NACA 0015 (naca0015-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 0015 (naca0015-il) Reynolds number: 200,000 Max Cl/Cd: 48.6 at α=7° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-naca0015-il-200000-n5.txt Download as CSV file: xf-naca0015-il-200000-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 = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.000 -0.9801 0.14046 0.13585 0.0034 1.0000 0.0373
-18.750 -1.0458 0.12227 0.11729 -0.0078 1.0000 0.0375
-18.500 -1.0733 0.11293 0.10772 -0.0134 1.0000 0.0377
-18.250 -1.0940 0.10521 0.09979 -0.0178 1.0000 0.0380
-18.000 -1.1109 0.09843 0.09280 -0.0216 1.0000 0.0383
-17.750 -1.1252 0.09230 0.08648 -0.0248 1.0000 0.0387
-17.500 -1.1377 0.08660 0.08057 -0.0278 1.0000 0.0390
-17.250 -1.1393 0.08304 0.07698 -0.0291 1.0000 0.0394
-17.000 -1.1419 0.07930 0.07318 -0.0306 1.0000 0.0398
-16.750 -1.1449 0.07551 0.06932 -0.0322 1.0000 0.0402
-16.500 -1.1480 0.07176 0.06548 -0.0337 1.0000 0.0407
-16.250 -1.1510 0.06809 0.06171 -0.0351 1.0000 0.0412
-16.000 -1.1536 0.06457 0.05808 -0.0363 1.0000 0.0417
-15.750 -1.1554 0.06122 0.05461 -0.0374 1.0000 0.0422
-15.500 -1.1563 0.05807 0.05133 -0.0382 1.0000 0.0427
-15.250 -1.1563 0.05510 0.04823 -0.0389 1.0000 0.0432
-15.000 -1.1554 0.05229 0.04528 -0.0394 1.0000 0.0438
-14.750 -1.1533 0.04965 0.04248 -0.0398 1.0000 0.0445
-14.500 -1.1509 0.04721 0.04000 -0.0399 1.0000 0.0450
-14.250 -1.1479 0.04487 0.03761 -0.0400 1.0000 0.0457
-14.000 -1.1439 0.04268 0.03536 -0.0399 1.0000 0.0464
-13.750 -1.1390 0.04065 0.03325 -0.0397 1.0000 0.0471
-13.500 -1.1334 0.03875 0.03126 -0.0393 1.0000 0.0479
-13.250 -1.1270 0.03698 0.02940 -0.0387 1.0000 0.0487
-13.000 -1.1198 0.03534 0.02766 -0.0379 1.0000 0.0496
-12.750 -1.1115 0.03385 0.02605 -0.0370 1.0000 0.0505
-12.500 -1.1053 0.03230 0.02446 -0.0359 1.0000 0.0515
-12.250 -1.0980 0.03091 0.02304 -0.0346 1.0000 0.0525
-12.000 -1.0892 0.02970 0.02178 -0.0333 1.0000 0.0538
-11.750 -1.0794 0.02861 0.02061 -0.0318 1.0000 0.0552
-11.500 -1.0689 0.02761 0.01953 -0.0301 1.0000 0.0567
-11.250 -1.0591 0.02663 0.01849 -0.0282 1.0000 0.0582
-11.000 -1.0505 0.02568 0.01752 -0.0260 1.0000 0.0597
-10.750 -1.0405 0.02487 0.01669 -0.0238 1.0000 0.0616
-10.500 -1.0298 0.02417 0.01593 -0.0214 1.0000 0.0638
-10.250 -1.0186 0.02350 0.01520 -0.0190 1.0000 0.0662
-10.000 -1.0068 0.02279 0.01451 -0.0167 1.0000 0.0689
-9.750 -0.9928 0.02220 0.01387 -0.0146 1.0000 0.0724
-9.500 -0.9793 0.02160 0.01326 -0.0124 1.0000 0.0758
-9.250 -0.9658 0.02102 0.01269 -0.0102 1.0000 0.0797
-9.000 -0.9508 0.02054 0.01215 -0.0081 1.0000 0.0841
-8.750 -0.9374 0.01999 0.01163 -0.0058 1.0000 0.0888
-8.500 -0.9218 0.01955 0.01116 -0.0037 1.0000 0.0943
-8.250 -0.9076 0.01905 0.01070 -0.0015 1.0000 0.1002
-8.000 -0.8917 0.01865 0.01028 0.0006 1.0000 0.1068
-7.750 -0.8768 0.01819 0.00987 0.0027 1.0000 0.1141
-7.500 -0.8609 0.01781 0.00949 0.0047 1.0000 0.1215
-7.250 -0.8448 0.01743 0.00913 0.0067 1.0000 0.1301
-7.000 -0.8287 0.01706 0.00880 0.0087 1.0000 0.1392
-6.750 -0.8042 0.01666 0.00844 0.0090 0.9982 0.1509
-6.500 -0.7699 0.01623 0.00807 0.0072 0.9942 0.1663
-6.250 -0.7365 0.01579 0.00771 0.0057 0.9897 0.1839
-6.000 -0.7027 0.01538 0.00738 0.0040 0.9848 0.2034
-5.750 -0.6673 0.01500 0.00707 0.0021 0.9807 0.2242
-5.500 -0.6355 0.01462 0.00678 0.0011 0.9743 0.2438
-5.250 -0.6000 0.01425 0.00650 -0.0008 0.9698 0.2648
-5.000 -0.5678 0.01391 0.00624 -0.0018 0.9633 0.2849
-4.750 -0.5343 0.01360 0.00599 -0.0031 0.9571 0.3057
-4.500 -0.5021 0.01330 0.00576 -0.0041 0.9501 0.3259
-4.250 -0.4707 0.01301 0.00554 -0.0048 0.9420 0.3461
-4.000 -0.4399 0.01273 0.00534 -0.0054 0.9336 0.3668
-3.750 -0.4094 0.01246 0.00514 -0.0059 0.9244 0.3880
-3.500 -0.3804 0.01222 0.00497 -0.0060 0.9139 0.4091
-3.250 -0.3493 0.01198 0.00478 -0.0065 0.9045 0.4310
-3.000 -0.3220 0.01177 0.00464 -0.0062 0.8916 0.4518
-2.750 -0.2939 0.01156 0.00449 -0.0061 0.8792 0.4723
-2.500 -0.2655 0.01136 0.00434 -0.0059 0.8663 0.4924
-2.250 -0.2381 0.01118 0.00421 -0.0055 0.8518 0.5123
-2.000 -0.2112 0.01103 0.00410 -0.0050 0.8360 0.5320
-1.750 -0.1845 0.01089 0.00399 -0.0045 0.8197 0.5519
-1.500 -0.1578 0.01078 0.00390 -0.0039 0.8027 0.5719
-1.250 -0.1313 0.01068 0.00382 -0.0033 0.7851 0.5918
-1.000 -0.1049 0.01060 0.00375 -0.0027 0.7670 0.6117
-0.750 -0.0786 0.01054 0.00370 -0.0020 0.7485 0.6317
-0.500 -0.0523 0.01050 0.00366 -0.0014 0.7296 0.6515
-0.250 -0.0262 0.01047 0.00364 -0.0007 0.7104 0.6713
0.000 0.0000 0.01046 0.00364 0.0000 0.6910 0.6910
0.250 0.0262 0.01047 0.00364 0.0007 0.6712 0.7104
0.500 0.0523 0.01050 0.00366 0.0014 0.6515 0.7296
0.750 0.0786 0.01054 0.00370 0.0020 0.6316 0.7485
1.000 0.1049 0.01060 0.00375 0.0027 0.6117 0.7670
1.250 0.1313 0.01068 0.00382 0.0033 0.5918 0.7851
1.500 0.1578 0.01078 0.00390 0.0039 0.5720 0.8027
1.750 0.1845 0.01089 0.00399 0.0045 0.5520 0.8197
2.000 0.2112 0.01103 0.00410 0.0050 0.5320 0.8360
2.250 0.2380 0.01118 0.00421 0.0055 0.5123 0.8518
2.500 0.2655 0.01136 0.00434 0.0059 0.4924 0.8663
2.750 0.2939 0.01156 0.00449 0.0061 0.4722 0.8792
3.000 0.3220 0.01177 0.00464 0.0062 0.4518 0.8916
3.250 0.3493 0.01198 0.00478 0.0065 0.4310 0.9045
3.500 0.3804 0.01222 0.00497 0.0060 0.4091 0.9139
3.750 0.4094 0.01246 0.00514 0.0059 0.3880 0.9244
4.000 0.4399 0.01273 0.00534 0.0054 0.3668 0.9337
4.250 0.4707 0.01301 0.00554 0.0048 0.3461 0.9420
4.500 0.5021 0.01330 0.00576 0.0041 0.3259 0.9501
4.750 0.5343 0.01360 0.00599 0.0031 0.3057 0.9571
5.000 0.5678 0.01391 0.00624 0.0018 0.2849 0.9633
5.250 0.6000 0.01425 0.00650 0.0008 0.2647 0.9698
5.500 0.6355 0.01461 0.00677 -0.0011 0.2438 0.9743
5.750 0.6673 0.01499 0.00707 -0.0021 0.2242 0.9808
6.000 0.7028 0.01538 0.00738 -0.0041 0.2034 0.9848
6.250 0.7366 0.01579 0.00771 -0.0057 0.1839 0.9897
6.500 0.7699 0.01622 0.00806 -0.0072 0.1663 0.9942
6.750 0.8042 0.01666 0.00844 -0.0090 0.1508 0.9983
7.000 0.8286 0.01705 0.00879 -0.0087 0.1392 1.0000
7.250 0.8447 0.01743 0.00913 -0.0067 0.1302 1.0000
7.500 0.8608 0.01781 0.00949 -0.0047 0.1215 1.0000
7.750 0.8767 0.01819 0.00987 -0.0027 0.1140 1.0000
8.000 0.8916 0.01865 0.01028 -0.0005 0.1068 1.0000
8.250 0.9075 0.01905 0.01070 0.0015 0.1002 1.0000
8.500 0.9218 0.01955 0.01116 0.0037 0.0943 1.0000
8.750 0.9374 0.01998 0.01163 0.0058 0.0888 1.0000
9.000 0.9508 0.02054 0.01215 0.0081 0.0841 1.0000
9.250 0.9658 0.02102 0.01268 0.0102 0.0797 1.0000
9.500 0.9794 0.02160 0.01325 0.0124 0.0758 1.0000
9.750 0.9930 0.02220 0.01387 0.0146 0.0723 1.0000
10.000 1.0070 0.02279 0.01450 0.0167 0.0689 1.0000
10.250 1.0189 0.02350 0.01521 0.0189 0.0662 1.0000
10.500 1.0302 0.02417 0.01592 0.0213 0.0638 1.0000
10.750 1.0409 0.02487 0.01669 0.0237 0.0615 1.0000
11.000 1.0510 0.02567 0.01752 0.0259 0.0597 1.0000
11.250 1.0596 0.02663 0.01848 0.0281 0.0581 1.0000
11.500 1.0696 0.02760 0.01952 0.0300 0.0567 1.0000
11.750 1.0801 0.02860 0.02061 0.0316 0.0552 1.0000
12.000 1.0899 0.02970 0.02177 0.0331 0.0538 1.0000
12.250 1.0988 0.03091 0.02303 0.0345 0.0525 1.0000
12.500 1.1062 0.03229 0.02445 0.0358 0.0515 1.0000
12.750 1.1126 0.03384 0.02604 0.0369 0.0505 1.0000
13.000 1.1209 0.03532 0.02764 0.0378 0.0496 1.0000
13.250 1.1282 0.03696 0.02938 0.0385 0.0487 1.0000
13.500 1.1346 0.03873 0.03124 0.0391 0.0479 1.0000
13.750 1.1404 0.04062 0.03322 0.0395 0.0471 1.0000
14.000 1.1454 0.04265 0.03533 0.0397 0.0463 1.0000
14.250 1.1494 0.04483 0.03758 0.0398 0.0457 1.0000
14.500 1.1525 0.04717 0.03996 0.0397 0.0450 1.0000
14.750 1.1550 0.04962 0.04245 0.0396 0.0444 1.0000
15.000 1.1572 0.05225 0.04524 0.0392 0.0438 1.0000
15.250 1.1582 0.05506 0.04819 0.0386 0.0432 1.0000
15.500 1.1583 0.05802 0.05128 0.0380 0.0427 1.0000
15.750 1.1575 0.06117 0.05456 0.0371 0.0421 1.0000
16.000 1.1557 0.06451 0.05802 0.0361 0.0416 1.0000
16.250 1.1532 0.06803 0.06164 0.0348 0.0411 1.0000
16.500 1.1504 0.07168 0.06540 0.0334 0.0407 1.0000
16.750 1.1474 0.07543 0.06923 0.0319 0.0402 1.0000
17.000 1.1445 0.07920 0.07308 0.0304 0.0398 1.0000
17.250 1.1420 0.08292 0.07685 0.0288 0.0394 1.0000
17.500 1.1397 0.08661 0.08059 0.0274 0.0390 1.0000
17.750 1.1274 0.09229 0.08647 0.0245 0.0386 1.0000
18.000 1.1130 0.09845 0.09284 0.0212 0.0383 1.0000
18.250 1.0962 0.10522 0.09980 0.0175 0.0380 1.0000
18.500 1.0753 0.11301 0.10780 0.0130 0.0377 1.0000
18.750 1.0476 0.12239 0.11741 0.0074 0.0374 1.0000
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