NACA 0015 (naca0015-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 0015 (naca0015-il) Reynolds number: 1,000,000 Max Cl/Cd: 75.1 at α=10.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-naca0015-il-1000000-n5.txt Download as CSV file: xf-naca0015-il-1000000-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 = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.3543 0.09065 0.08669 -0.0171 1.0000 0.0219
-19.500 -1.3750 0.08409 0.08002 -0.0201 1.0000 0.0221
-19.250 -1.3937 0.07786 0.07368 -0.0228 1.0000 0.0222
-19.000 -1.4104 0.07207 0.06778 -0.0252 1.0000 0.0224
-18.750 -1.4243 0.06680 0.06240 -0.0274 1.0000 0.0226
-18.500 -1.4358 0.06191 0.05741 -0.0293 1.0000 0.0228
-18.250 -1.4446 0.05753 0.05294 -0.0309 1.0000 0.0230
-18.000 -1.4512 0.05351 0.04882 -0.0323 1.0000 0.0232
-17.750 -1.4556 0.04987 0.04508 -0.0334 1.0000 0.0234
-17.500 -1.4581 0.04656 0.04169 -0.0343 1.0000 0.0236
-17.250 -1.4587 0.04357 0.03861 -0.0350 1.0000 0.0238
-17.000 -1.4571 0.04090 0.03586 -0.0355 1.0000 0.0241
-16.750 -1.4540 0.03847 0.03335 -0.0358 1.0000 0.0244
-16.500 -1.4492 0.03632 0.03112 -0.0359 1.0000 0.0247
-16.250 -1.4433 0.03433 0.02905 -0.0358 1.0000 0.0249
-16.000 -1.4363 0.03253 0.02718 -0.0356 1.0000 0.0252
-15.750 -1.4281 0.03091 0.02549 -0.0352 1.0000 0.0254
-15.500 -1.4197 0.02938 0.02389 -0.0347 1.0000 0.0256
-15.250 -1.4134 0.02775 0.02220 -0.0338 1.0000 0.0260
-15.000 -1.4052 0.02637 0.02077 -0.0329 1.0000 0.0264
-14.750 -1.3952 0.02518 0.01953 -0.0318 1.0000 0.0268
-14.500 -1.3841 0.02413 0.01843 -0.0307 1.0000 0.0272
-14.250 -1.3720 0.02319 0.01745 -0.0295 1.0000 0.0275
-14.000 -1.3591 0.02235 0.01656 -0.0282 1.0000 0.0280
-13.750 -1.3454 0.02160 0.01576 -0.0269 1.0000 0.0284
-13.500 -1.3311 0.02091 0.01502 -0.0255 1.0000 0.0287
-13.250 -1.3164 0.02027 0.01434 -0.0240 1.0000 0.0291
-13.000 -1.3009 0.01970 0.01372 -0.0225 1.0000 0.0294
-12.750 -1.2865 0.01911 0.01309 -0.0208 1.0000 0.0298
-12.500 -1.2728 0.01852 0.01248 -0.0188 1.0000 0.0304
-12.250 -1.2588 0.01802 0.01194 -0.0168 1.0000 0.0309
-12.000 -1.2438 0.01756 0.01146 -0.0148 1.0000 0.0314
-11.750 -1.2266 0.01713 0.01101 -0.0132 1.0000 0.0320
-11.500 -1.2089 0.01673 0.01059 -0.0116 1.0000 0.0326
-11.250 -1.1912 0.01636 0.01020 -0.0100 1.0000 0.0333
-11.000 -1.1738 0.01603 0.00983 -0.0082 1.0000 0.0338
-10.750 -1.1575 0.01567 0.00946 -0.0062 1.0000 0.0345
-10.500 -1.1416 0.01532 0.00909 -0.0040 1.0000 0.0354
-10.250 -1.1258 0.01499 0.00876 -0.0019 1.0000 0.0363
-10.000 -1.0962 0.01460 0.00836 -0.0026 0.9983 0.0375
-9.750 -1.0659 0.01424 0.00799 -0.0034 0.9963 0.0387
-9.500 -1.0354 0.01385 0.00761 -0.0043 0.9945 0.0405
-9.250 -1.0040 0.01348 0.00724 -0.0054 0.9930 0.0429
-9.000 -0.9750 0.01314 0.00691 -0.0059 0.9900 0.0454
-8.750 -0.9454 0.01277 0.00657 -0.0065 0.9868 0.0486
-8.500 -0.9149 0.01245 0.00625 -0.0073 0.9836 0.0519
-8.250 -0.8847 0.01211 0.00594 -0.0080 0.9802 0.0563
-8.000 -0.8575 0.01180 0.00566 -0.0080 0.9743 0.0607
-7.750 -0.8278 0.01152 0.00539 -0.0085 0.9694 0.0655
-7.500 -0.8013 0.01121 0.00512 -0.0084 0.9625 0.0712
-7.250 -0.7739 0.01094 0.00487 -0.0083 0.9553 0.0769
-7.000 -0.7478 0.01069 0.00464 -0.0080 0.9468 0.0830
-6.750 -0.7217 0.01043 0.00439 -0.0076 0.9378 0.0894
-6.500 -0.6958 0.01022 0.00419 -0.0072 0.9271 0.0952
-6.250 -0.6703 0.00998 0.00397 -0.0067 0.9162 0.1028
-6.000 -0.6445 0.00978 0.00377 -0.0062 0.9038 0.1102
-5.750 -0.6185 0.00959 0.00358 -0.0058 0.8904 0.1185
-5.500 -0.5927 0.00938 0.00339 -0.0053 0.8765 0.1291
-5.250 -0.5668 0.00918 0.00320 -0.0049 0.8619 0.1407
-5.000 -0.5406 0.00902 0.00303 -0.0045 0.8466 0.1517
-4.750 -0.5144 0.00886 0.00287 -0.0041 0.8304 0.1643
-4.500 -0.4886 0.00865 0.00270 -0.0037 0.8134 0.1826
-4.250 -0.4625 0.00847 0.00255 -0.0033 0.7959 0.2016
-4.000 -0.4362 0.00832 0.00241 -0.0029 0.7778 0.2190
-3.750 -0.4095 0.00820 0.00229 -0.0026 0.7592 0.2338
-3.500 -0.3827 0.00809 0.00218 -0.0024 0.7405 0.2491
-3.250 -0.3557 0.00800 0.00208 -0.0021 0.7220 0.2635
-3.000 -0.3286 0.00791 0.00199 -0.0019 0.7035 0.2790
-2.750 -0.3014 0.00784 0.00191 -0.0017 0.6851 0.2941
-2.500 -0.2742 0.00776 0.00183 -0.0015 0.6668 0.3097
-2.250 -0.2470 0.00769 0.00176 -0.0013 0.6485 0.3273
-1.750 -0.1925 0.00756 0.00164 -0.0010 0.6116 0.3636
-1.500 -0.1652 0.00750 0.00160 -0.0008 0.5935 0.3823
-1.250 -0.1379 0.00746 0.00156 -0.0006 0.5748 0.4008
-1.000 -0.1103 0.00743 0.00153 -0.0005 0.5565 0.4175
-0.750 -0.0828 0.00741 0.00150 -0.0004 0.5385 0.4344
-0.500 -0.0551 0.00740 0.00149 -0.0003 0.5210 0.4509
-0.250 -0.0276 0.00739 0.00148 -0.0001 0.5036 0.4681
0.000 0.0000 0.00739 0.00148 0.0000 0.4857 0.4859
0.250 0.0276 0.00739 0.00148 0.0001 0.4681 0.5035
0.500 0.0551 0.00740 0.00149 0.0003 0.4508 0.5211
0.750 0.0828 0.00741 0.00150 0.0004 0.4344 0.5389
1.000 0.1104 0.00743 0.00153 0.0005 0.4177 0.5565
1.250 0.1379 0.00746 0.00156 0.0006 0.4007 0.5747
1.500 0.1652 0.00750 0.00160 0.0008 0.3823 0.5935
1.750 0.1925 0.00756 0.00164 0.0010 0.3637 0.6118
2.250 0.2470 0.00769 0.00176 0.0013 0.3271 0.6483
2.500 0.2742 0.00777 0.00183 0.0015 0.3096 0.6667
2.750 0.3014 0.00783 0.00191 0.0017 0.2941 0.6853
3.000 0.3287 0.00791 0.00199 0.0019 0.2790 0.7035
3.250 0.3557 0.00800 0.00208 0.0021 0.2636 0.7221
3.500 0.3827 0.00809 0.00218 0.0024 0.2489 0.7406
3.750 0.4095 0.00820 0.00229 0.0026 0.2338 0.7592
4.000 0.4362 0.00832 0.00241 0.0029 0.2189 0.7778
4.250 0.4626 0.00847 0.00255 0.0033 0.2024 0.7959
4.500 0.4886 0.00865 0.00270 0.0037 0.1827 0.8134
4.750 0.5144 0.00886 0.00287 0.0041 0.1641 0.8304
5.000 0.5407 0.00902 0.00303 0.0045 0.1517 0.8465
5.250 0.5669 0.00918 0.00320 0.0049 0.1406 0.8619
5.500 0.5928 0.00938 0.00339 0.0053 0.1291 0.8765
5.750 0.6186 0.00959 0.00358 0.0058 0.1185 0.8904
6.000 0.6446 0.00979 0.00377 0.0062 0.1101 0.9038
6.250 0.6703 0.00999 0.00397 0.0067 0.1028 0.9161
6.500 0.6959 0.01022 0.00419 0.0072 0.0952 0.9271
6.750 0.7218 0.01043 0.00439 0.0076 0.0894 0.9378
7.000 0.7479 0.01069 0.00464 0.0080 0.0829 0.9468
7.250 0.7739 0.01094 0.00487 0.0083 0.0768 0.9553
7.500 0.8014 0.01121 0.00512 0.0083 0.0711 0.9625
7.750 0.8279 0.01152 0.00539 0.0085 0.0654 0.9694
8.000 0.8576 0.01180 0.00566 0.0080 0.0606 0.9743
8.250 0.8848 0.01211 0.00594 0.0080 0.0562 0.9803
8.500 0.9150 0.01245 0.00625 0.0073 0.0519 0.9837
8.750 0.9455 0.01277 0.00657 0.0065 0.0485 0.9868
9.000 0.9751 0.01314 0.00691 0.0059 0.0454 0.9901
9.250 1.0042 0.01347 0.00724 0.0054 0.0430 0.9930
9.500 1.0356 0.01385 0.00761 0.0043 0.0405 0.9945
9.750 1.0661 0.01424 0.00799 0.0034 0.0387 0.9963
10.000 1.0963 0.01460 0.00836 0.0026 0.0375 0.9983
10.250 1.1258 0.01499 0.00876 0.0019 0.0363 1.0000
10.500 1.1416 0.01531 0.00909 0.0041 0.0354 1.0000
10.750 1.1575 0.01567 0.00946 0.0062 0.0345 1.0000
11.000 1.1738 0.01603 0.00983 0.0082 0.0338 1.0000
11.250 1.1913 0.01636 0.01019 0.0099 0.0333 1.0000
11.500 1.2091 0.01673 0.01058 0.0116 0.0326 1.0000
11.750 1.2269 0.01713 0.01101 0.0131 0.0320 1.0000
12.000 1.2442 0.01756 0.01146 0.0147 0.0314 1.0000
12.250 1.2593 0.01802 0.01194 0.0167 0.0309 1.0000
12.500 1.2735 0.01852 0.01248 0.0187 0.0304 1.0000
12.750 1.2871 0.01911 0.01309 0.0207 0.0298 1.0000
13.000 1.3017 0.01970 0.01372 0.0224 0.0294 1.0000
13.250 1.3172 0.02027 0.01433 0.0239 0.0291 1.0000
13.500 1.3320 0.02090 0.01501 0.0253 0.0287 1.0000
13.750 1.3463 0.02159 0.01575 0.0267 0.0284 1.0000
14.000 1.3601 0.02234 0.01655 0.0280 0.0279 1.0000
14.250 1.3732 0.02318 0.01743 0.0293 0.0275 1.0000
14.500 1.3853 0.02412 0.01842 0.0305 0.0271 1.0000
14.750 1.3965 0.02517 0.01951 0.0316 0.0268 1.0000
15.000 1.4066 0.02635 0.02075 0.0327 0.0264 1.0000
15.250 1.4150 0.02773 0.02217 0.0336 0.0260 1.0000
15.500 1.4212 0.02937 0.02387 0.0344 0.0256 1.0000
15.750 1.4301 0.03086 0.02544 0.0349 0.0254 1.0000
16.000 1.4382 0.03248 0.02713 0.0353 0.0252 1.0000
16.250 1.4453 0.03428 0.02900 0.0355 0.0249 1.0000
16.500 1.4516 0.03623 0.03103 0.0356 0.0247 1.0000
16.750 1.4562 0.03842 0.03330 0.0355 0.0244 1.0000
17.000 1.4596 0.04081 0.03577 0.0352 0.0241 1.0000
17.250 1.4613 0.04348 0.03852 0.0347 0.0238 1.0000
17.500 1.4609 0.04646 0.04158 0.0340 0.0236 1.0000
17.750 1.4585 0.04975 0.04496 0.0331 0.0234 1.0000
18.000 1.4542 0.05339 0.04870 0.0319 0.0231 1.0000
18.250 1.4479 0.05738 0.05278 0.0306 0.0229 1.0000
18.500 1.4391 0.06177 0.05726 0.0289 0.0228 1.0000
18.750 1.4277 0.06664 0.06224 0.0270 0.0226 1.0000
19.000 1.4138 0.07193 0.06764 0.0249 0.0224 1.0000
19.250 1.3972 0.07771 0.07353 0.0224 0.0222 1.0000
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