N-14 (n14-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: N-14 (n14-il) Reynolds number: 1,000,000 Max Cl/Cd: 73.17 at α=10° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-n14-il-1000000-n5.txt Download as CSV file: xf-n14-il-1000000-n5.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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.500 -1.1134 0.11322 0.11047 -0.0194 1.0000 0.0082
-19.250 -1.1672 0.09971 0.09676 -0.0266 1.0000 0.0079
-19.000 -1.2174 0.08729 0.08416 -0.0332 1.0000 0.0078
-18.750 -1.2587 0.07652 0.07319 -0.0391 1.0000 0.0077
-18.500 -1.2912 0.06742 0.06391 -0.0442 1.0000 0.0078
-18.250 -1.3125 0.06047 0.05679 -0.0481 1.0000 0.0077
-18.000 -1.3299 0.05453 0.05071 -0.0511 1.0000 0.0077
-17.750 -1.3418 0.04977 0.04581 -0.0531 1.0000 0.0078
-17.500 -1.3514 0.04567 0.04160 -0.0545 1.0000 0.0080
-17.250 -1.3574 0.04229 0.03811 -0.0552 1.0000 0.0081
-17.000 -1.3612 0.03938 0.03508 -0.0554 1.0000 0.0081
-16.750 -1.3620 0.03698 0.03257 -0.0552 1.0000 0.0084
-16.500 -1.3627 0.03471 0.03021 -0.0546 1.0000 0.0086
-16.250 -1.3609 0.03282 0.02821 -0.0537 1.0000 0.0088
-16.000 -1.3579 0.03112 0.02642 -0.0526 1.0000 0.0089
-15.750 -1.3534 0.02965 0.02486 -0.0513 1.0000 0.0092
-15.500 -1.3501 0.02815 0.02328 -0.0497 1.0000 0.0095
-15.250 -1.3450 0.02685 0.02192 -0.0480 1.0000 0.0099
-15.000 -1.3386 0.02571 0.02071 -0.0462 1.0000 0.0102
-14.750 -1.3312 0.02469 0.01963 -0.0443 1.0000 0.0105
-14.500 -1.3227 0.02380 0.01867 -0.0423 1.0000 0.0110
-14.250 -1.3137 0.02297 0.01777 -0.0401 1.0000 0.0114
-14.000 -1.3041 0.02222 0.01695 -0.0379 1.0000 0.0118
-13.750 -1.2943 0.02152 0.01620 -0.0356 1.0000 0.0124
-13.500 -1.2841 0.02088 0.01553 -0.0332 1.0000 0.0130
-13.250 -1.2737 0.02030 0.01491 -0.0307 1.0000 0.0136
-13.000 -1.2630 0.01980 0.01438 -0.0281 1.0000 0.0144
-12.750 -1.2530 0.01934 0.01386 -0.0252 1.0000 0.0149
-12.500 -1.2438 0.01891 0.01338 -0.0220 1.0000 0.0154
-12.250 -1.2348 0.01852 0.01297 -0.0187 1.0000 0.0162
-12.000 -1.2240 0.01815 0.01258 -0.0157 1.0000 0.0169
-11.750 -1.2103 0.01776 0.01217 -0.0133 1.0000 0.0176
-11.500 -1.1960 0.01740 0.01177 -0.0110 1.0000 0.0183
-11.250 -1.1810 0.01707 0.01140 -0.0087 1.0000 0.0189
-11.000 -1.1657 0.01674 0.01102 -0.0065 1.0000 0.0193
-10.750 -1.1515 0.01634 0.01060 -0.0041 1.0000 0.0202
-10.500 -1.1266 0.01596 0.01021 -0.0039 0.9993 0.0209
-10.250 -1.0979 0.01560 0.00984 -0.0045 0.9982 0.0218
-10.000 -1.0692 0.01527 0.00948 -0.0051 0.9969 0.0226
-9.750 -1.0403 0.01496 0.00913 -0.0057 0.9955 0.0233
-9.500 -1.0109 0.01465 0.00879 -0.0064 0.9942 0.0238
-9.250 -0.9835 0.01435 0.00846 -0.0066 0.9925 0.0242
-9.000 -0.9573 0.01387 0.00794 -0.0067 0.9903 0.0251
-8.750 -0.9292 0.01346 0.00753 -0.0071 0.9882 0.0260
-8.500 -0.8999 0.01311 0.00715 -0.0077 0.9864 0.0267
-8.250 -0.8697 0.01280 0.00684 -0.0085 0.9850 0.0276
-8.000 -0.8403 0.01250 0.00653 -0.0090 0.9833 0.0283
-7.750 -0.8151 0.01222 0.00622 -0.0087 0.9794 0.0290
-7.500 -0.7859 0.01196 0.00593 -0.0091 0.9767 0.0296
-7.250 -0.7556 0.01168 0.00563 -0.0098 0.9746 0.0300
-7.000 -0.7249 0.01135 0.00528 -0.0106 0.9729 0.0306
-6.750 -0.7016 0.01104 0.00494 -0.0098 0.9669 0.0316
-6.500 -0.6722 0.01073 0.00463 -0.0102 0.9633 0.0326
-6.000 -0.6105 0.01020 0.00410 -0.0118 0.9549 0.0350
-5.750 -0.5758 0.00994 0.00383 -0.0135 0.9502 0.0363
-5.500 -0.5386 0.00970 0.00358 -0.0156 0.9461 0.0375
-5.250 -0.5065 0.00944 0.00332 -0.0167 0.9378 0.0410
-5.000 -0.4707 0.00918 0.00307 -0.0186 0.9306 0.0452
-4.750 -0.4379 0.00890 0.00280 -0.0198 0.9173 0.0556
-4.500 -0.4091 0.00859 0.00262 -0.0201 0.9024 0.0881
-4.250 -0.3814 0.00846 0.00249 -0.0201 0.8873 0.0960
-4.000 -0.3549 0.00839 0.00237 -0.0198 0.8741 0.0997
-3.750 -0.3287 0.00834 0.00227 -0.0194 0.8628 0.1013
-3.500 -0.3031 0.00829 0.00217 -0.0188 0.8514 0.1028
-3.250 -0.2782 0.00821 0.00206 -0.0182 0.8402 0.1054
-3.000 -0.2530 0.00813 0.00196 -0.0176 0.8309 0.1079
-2.500 -0.2028 0.00799 0.00179 -0.0163 0.8116 0.1133
-2.250 -0.1778 0.00794 0.00171 -0.0156 0.8000 0.1156
-2.000 -0.1530 0.00790 0.00164 -0.0148 0.7868 0.1184
-1.750 -0.1291 0.00782 0.00155 -0.0139 0.7712 0.1267
-1.500 -0.1057 0.00771 0.00146 -0.0129 0.7550 0.1424
-1.250 -0.0854 0.00737 0.00135 -0.0114 0.7412 0.2131
-1.000 -0.0620 0.00726 0.00129 -0.0104 0.7240 0.2401
-0.750 -0.0396 0.00720 0.00123 -0.0092 0.6969 0.2662
-0.500 -0.0178 0.00713 0.00119 -0.0079 0.6688 0.2976
-0.250 0.0038 0.00710 0.00115 -0.0066 0.6374 0.3256
0.000 0.0254 0.00707 0.00113 -0.0052 0.6071 0.3573
0.250 0.0449 0.00705 0.00112 -0.0035 0.5643 0.4026
0.500 0.0645 0.00704 0.00112 -0.0018 0.5193 0.4490
0.750 0.0814 0.00714 0.00114 0.0004 0.4477 0.5032
1.000 0.0991 0.00726 0.00119 0.0024 0.3830 0.5511
1.250 0.1188 0.00730 0.00123 0.0041 0.3435 0.5956
1.500 0.1398 0.00727 0.00127 0.0055 0.3217 0.6386
1.750 0.1610 0.00725 0.00131 0.0070 0.3023 0.6798
2.000 0.1828 0.00725 0.00137 0.0083 0.2845 0.7133
2.250 0.2040 0.00723 0.00144 0.0099 0.2698 0.7540
2.500 0.2259 0.00724 0.00152 0.0112 0.2540 0.7859
2.750 0.2474 0.00734 0.00161 0.0126 0.2260 0.8124
3.000 0.2685 0.00754 0.00173 0.0141 0.1880 0.8336
3.250 0.2906 0.00774 0.00186 0.0153 0.1590 0.8510
3.500 0.3143 0.00789 0.00199 0.0162 0.1404 0.8646
3.750 0.3391 0.00803 0.00212 0.0169 0.1283 0.8760
4.000 0.3643 0.00818 0.00226 0.0175 0.1166 0.8889
4.250 0.3903 0.00833 0.00241 0.0178 0.1049 0.9016
4.500 0.4172 0.00854 0.00257 0.0180 0.0876 0.9136
4.750 0.4454 0.00888 0.00280 0.0178 0.0608 0.9230
5.000 0.4753 0.00911 0.00302 0.0172 0.0541 0.9322
5.250 0.5099 0.00931 0.00324 0.0157 0.0514 0.9396
5.500 0.5454 0.00956 0.00349 0.0139 0.0487 0.9485
5.750 0.5803 0.00983 0.00376 0.0122 0.0461 0.9535
6.000 0.6085 0.01010 0.00403 0.0120 0.0433 0.9593
6.250 0.6419 0.01031 0.00425 0.0107 0.0424 0.9616
6.500 0.6746 0.01054 0.00450 0.0095 0.0412 0.9638
6.750 0.7045 0.01078 0.00475 0.0089 0.0399 0.9669
7.000 0.7283 0.01103 0.00499 0.0097 0.0382 0.9727
7.250 0.7591 0.01135 0.00530 0.0088 0.0360 0.9741
7.500 0.7894 0.01164 0.00561 0.0081 0.0347 0.9760
7.750 0.8191 0.01189 0.00587 0.0075 0.0338 0.9782
8.000 0.8469 0.01214 0.00614 0.0074 0.0326 0.9812
8.250 0.8728 0.01241 0.00642 0.0076 0.0313 0.9843
8.500 0.9031 0.01273 0.00673 0.0068 0.0298 0.9856
8.750 0.9328 0.01307 0.00708 0.0061 0.0283 0.9872
9.000 0.9621 0.01334 0.00738 0.0055 0.0273 0.9890
9.250 0.9904 0.01364 0.00769 0.0051 0.0257 0.9910
9.500 1.0174 0.01398 0.00803 0.0049 0.0242 0.9930
9.750 1.0451 0.01434 0.00840 0.0046 0.0227 0.9946
10.000 1.0741 0.01468 0.00877 0.0040 0.0213 0.9961
10.250 1.1023 0.01507 0.00915 0.0035 0.0193 0.9975
10.500 1.1303 0.01549 0.00959 0.0029 0.0178 0.9989
10.750 1.1581 0.01594 0.01006 0.0024 0.0161 0.9999
11.250 1.1866 0.01677 0.01092 0.0072 0.0140 1.0000
11.500 1.1997 0.01718 0.01138 0.0098 0.0133 1.0000
11.750 1.2119 0.01764 0.01187 0.0125 0.0126 1.0000
12.000 1.2225 0.01812 0.01238 0.0155 0.0119 1.0000
12.250 1.2293 0.01858 0.01288 0.0192 0.0114 1.0000
12.500 1.2371 0.01903 0.01338 0.0227 0.0110 1.0000
12.750 1.2463 0.01950 0.01391 0.0258 0.0107 1.0000
13.000 1.2556 0.02005 0.01451 0.0287 0.0103 1.0000
13.250 1.2654 0.02064 0.01516 0.0313 0.0100 1.0000
13.500 1.2748 0.02131 0.01587 0.0339 0.0096 1.0000
13.750 1.2838 0.02205 0.01667 0.0363 0.0093 1.0000
14.000 1.2919 0.02290 0.01758 0.0387 0.0090 1.0000
14.250 1.2991 0.02384 0.01859 0.0410 0.0086 1.0000
14.500 1.3083 0.02471 0.01952 0.0430 0.0083 1.0000
14.750 1.3162 0.02570 0.02060 0.0448 0.0082 1.0000
15.000 1.3231 0.02682 0.02179 0.0466 0.0081 1.0000
15.250 1.3291 0.02806 0.02312 0.0482 0.0080 1.0000
15.500 1.3350 0.02937 0.02452 0.0496 0.0077 1.0000
15.750 1.3386 0.03095 0.02618 0.0510 0.0075 1.0000
16.000 1.3410 0.03271 0.02803 0.0521 0.0074 1.0000
16.250 1.3427 0.03464 0.03005 0.0529 0.0073 1.0000
16.500 1.3424 0.03688 0.03238 0.0535 0.0071 1.0000
16.750 1.3406 0.03941 0.03501 0.0537 0.0070 1.0000
17.000 1.3357 0.04249 0.03819 0.0534 0.0069 1.0000
17.250 1.3283 0.04610 0.04192 0.0526 0.0067 1.0000
17.500 1.3179 0.05038 0.04633 0.0511 0.0067 1.0000
17.750 1.3038 0.05557 0.05165 0.0488 0.0065 1.0000
18.000 1.2872 0.06150 0.05772 0.0457 0.0065 1.0000
18.250 1.2659 0.06859 0.06498 0.0418 0.0065 1.0000
18.500 1.2386 0.07686 0.07341 0.0373 0.0066 1.0000
18.750 1.2023 0.08670 0.08343 0.0320 0.0066 1.0000
19.000 1.1704 0.09581 0.09269 0.0273 0.0067 1.0000
19.250 1.1197 0.10867 0.10574 0.0205 0.0067 1.0000
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