0.0119 1.0000
10.250 1.1175 0.01572 0.01000 0.0006 0.0109 1.0000
10.500 1.1352 0.01614 0.01047 0.0024 0.0105 1.0000
10.750 1.1523 0.01659 0.01098 0.0043 0.0101 1.0000
11.000 1.1692 0.01705 0.01148 0.0061 0.0096 1.0000
11.250 1.1853 0.01754 0.01202 0.0081 0.0091 1.0000
11.500 1.2007 0.01808 0.01260 0.0101 0.0088 1.0000
11.750 1.2148 0.01868 0.01325 0.0123 0.0083 1.0000
12.000 1.2285 0.01928 0.01392 0.0146 0.0080 1.0000
12.250 1.2420 0.01987 0.01458 0.0169 0.0078 1.0000
12.500 1.2550 0.02048 0.01526 0.0192 0.0075 1.0000
12.750 1.2650 0.02111 0.01596 0.0220 0.0074 1.0000
13.000 1.2721 0.02171 0.01663 0.0253 0.0071 1.0000
13.250 1.2791 0.02238 0.01737 0.0285 0.0070 1.0000
13.500 1.2864 0.02313 0.01819 0.0314 0.0067 1.0000
13.750 1.2934 0.02396 0.01910 0.0341 0.0066 1.0000
14.000 1.2999 0.02489 0.02010 0.0366 0.0063 1.0000
14.250 1.3044 0.02603 0.02132 0.0390 0.0063 1.0000
14.500 1.3066 0.02741 0.02279 0.0412 0.0060 1.0000
14.750 1.3072 0.02903 0.02452 0.0432 0.0058 1.0000
15.000 1.3108 0.03053 0.02613 0.0446 0.0057 1.0000
15.250 1.3130 0.03230 0.02800 0.0457 0.0057 1.0000
15.500 1.3138 0.03433 0.03013 0.0465 0.0056 1.0000
15.750 1.3138 0.03662 0.03254 0.0468 0.0055 1.0000
16.000 1.3106 0.03947 0.03551 0.0466 0.0054 1.0000
16.250 1.3072 0.04258 0.03874 0.0459 0.0054 1.0000
16.500 1.2988 0.04661 0.04290 0.0444 0.0053 1.0000
16.750 1.2898 0.05103 0.04746 0.0424 0.0053 1.0000
17.000 1.2730 0.05691 0.05350 0.0393 0.0053 1.0000
17.250 1.2523 0.06375 0.06050 0.0355 0.0053 1.0000
17.500 1.2329 0.07066 0.06754 0.0317 0.0052 1.0000
17.750 1.1987 0.08031 0.07736 0.0263 0.0053 1.0000
18.000 1.1696 0.08914 0.08634 0.0216 0.0053 1.0000
18.250 1.1258 0.10080 0.09816 0.0153 0.0054 1.0000
18.500 1.0848 0.11244 0.10995 0.0091 0.0054 1.0000
18.750 1.0327 0.12709 0.12478 0.0016 0.0056 1.0000
19.000 0.9678 0.14559 0.14344 -0.0080 0.0057 1.0000
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