NACA 65(2)-215 (naca652215-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 65(2)-215 (naca652215-il) Reynolds number: 1,000,000 Max Cl/Cd: 79.05 at α=3.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-naca652215-il-1000000-n5.txt Download as CSV file: xf-naca652215-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NACA 65(2)-215
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 -0.9710 0.12044 0.11804 -0.0261 1.0000 0.0094
-19.500 -1.0147 0.10738 0.10479 -0.0335 1.0000 0.0094
-19.250 -1.0498 0.09660 0.09382 -0.0396 1.0000 0.0094
-19.000 -1.0741 0.08815 0.08523 -0.0444 1.0000 0.0094
-18.750 -1.0925 0.08114 0.07808 -0.0483 1.0000 0.0094
-18.500 -1.1132 0.07407 0.07086 -0.0521 1.0000 0.0095
-18.250 -1.1266 0.06851 0.06517 -0.0548 1.0000 0.0095
-18.000 -1.1380 0.06355 0.06009 -0.0571 1.0000 0.0096
-17.750 -1.1462 0.05920 0.05564 -0.0589 1.0000 0.0097
-17.500 -1.1501 0.05561 0.05195 -0.0602 1.0000 0.0098
-17.250 -1.1513 0.05252 0.04877 -0.0611 1.0000 0.0099
-17.000 -1.1526 0.04951 0.04568 -0.0619 1.0000 0.0099
-16.750 -1.1497 0.04709 0.04319 -0.0625 1.0000 0.0101
-16.500 -1.1466 0.04477 0.04079 -0.0628 1.0000 0.0102
-16.250 -1.1440 0.04249 0.03843 -0.0630 1.0000 0.0103
-16.000 -1.1356 0.04087 0.03675 -0.0632 1.0000 0.0105
-15.750 -1.1330 0.03873 0.03453 -0.0631 1.0000 0.0106
-15.500 -1.1261 0.03707 0.03280 -0.0629 1.0000 0.0107
-15.250 -1.1198 0.03537 0.03102 -0.0626 1.0000 0.0108
-15.000 -1.1102 0.03403 0.02962 -0.0623 1.0000 0.0110
-14.750 -1.1047 0.03234 0.02785 -0.0617 1.0000 0.0111
-14.500 -1.0962 0.03095 0.02638 -0.0612 1.0000 0.0112
-14.250 -1.0845 0.02986 0.02523 -0.0607 1.0000 0.0115
-14.000 -1.0738 0.02870 0.02400 -0.0600 1.0000 0.0117
-13.750 -1.0656 0.02737 0.02258 -0.0591 1.0000 0.0117
-13.500 -1.0535 0.02638 0.02153 -0.0584 1.0000 0.0119
-13.250 -1.0412 0.02542 0.02051 -0.0576 1.0000 0.0120
-12.750 -1.0060 0.02302 0.01796 -0.0586 0.9683 0.0123
-12.500 -0.9707 0.02185 0.01671 -0.0626 0.9485 0.0127
-12.250 -0.9483 0.02114 0.01590 -0.0632 0.9249 0.0130
-12.000 -0.9340 0.02052 0.01516 -0.0621 0.9041 0.0132
-11.750 -0.9201 0.01995 0.01451 -0.0607 0.8883 0.0134
-11.500 -0.9072 0.01931 0.01377 -0.0592 0.8744 0.0136
-11.250 -0.8937 0.01872 0.01310 -0.0577 0.8624 0.0138
-11.000 -0.8803 0.01813 0.01241 -0.0561 0.8515 0.0140
-10.750 -0.8657 0.01761 0.01181 -0.0546 0.8413 0.0142
-10.500 -0.8521 0.01706 0.01118 -0.0530 0.8318 0.0144
-10.250 -0.8381 0.01657 0.01060 -0.0512 0.8226 0.0146
-10.000 -0.8231 0.01615 0.01012 -0.0495 0.8148 0.0149
-9.750 -0.8082 0.01579 0.00970 -0.0477 0.8069 0.0151
-9.500 -0.7921 0.01539 0.00923 -0.0461 0.8000 0.0152
-9.250 -0.7754 0.01488 0.00865 -0.0446 0.7923 0.0156
-9.000 -0.7571 0.01441 0.00812 -0.0434 0.7859 0.0160
-8.750 -0.7368 0.01403 0.00769 -0.0425 0.7790 0.0163
-8.250 -0.6932 0.01336 0.00695 -0.0411 0.7676 0.0170
-8.000 -0.6705 0.01305 0.00660 -0.0405 0.7618 0.0174
-7.750 -0.6475 0.01277 0.00626 -0.0399 0.7562 0.0178
-7.500 -0.6237 0.01248 0.00593 -0.0395 0.7508 0.0183
-7.250 -0.5995 0.01223 0.00564 -0.0392 0.7450 0.0187
-7.000 -0.5751 0.01199 0.00535 -0.0388 0.7398 0.0190
-6.750 -0.5513 0.01165 0.00499 -0.0384 0.7351 0.0198
-6.500 -0.5266 0.01138 0.00470 -0.0381 0.7301 0.0206
-6.250 -0.5015 0.01116 0.00444 -0.0379 0.7255 0.0215
-6.000 -0.4757 0.01094 0.00421 -0.0377 0.7214 0.0222
-5.750 -0.4496 0.01074 0.00398 -0.0376 0.7167 0.0232
-5.500 -0.4237 0.01054 0.00375 -0.0375 0.7120 0.0242
-5.250 -0.3978 0.01033 0.00353 -0.0374 0.7077 0.0260
-5.000 -0.3712 0.01014 0.00334 -0.0374 0.7035 0.0281
-4.750 -0.3445 0.00997 0.00315 -0.0374 0.6994 0.0306
-4.500 -0.3179 0.00979 0.00297 -0.0374 0.6954 0.0343
-4.250 -0.2912 0.00961 0.00280 -0.0374 0.6918 0.0402
-4.000 -0.2645 0.00939 0.00263 -0.0374 0.6880 0.0517
-3.750 -0.2383 0.00912 0.00244 -0.0374 0.6839 0.0752
-3.500 -0.2127 0.00878 0.00224 -0.0374 0.6798 0.1156
-3.000 -0.1627 0.00782 0.00180 -0.0372 0.6731 0.2555
-2.750 -0.1379 0.00727 0.00156 -0.0372 0.6695 0.3430
-2.500 -0.1143 0.00654 0.00130 -0.0370 0.6658 0.4726
-2.250 -0.0879 0.00623 0.00125 -0.0370 0.6621 0.5497
-2.000 -0.0596 0.00614 0.00124 -0.0373 0.6590 0.5798
-1.750 -0.0308 0.00610 0.00124 -0.0376 0.6558 0.6000
-1.500 -0.0020 0.00608 0.00123 -0.0379 0.6524 0.6102
-1.250 0.0271 0.00609 0.00121 -0.0382 0.6489 0.6154
-0.750 0.0853 0.00609 0.00118 -0.0389 0.6427 0.6215
-0.500 0.1145 0.00608 0.00118 -0.0393 0.6396 0.6248
-0.250 0.1436 0.00609 0.00118 -0.0396 0.6362 0.6281
0.000 0.1727 0.00611 0.00118 -0.0400 0.6329 0.6311
0.250 0.2016 0.00613 0.00119 -0.0403 0.6298 0.6340
0.500 0.2308 0.00613 0.00120 -0.0407 0.6271 0.6373
0.750 0.2599 0.00613 0.00123 -0.0410 0.6239 0.6407
1.000 0.2890 0.00615 0.00125 -0.0414 0.6206 0.6439
1.250 0.3180 0.00618 0.00128 -0.0417 0.6174 0.6472
1.500 0.3468 0.00621 0.00131 -0.0420 0.6142 0.6504
1.750 0.3759 0.00621 0.00136 -0.0424 0.6105 0.6539
2.000 0.4047 0.00624 0.00139 -0.0427 0.6043 0.6575
2.250 0.4331 0.00629 0.00144 -0.0429 0.5965 0.6610
2.500 0.4614 0.00635 0.00147 -0.0431 0.5848 0.6645
2.750 0.4889 0.00643 0.00152 -0.0432 0.5674 0.6682
3.000 0.5161 0.00654 0.00159 -0.0432 0.5430 0.6721
3.250 0.5407 0.00684 0.00170 -0.0428 0.4926 0.6760
3.500 0.5591 0.00764 0.00204 -0.0414 0.3852 0.6796
3.750 0.5780 0.00840 0.00243 -0.0402 0.2973 0.6834
4.000 0.5981 0.00904 0.00277 -0.0392 0.2275 0.6877
4.250 0.6182 0.00966 0.00312 -0.0382 0.1632 0.6922
4.500 0.6396 0.01016 0.00343 -0.0374 0.1171 0.6964
4.750 0.6613 0.01061 0.00374 -0.0366 0.0826 0.7003
5.000 0.6834 0.01101 0.00404 -0.0359 0.0567 0.7047
5.250 0.7059 0.01138 0.00432 -0.0352 0.0397 0.7093
5.750 0.7534 0.01190 0.00484 -0.0342 0.0293 0.7186
6.000 0.7765 0.01217 0.00511 -0.0336 0.0262 0.7239
6.250 0.8001 0.01241 0.00537 -0.0330 0.0245 0.7288
6.500 0.8227 0.01268 0.00566 -0.0324 0.0227 0.7335
6.750 0.8443 0.01299 0.00599 -0.0315 0.0209 0.7388
7.000 0.8666 0.01325 0.00627 -0.0308 0.0199 0.7441
7.250 0.8877 0.01354 0.00659 -0.0298 0.0188 0.7496
7.500 0.9073 0.01385 0.00693 -0.0286 0.0178 0.7560
7.750 0.9240 0.01419 0.00729 -0.0269 0.0170 0.7623
8.000 0.9407 0.01452 0.00767 -0.0252 0.0164 0.7686
8.250 0.9577 0.01487 0.00808 -0.0236 0.0161 0.7754
8.500 0.9742 0.01526 0.00852 -0.0220 0.0156 0.7818
8.750 0.9906 0.01568 0.00898 -0.0204 0.0151 0.7892
9.000 1.0065 0.01613 0.00948 -0.0188 0.0147 0.7966
9.250 1.0221 0.01661 0.01000 -0.0173 0.0144 0.8052
9.500 1.0367 0.01716 0.01060 -0.0157 0.0139 0.8134
9.750 1.0505 0.01776 0.01127 -0.0140 0.0136 0.8227
10.000 1.0637 0.01842 0.01200 -0.0123 0.0132 0.8314
10.250 1.0780 0.01904 0.01268 -0.0109 0.0131 0.8414
10.500 1.0917 0.01969 0.01342 -0.0093 0.0129 0.8521
10.750 1.1049 0.02037 0.01418 -0.0078 0.0128 0.8643
11.000 1.1180 0.02106 0.01496 -0.0063 0.0126 0.8782
11.250 1.1310 0.02172 0.01572 -0.0048 0.0123 0.8951
11.500 1.1422 0.02246 0.01656 -0.0031 0.0121 0.9164
11.750 1.1552 0.02323 0.01745 -0.0018 0.0119 0.9493
12.000 1.1756 0.02417 0.01848 -0.0024 0.0117 1.0000
12.250 1.1884 0.02514 0.01949 -0.0015 0.0116 1.0000
12.500 1.2012 0.02613 0.02051 -0.0005 0.0114 1.0000
12.750 1.2133 0.02718 0.02161 0.0004 0.0112 1.0000
13.000 1.2244 0.02833 0.02280 0.0013 0.0110 1.0000
13.250 1.2352 0.02952 0.02404 0.0022 0.0109 1.0000
13.500 1.2446 0.03086 0.02543 0.0031 0.0108 1.0000
13.750 1.2504 0.03252 0.02715 0.0041 0.0105 1.0000
14.000 1.2565 0.03418 0.02889 0.0050 0.0104 1.0000
14.250 1.2649 0.03570 0.03047 0.0057 0.0104 1.0000
14.500 1.2732 0.03727 0.03211 0.0063 0.0103 1.0000
14.750 1.2812 0.03889 0.03381 0.0069 0.0102 1.0000
15.000 1.2896 0.04052 0.03551 0.0073 0.0101 1.0000
15.250 1.2960 0.04239 0.03746 0.0077 0.0101 1.0000
15.500 1.3026 0.04429 0.03945 0.0080 0.0099 1.0000
15.750 1.3105 0.04609 0.04131 0.0082 0.0098 1.0000
16.000 1.3139 0.04841 0.04373 0.0084 0.0097 1.0000
16.250 1.3188 0.05063 0.04603 0.0084 0.0097 1.0000
16.500 1.3244 0.05284 0.04832 0.0082 0.0095 1.0000
16.750 1.3260 0.05557 0.05114 0.0081 0.0095 1.0000
17.000 1.3284 0.05826 0.05392 0.0077 0.0094 1.0000
17.250 1.3292 0.06125 0.05701 0.0072 0.0093 1.0000
17.500 1.3319 0.06408 0.05992 0.0066 0.0092 1.0000
17.750 1.3294 0.06767 0.06362 0.0057 0.0091 1.0000
18.000 1.3274 0.07130 0.06736 0.0046 0.0091 1.0000
18.250 1.3269 0.07483 0.07098 0.0034 0.0090 1.0000
18.500 1.3230 0.07896 0.07522 0.0019 0.0090 1.0000
18.750 1.3189 0.08327 0.07962 0.0002 0.0089 1.0000
19.000 1.3118 0.08816 0.08464 -0.0019 0.0089 1.0000
19.250 1.3089 0.09252 0.08909 -0.0040 0.0087 1.0000
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