N-14 (n14-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: N-14 (n14-il) Reynolds number: 1,000,000 Max Cl/Cd: 71.76 at α=9.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-n14-il-1000000.txt Download as CSV file: xf-n14-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: N-14
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
------ -------- --------- --------- -------- -------- --------
-19.000 -1.1012 0.10667 0.10393 -0.0231 1.0000 0.0126
-18.750 -1.1331 0.09722 0.09435 -0.0282 1.0000 0.0127
-18.500 -1.1672 0.08767 0.08467 -0.0333 1.0000 0.0127
-18.250 -1.1905 0.07997 0.07683 -0.0374 1.0000 0.0127
-18.000 -1.2184 0.07169 0.06840 -0.0419 1.0000 0.0127
-17.750 -1.2405 0.06442 0.06099 -0.0459 1.0000 0.0128
-17.500 -1.2589 0.05805 0.05449 -0.0493 1.0000 0.0129
-17.250 -1.2741 0.05251 0.04883 -0.0521 1.0000 0.0132
-17.000 -1.2864 0.04782 0.04400 -0.0539 1.0000 0.0132
-16.750 -1.2913 0.04436 0.04044 -0.0549 1.0000 0.0134
-16.500 -1.2937 0.04141 0.03739 -0.0555 1.0000 0.0135
-16.250 -1.2860 0.03970 0.03564 -0.0556 1.0000 0.0139
-16.000 -1.2920 0.03674 0.03256 -0.0553 1.0000 0.0140
-15.750 -1.2857 0.03512 0.03087 -0.0549 1.0000 0.0143
-15.500 -1.2769 0.03380 0.02949 -0.0543 1.0000 0.0147
-15.250 -1.2781 0.03171 0.02728 -0.0530 1.0000 0.0149
-15.000 -1.2685 0.03060 0.02610 -0.0521 1.0000 0.0152
-14.750 -1.2632 0.02922 0.02461 -0.0506 1.0000 0.0154
-14.500 -1.2581 0.02790 0.02320 -0.0490 1.0000 0.0158
-14.250 -1.2579 0.02635 0.02157 -0.0466 1.0000 0.0163
-14.000 -1.2501 0.02539 0.02056 -0.0447 1.0000 0.0166
-13.750 -1.2400 0.02461 0.01975 -0.0429 1.0000 0.0170
-13.500 -1.2274 0.02404 0.01914 -0.0411 1.0000 0.0174
-13.250 -1.2161 0.02342 0.01846 -0.0391 1.0000 0.0178
-13.000 -1.2045 0.02284 0.01783 -0.0370 1.0000 0.0183
-12.750 -1.1948 0.02221 0.01712 -0.0345 1.0000 0.0186
-12.500 -1.1806 0.02188 0.01673 -0.0325 1.0000 0.0190
-12.250 -1.1693 0.02144 0.01623 -0.0299 1.0000 0.0193
-12.000 -1.1725 0.02037 0.01510 -0.0250 1.0000 0.0200
-11.750 -1.1668 0.01989 0.01459 -0.0212 1.0000 0.0205
-11.500 -1.1568 0.01958 0.01426 -0.0180 1.0000 0.0209
-11.250 -1.1435 0.01923 0.01389 -0.0155 1.0000 0.0214
-11.000 -1.1304 0.01882 0.01343 -0.0129 1.0000 0.0220
-10.750 -1.1158 0.01850 0.01306 -0.0106 1.0000 0.0226
-10.500 -1.1016 0.01813 0.01264 -0.0082 1.0000 0.0230
-10.250 -1.0847 0.01793 0.01241 -0.0062 1.0000 0.0234
-10.000 -1.0751 0.01724 0.01165 -0.0030 1.0000 0.0239
-9.750 -1.0661 0.01654 0.01091 0.0003 1.0000 0.0248
-9.500 -1.0519 0.01617 0.01054 0.0028 1.0000 0.0255
-9.250 -1.0373 0.01585 0.01019 0.0052 1.0000 0.0260
-9.000 -1.0163 0.01550 0.00982 0.0062 0.9996 0.0267
-8.750 -0.9837 0.01520 0.00949 0.0049 0.9982 0.0277
-8.500 -0.9516 0.01487 0.00912 0.0037 0.9966 0.0283
-8.250 -0.9194 0.01451 0.00872 0.0024 0.9951 0.0289
-8.000 -0.8908 0.01366 0.00783 0.0017 0.9935 0.0303
-7.750 -0.8616 0.01324 0.00740 0.0011 0.9910 0.0314
-7.500 -0.8305 0.01287 0.00701 0.0001 0.9887 0.0324
-7.250 -0.7984 0.01252 0.00664 -0.0010 0.9867 0.0334
-7.000 -0.7651 0.01222 0.00631 -0.0024 0.9851 0.0343
-6.750 -0.7310 0.01192 0.00600 -0.0039 0.9839 0.0350
-6.500 -0.7015 0.01138 0.00542 -0.0045 0.9814 0.0368
-6.250 -0.6733 0.01101 0.00504 -0.0047 0.9773 0.0385
-6.000 -0.6406 0.01069 0.00471 -0.0059 0.9748 0.0404
-5.750 -0.6064 0.01040 0.00441 -0.0074 0.9730 0.0419
-5.500 -0.5723 0.01002 0.00403 -0.0088 0.9714 0.0455
-5.250 -0.5420 0.00967 0.00371 -0.0095 0.9683 0.0507
-5.000 -0.5161 0.00913 0.00343 -0.0093 0.9629 0.0912
-4.750 -0.4814 0.00891 0.00326 -0.0108 0.9601 0.1028
-4.500 -0.4441 0.00876 0.00310 -0.0129 0.9578 0.1079
-4.250 -0.4130 0.00857 0.00290 -0.0136 0.9510 0.1121
-4.000 -0.3790 0.00834 0.00270 -0.0150 0.9451 0.1168
-3.750 -0.3448 0.00816 0.00251 -0.0164 0.9384 0.1204
-3.500 -0.3117 0.00801 0.00234 -0.0176 0.9296 0.1234
-3.250 -0.2815 0.00783 0.00218 -0.0181 0.9204 0.1302
-3.000 -0.2507 0.00768 0.00203 -0.0187 0.9105 0.1364
-2.750 -0.2256 0.00743 0.00187 -0.0182 0.8984 0.1624
-2.500 -0.2042 0.00702 0.00172 -0.0169 0.8864 0.2346
-2.250 -0.1811 0.00675 0.00161 -0.0159 0.8755 0.2863
-2.000 -0.1588 0.00648 0.00149 -0.0148 0.8641 0.3389
-1.750 -0.1376 0.00621 0.00140 -0.0134 0.8529 0.3934
-1.500 -0.1182 0.00584 0.00130 -0.0116 0.8434 0.4723
-1.250 -0.0986 0.00554 0.00123 -0.0099 0.8341 0.5457
-1.000 -0.0779 0.00532 0.00118 -0.0082 0.8239 0.5991
-0.750 -0.0570 0.00516 0.00114 -0.0066 0.8127 0.6464
-0.500 -0.0355 0.00503 0.00113 -0.0051 0.8018 0.6884
-0.250 -0.0127 0.00494 0.00112 -0.0038 0.7910 0.7201
0.000 0.0104 0.00489 0.00112 -0.0026 0.7789 0.7455
0.250 0.0343 0.00488 0.00113 -0.0015 0.7662 0.7672
0.500 0.0582 0.00486 0.00113 -0.0004 0.7514 0.7846
0.750 0.0818 0.00486 0.00114 0.0007 0.7318 0.8015
1.000 0.1042 0.00492 0.00114 0.0021 0.7006 0.8151
1.250 0.1250 0.00505 0.00115 0.0038 0.6559 0.8271
1.500 0.1460 0.00522 0.00119 0.0054 0.6108 0.8390
1.750 0.1664 0.00544 0.00125 0.0071 0.5561 0.8501
2.000 0.1860 0.00573 0.00133 0.0089 0.4913 0.8621
2.250 0.2066 0.00603 0.00144 0.0105 0.4279 0.8749
2.500 0.2288 0.00628 0.00157 0.0118 0.3808 0.8903
2.750 0.2535 0.00648 0.00169 0.0125 0.3488 0.9051
3.000 0.2810 0.00665 0.00183 0.0126 0.3265 0.9177
3.250 0.3084 0.00683 0.00195 0.0128 0.3065 0.9285
3.500 0.3391 0.00702 0.00210 0.0121 0.2864 0.9370
3.750 0.3694 0.00726 0.00225 0.0116 0.2596 0.9445
4.000 0.4007 0.00757 0.00242 0.0107 0.2222 0.9496
4.250 0.4250 0.00794 0.00260 0.0113 0.1787 0.9568
4.500 0.4592 0.00834 0.00286 0.0098 0.1470 0.9592
4.750 0.4944 0.00872 0.00312 0.0080 0.1239 0.9622
5.000 0.5256 0.00907 0.00338 0.0071 0.1004 0.9658
5.250 0.5507 0.00958 0.00368 0.0075 0.0656 0.9709
5.500 0.5848 0.00992 0.00398 0.0061 0.0577 0.9720
5.750 0.6179 0.01030 0.00432 0.0048 0.0527 0.9735
6.000 0.6509 0.01060 0.00464 0.0035 0.0499 0.9752
6.250 0.6830 0.01086 0.00492 0.0025 0.0480 0.9775
6.500 0.7115 0.01116 0.00523 0.0022 0.0458 0.9810
6.750 0.7402 0.01159 0.00566 0.0018 0.0429 0.9836
7.000 0.7737 0.01191 0.00599 0.0004 0.0413 0.9848
7.250 0.8071 0.01214 0.00624 -0.0010 0.0398 0.9861
7.500 0.8395 0.01242 0.00653 -0.0022 0.0382 0.9878
7.750 0.8705 0.01277 0.00688 -0.0031 0.0363 0.9899
8.000 0.8989 0.01330 0.00744 -0.0036 0.0345 0.9924
8.250 0.9299 0.01350 0.00766 -0.0044 0.0333 0.9941
8.500 0.9629 0.01374 0.00791 -0.0058 0.0319 0.9953
8.750 0.9951 0.01404 0.00819 -0.0071 0.0301 0.9968
9.000 1.0249 0.01462 0.00880 -0.0080 0.0284 0.9985
9.250 1.0575 0.01479 0.00900 -0.0092 0.0272 0.9997
9.500 1.0779 0.01502 0.00924 -0.0080 0.0260 1.0000
9.750 1.0926 0.01530 0.00952 -0.0056 0.0250 1.0000
10.000 1.1020 0.01590 0.01014 -0.0023 0.0236 1.0000
10.250 1.1181 0.01612 0.01041 -0.0001 0.0230 1.0000
10.500 1.1333 0.01640 0.01072 0.0022 0.0221 1.0000
10.750 1.1488 0.01667 0.01101 0.0045 0.0211 1.0000
11.000 1.1625 0.01705 0.01139 0.0070 0.0203 1.0000
11.250 1.1707 0.01772 0.01210 0.0104 0.0192 1.0000
11.500 1.1847 0.01806 0.01250 0.0128 0.0187 1.0000
11.750 1.1968 0.01846 0.01293 0.0156 0.0181 1.0000
12.000 1.2045 0.01886 0.01338 0.0192 0.0176 1.0000
12.250 1.2127 0.01928 0.01383 0.0226 0.0170 1.0000
12.500 1.2200 0.01982 0.01440 0.0260 0.0164 1.0000
12.750 1.2223 0.02069 0.01533 0.0299 0.0158 1.0000
13.000 1.2307 0.02137 0.01609 0.0328 0.0155 1.0000
13.250 1.2419 0.02196 0.01674 0.0350 0.0151 1.0000
13.500 1.2519 0.02265 0.01751 0.0373 0.0147 1.0000
13.750 1.2609 0.02345 0.01837 0.0396 0.0144 1.0000
14.000 1.2713 0.02421 0.01918 0.0415 0.0139 1.0000
14.250 1.2800 0.02512 0.02014 0.0434 0.0135 1.0000
14.500 1.2836 0.02642 0.02151 0.0456 0.0132 1.0000
14.750 1.2822 0.02815 0.02333 0.0478 0.0128 1.0000
15.000 1.2794 0.03013 0.02542 0.0498 0.0126 1.0000
15.250 1.2890 0.03127 0.02665 0.0508 0.0123 1.0000
15.500 1.2901 0.03318 0.02867 0.0519 0.0122 1.0000
15.750 1.2922 0.03510 0.03069 0.0527 0.0120 1.0000
16.000 1.2936 0.03723 0.03292 0.0532 0.0118 1.0000
16.250 1.2921 0.03979 0.03559 0.0534 0.0116 1.0000
16.500 1.2873 0.04290 0.03881 0.0530 0.0115 1.0000
16.750 1.2858 0.04588 0.04189 0.0523 0.0113 1.0000
17.000 1.2770 0.04997 0.04611 0.0509 0.0112 1.0000
17.250 1.2672 0.05453 0.05079 0.0490 0.0112 1.0000
17.500 1.2528 0.06009 0.05649 0.0462 0.0111 1.0000
17.750 1.2375 0.06614 0.06266 0.0430 0.0109 1.0000
18.000 1.2174 0.07314 0.06981 0.0392 0.0110 1.0000
18.250 1.1981 0.08006 0.07685 0.0355 0.0109 1.0000
18.500 1.1703 0.08842 0.08535 0.0311 0.0109 1.0000
18.750 1.1398 0.09729 0.09436 0.0265 0.0109 1.0000
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