NACA 0015 (naca0015-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 0015 (naca0015-il) Reynolds number: 500,000 Max Cl/Cd: 63.23 at α=8.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-naca0015-il-500000-n5.txt Download as CSV file: xf-naca0015-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NACA 0015
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.500 -1.2035 0.10925 0.10499 -0.0097 1.0000 0.0270
-19.250 -1.2134 0.10396 0.09961 -0.0123 1.0000 0.0272
-19.000 -1.2233 0.09873 0.09428 -0.0148 1.0000 0.0274
-18.750 -1.2330 0.09358 0.08903 -0.0172 1.0000 0.0277
-18.500 -1.2424 0.08854 0.08388 -0.0194 1.0000 0.0279
-18.250 -1.2514 0.08364 0.07888 -0.0216 1.0000 0.0282
-18.000 -1.2597 0.07888 0.07402 -0.0237 1.0000 0.0284
-17.750 -1.2674 0.07429 0.06931 -0.0256 1.0000 0.0287
-17.500 -1.2744 0.06988 0.06480 -0.0274 1.0000 0.0289
-17.250 -1.2802 0.06571 0.06051 -0.0290 1.0000 0.0292
-17.000 -1.2847 0.06178 0.05647 -0.0305 1.0000 0.0294
-16.750 -1.2893 0.05793 0.05251 -0.0319 1.0000 0.0296
-16.500 -1.2961 0.05391 0.04840 -0.0332 1.0000 0.0299
-16.250 -1.3010 0.05022 0.04463 -0.0343 1.0000 0.0302
-16.000 -1.3034 0.04691 0.04124 -0.0352 1.0000 0.0305
-15.750 -1.3038 0.04392 0.03817 -0.0359 1.0000 0.0308
-15.500 -1.3022 0.04125 0.03541 -0.0364 1.0000 0.0312
-15.250 -1.2990 0.03884 0.03292 -0.0366 1.0000 0.0316
-15.000 -1.2946 0.03665 0.03064 -0.0366 1.0000 0.0320
-14.750 -1.2892 0.03465 0.02855 -0.0365 1.0000 0.0324
-14.500 -1.2826 0.03285 0.02667 -0.0361 1.0000 0.0328
-14.250 -1.2748 0.03123 0.02497 -0.0356 1.0000 0.0332
-14.000 -1.2658 0.02980 0.02345 -0.0349 1.0000 0.0337
-13.750 -1.2568 0.02844 0.02202 -0.0340 1.0000 0.0341
-13.500 -1.2502 0.02698 0.02050 -0.0328 1.0000 0.0346
-13.250 -1.2414 0.02576 0.01923 -0.0315 1.0000 0.0351
-13.000 -1.2310 0.02471 0.01813 -0.0301 1.0000 0.0357
-12.750 -1.2196 0.02378 0.01715 -0.0286 1.0000 0.0363
-12.500 -1.2071 0.02296 0.01628 -0.0271 1.0000 0.0370
-12.250 -1.1940 0.02222 0.01549 -0.0255 1.0000 0.0377
-12.000 -1.1805 0.02155 0.01476 -0.0237 1.0000 0.0384
-11.750 -1.1669 0.02094 0.01408 -0.0219 1.0000 0.0390
-11.500 -1.1557 0.02026 0.01338 -0.0196 1.0000 0.0399
-11.250 -1.1436 0.01969 0.01279 -0.0172 1.0000 0.0407
-11.000 -1.1292 0.01917 0.01224 -0.0152 1.0000 0.0418
-10.750 -1.1135 0.01870 0.01173 -0.0133 1.0000 0.0429
-10.500 -1.0973 0.01827 0.01126 -0.0114 1.0000 0.0441
-10.250 -1.0822 0.01781 0.01079 -0.0093 1.0000 0.0455
-10.000 -1.0673 0.01737 0.01035 -0.0071 1.0000 0.0473
-9.750 -1.0517 0.01699 0.00995 -0.0050 1.0000 0.0492
-9.500 -1.0359 0.01663 0.00957 -0.0029 1.0000 0.0512
-9.250 -1.0209 0.01624 0.00919 -0.0007 1.0000 0.0536
-9.000 -1.0052 0.01590 0.00885 0.0015 1.0000 0.0564
-8.750 -0.9786 0.01548 0.00843 0.0014 0.9983 0.0602
-8.500 -0.9470 0.01508 0.00804 0.0002 0.9957 0.0649
-8.250 -0.9150 0.01464 0.00764 -0.0010 0.9934 0.0706
-8.000 -0.8842 0.01425 0.00727 -0.0019 0.9903 0.0765
-7.750 -0.8529 0.01388 0.00692 -0.0029 0.9868 0.0832
-7.500 -0.8204 0.01349 0.00657 -0.0042 0.9839 0.0902
-7.250 -0.7866 0.01313 0.00624 -0.0057 0.9815 0.0976
-7.000 -0.7577 0.01281 0.00594 -0.0060 0.9759 0.1053
-6.750 -0.7266 0.01245 0.00563 -0.0069 0.9713 0.1144
-6.500 -0.6959 0.01212 0.00534 -0.0077 0.9665 0.1248
-6.250 -0.6677 0.01181 0.00508 -0.0078 0.9593 0.1358
-6.000 -0.6367 0.01150 0.00482 -0.0086 0.9538 0.1479
-5.750 -0.6102 0.01122 0.00459 -0.0084 0.9446 0.1600
-5.500 -0.5816 0.01092 0.00434 -0.0085 0.9368 0.1747
-5.000 -0.5293 0.01031 0.00390 -0.0079 0.9158 0.2132
-4.750 -0.5028 0.01006 0.00369 -0.0075 0.9043 0.2304
-4.500 -0.4768 0.00984 0.00351 -0.0071 0.8913 0.2466
-4.250 -0.4506 0.00963 0.00334 -0.0066 0.8779 0.2632
-4.000 -0.4243 0.00945 0.00317 -0.0062 0.8636 0.2795
-3.750 -0.3981 0.00928 0.00302 -0.0057 0.8483 0.2961
-3.500 -0.3719 0.00914 0.00288 -0.0053 0.8321 0.3126
-3.250 -0.3455 0.00901 0.00275 -0.0048 0.8149 0.3295
-3.000 -0.3193 0.00888 0.00263 -0.0044 0.7971 0.3475
-2.750 -0.2930 0.00876 0.00252 -0.0040 0.7790 0.3662
-2.500 -0.2666 0.00866 0.00242 -0.0035 0.7606 0.3854
-2.250 -0.2402 0.00857 0.00233 -0.0031 0.7420 0.4049
-2.000 -0.2138 0.00849 0.00226 -0.0027 0.7234 0.4245
-1.750 -0.1872 0.00843 0.00219 -0.0024 0.7045 0.4428
-1.500 -0.1605 0.00837 0.00213 -0.0020 0.6857 0.4609
-1.250 -0.1337 0.00833 0.00208 -0.0017 0.6667 0.4786
-1.000 -0.1070 0.00830 0.00205 -0.0013 0.6475 0.4966
-0.750 -0.0803 0.00827 0.00202 -0.0010 0.6283 0.5152
-0.500 -0.0535 0.00825 0.00199 -0.0007 0.6089 0.5337
-0.250 -0.0268 0.00824 0.00198 -0.0003 0.5897 0.5522
0.000 0.0000 0.00824 0.00198 0.0000 0.5710 0.5710
0.250 0.0268 0.00824 0.00198 0.0003 0.5523 0.5897
0.500 0.0535 0.00825 0.00199 0.0007 0.5337 0.6089
0.750 0.0803 0.00827 0.00202 0.0010 0.5152 0.6283
1.000 0.1070 0.00830 0.00205 0.0013 0.4965 0.6475
1.250 0.1338 0.00833 0.00208 0.0017 0.4786 0.6666
1.500 0.1605 0.00837 0.00213 0.0020 0.4609 0.6857
1.750 0.1872 0.00842 0.00219 0.0024 0.4428 0.7045
2.000 0.2138 0.00849 0.00226 0.0027 0.4244 0.7235
2.250 0.2402 0.00857 0.00233 0.0031 0.4049 0.7421
2.500 0.2666 0.00866 0.00242 0.0035 0.3854 0.7607
2.750 0.2930 0.00876 0.00252 0.0040 0.3661 0.7790
3.000 0.3193 0.00888 0.00263 0.0044 0.3476 0.7971
3.250 0.3456 0.00901 0.00275 0.0048 0.3295 0.8149
3.500 0.3719 0.00914 0.00288 0.0053 0.3126 0.8321
3.750 0.3982 0.00929 0.00302 0.0057 0.2961 0.8483
4.000 0.4244 0.00945 0.00317 0.0062 0.2795 0.8636
4.250 0.4506 0.00963 0.00334 0.0066 0.2632 0.8778
4.500 0.4768 0.00984 0.00351 0.0070 0.2466 0.8913
4.750 0.5029 0.01006 0.00369 0.0075 0.2305 0.9044
5.000 0.5294 0.01031 0.00390 0.0078 0.2132 0.9158
5.500 0.5817 0.01092 0.00434 0.0085 0.1746 0.9369
5.750 0.6102 0.01122 0.00459 0.0083 0.1600 0.9447
6.000 0.6367 0.01150 0.00482 0.0086 0.1479 0.9538
6.250 0.6678 0.01181 0.00508 0.0078 0.1357 0.9593
6.500 0.6959 0.01212 0.00534 0.0077 0.1248 0.9665
6.750 0.7267 0.01245 0.00563 0.0069 0.1145 0.9713
7.000 0.7578 0.01281 0.00594 0.0060 0.1053 0.9760
7.250 0.7867 0.01313 0.00624 0.0056 0.0975 0.9815
7.500 0.8205 0.01349 0.00657 0.0042 0.0902 0.9839
7.750 0.8530 0.01388 0.00692 0.0029 0.0831 0.9869
8.000 0.8843 0.01425 0.00727 0.0019 0.0765 0.9903
8.250 0.9151 0.01464 0.00764 0.0010 0.0705 0.9935
8.500 0.9472 0.01507 0.00804 -0.0003 0.0649 0.9958
8.750 0.9788 0.01548 0.00843 -0.0014 0.0601 0.9983
9.000 1.0051 0.01590 0.00885 -0.0015 0.0564 1.0000
9.250 1.0209 0.01623 0.00919 0.0007 0.0536 1.0000
9.500 1.0358 0.01663 0.00957 0.0029 0.0511 1.0000
9.750 1.0517 0.01698 0.00995 0.0050 0.0492 1.0000
10.000 1.0674 0.01737 0.01035 0.0071 0.0473 1.0000
10.250 1.0823 0.01781 0.01079 0.0093 0.0455 1.0000
10.500 1.0974 0.01826 0.01126 0.0114 0.0441 1.0000
10.750 1.1137 0.01869 0.01173 0.0132 0.0429 1.0000
11.000 1.1295 0.01917 0.01224 0.0151 0.0417 1.0000
11.250 1.1440 0.01969 0.01279 0.0171 0.0407 1.0000
11.500 1.1562 0.02026 0.01338 0.0195 0.0399 1.0000
11.750 1.1675 0.02094 0.01408 0.0218 0.0390 1.0000
12.000 1.1812 0.02155 0.01475 0.0236 0.0384 1.0000
12.250 1.1947 0.02222 0.01548 0.0253 0.0377 1.0000
12.500 1.2079 0.02296 0.01627 0.0269 0.0370 1.0000
12.750 1.2204 0.02378 0.01714 0.0285 0.0363 1.0000
13.000 1.2319 0.02470 0.01812 0.0299 0.0356 1.0000
13.250 1.2424 0.02575 0.01922 0.0313 0.0351 1.0000
13.500 1.2512 0.02697 0.02049 0.0326 0.0346 1.0000
13.750 1.2578 0.02843 0.02200 0.0338 0.0341 1.0000
14.000 1.2672 0.02977 0.02342 0.0347 0.0337 1.0000
14.250 1.2762 0.03121 0.02494 0.0354 0.0332 1.0000
14.500 1.2841 0.03281 0.02664 0.0359 0.0328 1.0000
14.750 1.2908 0.03461 0.02852 0.0362 0.0323 1.0000
15.000 1.2963 0.03660 0.03059 0.0364 0.0320 1.0000
15.250 1.3009 0.03879 0.03286 0.0363 0.0316 1.0000
15.500 1.3042 0.04119 0.03534 0.0361 0.0312 1.0000
15.750 1.3058 0.04387 0.03811 0.0356 0.0308 1.0000
16.000 1.3056 0.04685 0.04117 0.0349 0.0305 1.0000
16.250 1.3032 0.05016 0.04456 0.0340 0.0302 1.0000
16.500 1.2984 0.05384 0.04833 0.0329 0.0299 1.0000
16.750 1.2915 0.05787 0.05245 0.0315 0.0296 1.0000
17.000 1.2874 0.06167 0.05636 0.0302 0.0294 1.0000
17.250 1.2831 0.06559 0.06038 0.0287 0.0292 1.0000
17.500 1.2774 0.06975 0.06467 0.0271 0.0289 1.0000
17.750 1.2705 0.07416 0.06919 0.0253 0.0287 1.0000
18.000 1.2628 0.07876 0.07389 0.0233 0.0284 1.0000
18.250 1.2545 0.08352 0.07876 0.0213 0.0282 1.0000
18.500 1.2455 0.08842 0.08377 0.0191 0.0279 1.0000
18.750 1.2360 0.09347 0.08892 0.0168 0.0277 1.0000
19.000 1.2264 0.09864 0.09418 0.0144 0.0274 1.0000
19.250 1.2165 0.10387 0.09951 0.0119 0.0272 1.0000
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