NACA 23024 (naca23024-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 23024 (naca23024-il) Reynolds number: 200,000 Max Cl/Cd: 33.18 at α=8.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-naca23024-il-200000-n5.txt Download as CSV file: xf-naca23024-il-200000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NACA 23024
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
------ -------- --------- --------- -------- -------- --------
-19.750 -0.9467 0.09303 0.08617 -0.0654 1.0000 0.0895
-19.500 -0.9480 0.09008 0.08316 -0.0660 1.0000 0.0914
-19.250 -0.9490 0.08727 0.08035 -0.0664 1.0000 0.0930
-19.000 -0.9509 0.08433 0.07739 -0.0668 1.0000 0.0949
-18.750 -0.9526 0.08142 0.07442 -0.0672 1.0000 0.0970
-18.500 -0.9534 0.07867 0.07161 -0.0675 1.0000 0.0992
-18.250 -0.9563 0.07578 0.06872 -0.0677 1.0000 0.1011
-18.000 -0.9589 0.07292 0.06584 -0.0679 1.0000 0.1034
-17.750 -0.9600 0.07025 0.06311 -0.0679 1.0000 0.1060
-17.500 -0.9616 0.06762 0.06043 -0.0679 1.0000 0.1083
-17.250 -0.9654 0.06482 0.05763 -0.0678 1.0000 0.1109
-17.000 -0.9676 0.06221 0.05498 -0.0675 1.0000 0.1138
-16.750 -0.9673 0.05993 0.05264 -0.0671 1.0000 0.1166
-16.500 -0.9715 0.05728 0.05000 -0.0667 1.0000 0.1193
-16.250 -0.9742 0.05485 0.04753 -0.0661 1.0000 0.1227
-15.750 -0.9782 0.05037 0.04301 -0.0644 1.0000 0.1293
-15.500 -0.9804 0.04822 0.04084 -0.0634 1.0000 0.1329
-15.250 -0.9800 0.04639 0.03896 -0.0621 1.0000 0.1369
-15.000 -0.9843 0.04428 0.03686 -0.0607 1.0000 0.1407
-14.750 -0.9857 0.04249 0.03505 -0.0591 1.0000 0.1451
-14.500 -0.9869 0.04083 0.03337 -0.0574 1.0000 0.1492
-14.250 -0.9902 0.03913 0.03167 -0.0553 1.0000 0.1535
-14.000 -0.9907 0.03774 0.03025 -0.0532 1.0000 0.1584
-13.750 -0.9948 0.03625 0.02878 -0.0506 1.0000 0.1628
-13.500 -0.9978 0.03497 0.02749 -0.0479 1.0000 0.1677
-13.250 -1.0000 0.03386 0.02636 -0.0450 1.0000 0.1724
-13.000 -0.9911 0.03247 0.02498 -0.0444 0.9983 0.1786
-12.750 -0.9687 0.03125 0.02374 -0.0458 0.9946 0.1862
-12.500 -0.9487 0.02999 0.02249 -0.0468 0.9904 0.1939
-12.250 -0.9287 0.02887 0.02136 -0.0474 0.9857 0.2011
-12.000 -0.9071 0.02784 0.02033 -0.0482 0.9811 0.2092
-11.750 -0.8852 0.02687 0.01937 -0.0489 0.9768 0.2169
-11.500 -0.8672 0.02598 0.01846 -0.0486 0.9697 0.2243
-11.000 -0.8274 0.02436 0.01684 -0.0483 0.9567 0.2393
-10.750 -0.8037 0.02365 0.01612 -0.0486 0.9509 0.2467
-10.500 -0.7856 0.02294 0.01543 -0.0478 0.9432 0.2540
-10.250 -0.7625 0.02235 0.01479 -0.0476 0.9362 0.2614
-10.000 -0.7371 0.02164 0.01412 -0.0480 0.9317 0.2690
-9.750 -0.7197 0.02114 0.01358 -0.0466 0.9217 0.2761
-9.500 -0.6935 0.02052 0.01298 -0.0469 0.9159 0.2835
-9.250 -0.6644 0.01996 0.01241 -0.0476 0.9101 0.2918
-9.000 -0.6418 0.01950 0.01194 -0.0470 0.9004 0.2991
-8.750 -0.6086 0.01896 0.01141 -0.0485 0.8945 0.3073
-8.500 -0.5763 0.01853 0.01094 -0.0497 0.8866 0.3155
-8.250 -0.5480 0.01809 0.01053 -0.0502 0.8764 0.3233
-8.000 -0.5031 0.01765 0.01003 -0.0538 0.8694 0.3327
-7.750 -0.4745 0.01730 0.00971 -0.0542 0.8578 0.3400
-7.500 -0.4347 0.01692 0.00930 -0.0569 0.8471 0.3488
-7.250 -0.4055 0.01665 0.00898 -0.0573 0.8342 0.3561
-7.000 -0.3716 0.01633 0.00865 -0.0586 0.8213 0.3641
-6.750 -0.3489 0.01613 0.00839 -0.0577 0.8063 0.3716
-6.500 -0.3209 0.01589 0.00812 -0.0578 0.7926 0.3788
-6.250 -0.3004 0.01571 0.00791 -0.0563 0.7774 0.3860
-6.000 -0.2797 0.01557 0.00769 -0.0549 0.7632 0.3937
-5.750 -0.2574 0.01540 0.00748 -0.0537 0.7489 0.4006
-5.500 -0.2425 0.01527 0.00734 -0.0511 0.7341 0.4079
-5.250 -0.2233 0.01518 0.00714 -0.0492 0.7210 0.4155
-5.000 -0.2081 0.01506 0.00702 -0.0466 0.7071 0.4223
-4.750 -0.1919 0.01497 0.00689 -0.0441 0.6945 0.4300
-4.500 -0.1774 0.01491 0.00676 -0.0413 0.6817 0.4378
-4.250 -0.1622 0.01482 0.00667 -0.0387 0.6696 0.4451
-4.000 -0.1488 0.01476 0.00659 -0.0356 0.6573 0.4528
-3.500 -0.1211 0.01467 0.00644 -0.0296 0.6341 0.4684
-3.250 -0.1072 0.01464 0.00637 -0.0266 0.6234 0.4765
-3.000 -0.0956 0.01463 0.00633 -0.0231 0.6120 0.4845
-2.500 -0.0716 0.01460 0.00629 -0.0163 0.5910 0.5012
-2.250 -0.0582 0.01460 0.00624 -0.0132 0.5802 0.5093
-2.000 -0.0450 0.01458 0.00624 -0.0100 0.5701 0.5182
-1.750 -0.0326 0.01459 0.00621 -0.0067 0.5593 0.5276
-1.500 -0.0183 0.01458 0.00620 -0.0038 0.5495 0.5360
-1.250 -0.0058 0.01457 0.00620 -0.0005 0.5389 0.5454
-1.000 0.0077 0.01460 0.00617 0.0026 0.5293 0.5546
-0.750 0.0206 0.01458 0.00620 0.0058 0.5192 0.5642
-0.500 0.0328 0.01461 0.00618 0.0092 0.5098 0.5743
-0.250 0.0464 0.01460 0.00621 0.0122 0.5010 0.5841
0.000 0.0569 0.01460 0.00622 0.0159 0.4915 0.5944
0.250 0.0687 0.01463 0.00622 0.0193 0.4832 0.6045
0.500 0.0807 0.01462 0.00627 0.0227 0.4743 0.6155
0.750 0.0923 0.01466 0.00629 0.0262 0.4660 0.6265
1.000 0.1064 0.01470 0.00636 0.0291 0.4582 0.6380
1.500 0.1329 0.01481 0.00650 0.0352 0.4415 0.6610
1.750 0.1456 0.01487 0.00657 0.0383 0.4336 0.6735
2.000 0.1614 0.01494 0.00670 0.0408 0.4250 0.6857
2.500 0.1920 0.01512 0.00694 0.0460 0.4092 0.7122
2.750 0.2058 0.01523 0.00706 0.0488 0.4011 0.7255
3.000 0.2241 0.01536 0.00723 0.0507 0.3938 0.7399
3.250 0.2429 0.01549 0.00741 0.0524 0.3855 0.7537
3.500 0.2591 0.01565 0.00758 0.0547 0.3778 0.7688
3.750 0.2835 0.01583 0.00783 0.0552 0.3696 0.7830
4.000 0.3038 0.01603 0.00805 0.0566 0.3615 0.7981
4.250 0.3293 0.01628 0.00831 0.0568 0.3539 0.8126
4.500 0.3590 0.01653 0.00861 0.0561 0.3451 0.8261
4.750 0.3830 0.01683 0.00889 0.0565 0.3372 0.8406
5.000 0.4234 0.01719 0.00929 0.0536 0.3284 0.8514
5.250 0.4543 0.01756 0.00965 0.0525 0.3201 0.8639
5.500 0.4949 0.01799 0.01008 0.0495 0.3119 0.8722
5.750 0.5338 0.01845 0.01055 0.0467 0.3034 0.8804
6.000 0.5572 0.01890 0.01095 0.0470 0.2970 0.8916
6.250 0.5969 0.01941 0.01150 0.0441 0.2890 0.8968
6.500 0.6270 0.01996 0.01202 0.0430 0.2820 0.9039
6.750 0.6493 0.02044 0.01251 0.0434 0.2761 0.9133
7.000 0.6818 0.02103 0.01310 0.0418 0.2693 0.9178
7.250 0.7059 0.02164 0.01368 0.0417 0.2639 0.9247
7.500 0.7266 0.02219 0.01424 0.0423 0.2589 0.9330
7.750 0.7540 0.02281 0.01487 0.0414 0.2531 0.9379
8.000 0.7710 0.02344 0.01548 0.0425 0.2486 0.9474
8.250 0.7969 0.02413 0.01615 0.0417 0.2439 0.9521
8.500 0.8216 0.02476 0.01682 0.0412 0.2390 0.9585
8.750 0.8415 0.02547 0.01752 0.0414 0.2344 0.9656
9.000 0.8650 0.02628 0.01829 0.0406 0.2300 0.9706
9.250 0.8857 0.02701 0.01907 0.0407 0.2261 0.9777
9.500 0.9133 0.02773 0.01982 0.0392 0.2217 0.9811
9.750 0.9380 0.02856 0.02065 0.0380 0.2177 0.9855
10.000 0.9601 0.02951 0.02155 0.0372 0.2141 0.9900
10.250 0.9860 0.03033 0.02245 0.0358 0.2100 0.9938
10.500 1.0116 0.03122 0.02338 0.0342 0.2059 0.9975
10.750 1.0340 0.03222 0.02437 0.0330 0.2024 1.0000
11.000 1.0337 0.03310 0.02520 0.0359 0.1999 1.0000
11.250 1.0370 0.03389 0.02606 0.0384 0.1973 1.0000
11.500 1.0398 0.03480 0.02702 0.0408 0.1944 1.0000
11.750 1.0426 0.03579 0.02803 0.0430 0.1918 1.0000
12.000 1.0449 0.03688 0.02911 0.0451 0.1891 1.0000
12.250 1.0474 0.03803 0.03023 0.0470 0.1866 1.0000
12.500 1.0522 0.03915 0.03141 0.0487 0.1842 1.0000
12.750 1.0559 0.04040 0.03273 0.0502 0.1814 1.0000
13.000 1.0596 0.04171 0.03408 0.0517 0.1787 1.0000
13.250 1.0622 0.04315 0.03552 0.0531 0.1761 1.0000
13.500 1.0664 0.04450 0.03686 0.0543 0.1740 1.0000
13.750 1.0698 0.04603 0.03844 0.0554 0.1715 1.0000
14.000 1.0727 0.04766 0.04015 0.0563 0.1688 1.0000
14.250 1.0746 0.04943 0.04197 0.0572 0.1662 1.0000
14.500 1.0771 0.05118 0.04374 0.0580 0.1638 1.0000
14.750 1.0808 0.05284 0.04537 0.0587 0.1617 1.0000
15.000 1.0824 0.05482 0.04743 0.0592 0.1593 1.0000
15.250 1.0825 0.05701 0.04972 0.0596 0.1566 1.0000
15.500 1.0833 0.05916 0.05193 0.0600 0.1543 1.0000
15.750 1.0845 0.06130 0.05408 0.0602 0.1521 1.0000
16.000 1.0880 0.06316 0.05591 0.0605 0.1500 1.0000
16.250 1.0855 0.06587 0.05875 0.0605 0.1477 1.0000
16.500 1.0829 0.06863 0.06160 0.0604 0.1452 1.0000
16.750 1.0810 0.07132 0.06435 0.0602 0.1428 1.0000
17.000 1.0808 0.07383 0.06687 0.0600 0.1407 1.0000
17.250 1.0808 0.07634 0.06940 0.0597 0.1385 1.0000
17.500 1.0728 0.07999 0.07318 0.0590 0.1360 1.0000
17.750 1.0668 0.08341 0.07669 0.0583 0.1336 1.0000
18.000 1.0644 0.08639 0.07970 0.0577 0.1315 1.0000
18.250 1.0681 0.08854 0.08182 0.0574 0.1296 1.0000
18.500 1.0565 0.09285 0.08627 0.0562 0.1273 1.0000
18.750 1.0444 0.09730 0.09084 0.0549 0.1249 1.0000
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