NACA 0015 (naca0015-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: NACA 0015 (naca0015-il) Reynolds number: 500,000 Max Cl/Cd: 66.43 at α=7.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-naca0015-il-500000.txt Download as CSV file: xf-naca0015-il-500000.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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.000 -1.2266 0.09480 0.09051 -0.0217 1.0000 0.0323
-18.750 -1.2343 0.08997 0.08558 -0.0241 1.0000 0.0326
-18.500 -1.2418 0.08523 0.08072 -0.0264 1.0000 0.0330
-18.250 -1.2490 0.08063 0.07600 -0.0285 1.0000 0.0333
-18.000 -1.2550 0.07631 0.07155 -0.0305 1.0000 0.0337
-17.750 -1.2603 0.07213 0.06724 -0.0324 1.0000 0.0340
-17.500 -1.2647 0.06816 0.06313 -0.0340 1.0000 0.0343
-17.250 -1.2683 0.06439 0.05923 -0.0356 1.0000 0.0345
-17.000 -1.2705 0.06117 0.05592 -0.0362 1.0000 0.0349
-16.750 -1.2707 0.05830 0.05302 -0.0364 1.0000 0.0353
-16.500 -1.2702 0.05544 0.05011 -0.0370 1.0000 0.0357
-16.250 -1.2690 0.05267 0.04728 -0.0376 1.0000 0.0361
-16.000 -1.2671 0.04999 0.04454 -0.0382 1.0000 0.0366
-15.750 -1.2645 0.04742 0.04190 -0.0387 1.0000 0.0371
-15.500 -1.2614 0.04498 0.03937 -0.0390 1.0000 0.0376
-15.250 -1.2575 0.04266 0.03696 -0.0392 1.0000 0.0381
-15.000 -1.2527 0.04049 0.03468 -0.0392 1.0000 0.0386
-14.750 -1.2469 0.03848 0.03257 -0.0391 1.0000 0.0390
-14.500 -1.2398 0.03667 0.03064 -0.0389 1.0000 0.0394
-14.250 -1.2369 0.03453 0.02845 -0.0381 1.0000 0.0400
-14.000 -1.2328 0.03260 0.02650 -0.0373 1.0000 0.0407
-13.750 -1.2255 0.03101 0.02487 -0.0366 1.0000 0.0413
-13.500 -1.2167 0.02961 0.02342 -0.0357 1.0000 0.0420
-13.250 -1.2072 0.02832 0.02207 -0.0347 1.0000 0.0427
-13.000 -1.1972 0.02713 0.02081 -0.0336 1.0000 0.0434
-12.750 -1.1862 0.02606 0.01965 -0.0323 1.0000 0.0441
-12.500 -1.1736 0.02514 0.01865 -0.0310 1.0000 0.0448
-12.250 -1.1674 0.02385 0.01732 -0.0289 1.0000 0.0457
-12.000 -1.1587 0.02282 0.01627 -0.0269 1.0000 0.0467
-11.750 -1.1468 0.02203 0.01546 -0.0250 1.0000 0.0478
-11.500 -1.1345 0.02133 0.01472 -0.0230 1.0000 0.0489
-11.250 -1.1220 0.02071 0.01404 -0.0209 1.0000 0.0500
-11.000 -1.1086 0.02019 0.01345 -0.0186 1.0000 0.0510
-10.750 -1.1014 0.01935 0.01261 -0.0155 1.0000 0.0525
-10.500 -1.0881 0.01876 0.01202 -0.0133 1.0000 0.0542
-10.250 -1.0731 0.01830 0.01153 -0.0112 1.0000 0.0561
-10.000 -1.0583 0.01785 0.01103 -0.0089 1.0000 0.0581
-9.750 -1.0471 0.01724 0.01045 -0.0062 1.0000 0.0608
-9.500 -1.0323 0.01682 0.01002 -0.0039 1.0000 0.0637
-9.250 -1.0188 0.01634 0.00954 -0.0013 1.0000 0.0671
-9.000 -1.0047 0.01591 0.00912 0.0011 1.0000 0.0713
-8.750 -0.9903 0.01549 0.00872 0.0035 1.0000 0.0761
-8.500 -0.9750 0.01512 0.00836 0.0057 1.0000 0.0818
-8.250 -0.9602 0.01471 0.00800 0.0080 1.0000 0.0883
-8.000 -0.9438 0.01439 0.00768 0.0100 1.0000 0.0949
-7.750 -0.9276 0.01405 0.00737 0.0121 1.0000 0.1024
-7.500 -0.9108 0.01372 0.00709 0.0140 1.0000 0.1102
-7.250 -0.8772 0.01334 0.00675 0.0124 0.9979 0.1213
-7.000 -0.8411 0.01295 0.00644 0.0104 0.9954 0.1343
-6.750 -0.8042 0.01258 0.00615 0.0082 0.9932 0.1493
-6.500 -0.7699 0.01221 0.00585 0.0066 0.9898 0.1651
-6.250 -0.7344 0.01185 0.00558 0.0048 0.9863 0.1823
-6.000 -0.6973 0.01151 0.00532 0.0026 0.9836 0.2014
-5.750 -0.6589 0.01118 0.00507 0.0002 0.9815 0.2217
-5.500 -0.6260 0.01083 0.00483 -0.0010 0.9767 0.2420
-5.250 -0.5899 0.01049 0.00460 -0.0029 0.9730 0.2652
-5.000 -0.5517 0.01015 0.00437 -0.0052 0.9703 0.2910
-4.750 -0.5141 0.00982 0.00415 -0.0073 0.9676 0.3154
-4.500 -0.4856 0.00955 0.00397 -0.0074 0.9595 0.3358
-4.250 -0.4519 0.00929 0.00377 -0.0085 0.9543 0.3572
-4.000 -0.4243 0.00905 0.00360 -0.0083 0.9453 0.3768
-3.750 -0.3947 0.00880 0.00342 -0.0085 0.9377 0.3971
-3.500 -0.3691 0.00859 0.00328 -0.0078 0.9262 0.4164
-3.250 -0.3421 0.00839 0.00313 -0.0074 0.9157 0.4362
-3.000 -0.3158 0.00821 0.00299 -0.0068 0.9038 0.4563
-2.750 -0.2899 0.00805 0.00288 -0.0061 0.8900 0.4766
-2.500 -0.2637 0.00791 0.00277 -0.0055 0.8761 0.4971
-2.250 -0.2373 0.00778 0.00267 -0.0050 0.8616 0.5177
-2.000 -0.2110 0.00767 0.00257 -0.0044 0.8462 0.5379
-1.750 -0.1848 0.00757 0.00249 -0.0038 0.8299 0.5579
-1.500 -0.1584 0.00749 0.00242 -0.0032 0.8127 0.5776
-1.250 -0.1321 0.00742 0.00237 -0.0027 0.7947 0.5975
-1.000 -0.1057 0.00736 0.00232 -0.0021 0.7763 0.6175
-0.750 -0.0793 0.00732 0.00228 -0.0016 0.7574 0.6376
-0.500 -0.0529 0.00729 0.00225 -0.0010 0.7380 0.6580
-0.250 -0.0265 0.00728 0.00224 -0.0005 0.7183 0.6781
0.000 0.0000 0.00727 0.00223 0.0000 0.6982 0.6982
0.250 0.0265 0.00728 0.00224 0.0005 0.6781 0.7183
0.500 0.0529 0.00729 0.00225 0.0010 0.6580 0.7379
0.750 0.0793 0.00732 0.00228 0.0016 0.6376 0.7574
1.000 0.1057 0.00736 0.00232 0.0021 0.6175 0.7764
1.250 0.1321 0.00742 0.00237 0.0027 0.5975 0.7947
1.500 0.1584 0.00749 0.00242 0.0032 0.5776 0.8126
1.750 0.1848 0.00757 0.00249 0.0038 0.5579 0.8299
2.000 0.2110 0.00767 0.00257 0.0044 0.5380 0.8461
2.250 0.2373 0.00778 0.00267 0.0050 0.5177 0.8616
2.500 0.2637 0.00791 0.00277 0.0055 0.4971 0.8760
2.750 0.2899 0.00805 0.00288 0.0061 0.4765 0.8900
3.000 0.3158 0.00821 0.00299 0.0068 0.4564 0.9038
3.250 0.3421 0.00839 0.00313 0.0074 0.4363 0.9157
3.500 0.3691 0.00859 0.00328 0.0078 0.4164 0.9262
3.750 0.3947 0.00880 0.00342 0.0085 0.3971 0.9376
4.000 0.4243 0.00905 0.00360 0.0083 0.3768 0.9453
4.250 0.4519 0.00929 0.00377 0.0085 0.3572 0.9543
4.500 0.4856 0.00955 0.00397 0.0074 0.3358 0.9595
4.750 0.5141 0.00982 0.00415 0.0073 0.3154 0.9676
5.000 0.5517 0.01015 0.00437 0.0052 0.2910 0.9703
5.250 0.5899 0.01049 0.00460 0.0029 0.2652 0.9730
5.500 0.6260 0.01083 0.00483 0.0010 0.2419 0.9767
5.750 0.6590 0.01118 0.00507 -0.0002 0.2216 0.9816
6.000 0.6974 0.01150 0.00532 -0.0026 0.2013 0.9836
6.250 0.7345 0.01185 0.00557 -0.0048 0.1823 0.9864
6.500 0.7700 0.01220 0.00585 -0.0066 0.1652 0.9898
6.750 0.8043 0.01258 0.00614 -0.0082 0.1493 0.9932
7.000 0.8412 0.01295 0.00643 -0.0104 0.1343 0.9954
7.250 0.8773 0.01333 0.00675 -0.0125 0.1213 0.9980
7.500 0.9107 0.01371 0.00708 -0.0139 0.1103 1.0000
7.750 0.9274 0.01404 0.00737 -0.0120 0.1025 1.0000
8.000 0.9437 0.01439 0.00768 -0.0100 0.0950 1.0000
8.250 0.9601 0.01471 0.00799 -0.0080 0.0883 1.0000
8.500 0.9749 0.01512 0.00836 -0.0057 0.0818 1.0000
8.750 0.9902 0.01549 0.00871 -0.0034 0.0761 1.0000
9.000 1.0046 0.01590 0.00912 -0.0011 0.0713 1.0000
9.250 1.0187 0.01634 0.00954 0.0014 0.0671 1.0000
9.500 1.0323 0.01681 0.01001 0.0039 0.0637 1.0000
9.750 1.0471 0.01723 0.01045 0.0062 0.0608 1.0000
10.000 1.0584 0.01785 0.01103 0.0089 0.0581 1.0000
10.250 1.0732 0.01830 0.01153 0.0111 0.0561 1.0000
10.500 1.0883 0.01876 0.01202 0.0132 0.0542 1.0000
10.750 1.1017 0.01935 0.01261 0.0155 0.0525 1.0000
11.000 1.1090 0.02019 0.01345 0.0186 0.0510 1.0000
11.250 1.1225 0.02071 0.01404 0.0208 0.0500 1.0000
11.500 1.1351 0.02133 0.01471 0.0229 0.0488 1.0000
11.750 1.1475 0.02203 0.01546 0.0249 0.0477 1.0000
12.000 1.1594 0.02282 0.01627 0.0268 0.0467 1.0000
12.250 1.1681 0.02385 0.01732 0.0288 0.0457 1.0000
12.500 1.1745 0.02513 0.01864 0.0308 0.0448 1.0000
12.750 1.1871 0.02605 0.01965 0.0321 0.0441 1.0000
13.000 1.1982 0.02712 0.02079 0.0334 0.0434 1.0000
13.250 1.2083 0.02831 0.02205 0.0346 0.0427 1.0000
13.500 1.2179 0.02959 0.02340 0.0356 0.0420 1.0000
13.750 1.2267 0.03099 0.02485 0.0364 0.0413 1.0000
14.000 1.2340 0.03259 0.02649 0.0372 0.0406 1.0000
14.250 1.2382 0.03452 0.02844 0.0379 0.0400 1.0000
14.500 1.2414 0.03663 0.03060 0.0387 0.0394 1.0000
14.750 1.2486 0.03845 0.03253 0.0389 0.0390 1.0000
15.000 1.2545 0.04045 0.03464 0.0390 0.0386 1.0000
15.250 1.2593 0.04262 0.03691 0.0390 0.0381 1.0000
15.500 1.2634 0.04493 0.03932 0.0388 0.0376 1.0000
15.750 1.2666 0.04737 0.04184 0.0384 0.0370 1.0000
16.000 1.2692 0.04992 0.04447 0.0379 0.0366 1.0000
16.250 1.2712 0.05260 0.04721 0.0374 0.0361 1.0000
16.500 1.2725 0.05536 0.05003 0.0367 0.0357 1.0000
16.750 1.2731 0.05822 0.05292 0.0362 0.0353 1.0000
17.000 1.2729 0.06107 0.05582 0.0359 0.0348 1.0000
17.250 1.2706 0.06434 0.05918 0.0353 0.0345 1.0000
17.500 1.2671 0.06811 0.06309 0.0337 0.0342 1.0000
17.750 1.2628 0.07208 0.06719 0.0320 0.0339 1.0000
18.000 1.2575 0.07625 0.07150 0.0301 0.0336 1.0000
18.250 1.2516 0.08057 0.07593 0.0282 0.0333 1.0000
18.500 1.2444 0.08518 0.08066 0.0260 0.0329 1.0000
18.750 1.2370 0.08991 0.08551 0.0237 0.0326 1.0000
19.000 1.2295 0.09472 0.09044 0.0213 0.0323 1.0000
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