NACA 63(3)-018 (naca633018-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 63(3)-018 (naca633018-il) Reynolds number: 200,000 Max Cl/Cd: 50.2 at α=6.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-naca633018-il-200000-n5.txt Download as CSV file: xf-naca633018-il-200000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NACA 63(3)-018
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 -1.0705 0.12223 0.11730 0.0005 1.0000 0.0302
-19.500 -1.0733 0.11775 0.11278 -0.0021 1.0000 0.0308
-19.250 -1.0771 0.11308 0.10803 -0.0048 1.0000 0.0314
-19.000 -1.0810 0.10842 0.10329 -0.0075 1.0000 0.0322
-18.750 -1.0847 0.10387 0.09862 -0.0100 1.0000 0.0329
-18.500 -1.0884 0.09939 0.09401 -0.0123 1.0000 0.0338
-18.250 -1.0917 0.09504 0.08951 -0.0145 1.0000 0.0347
-18.000 -1.0940 0.09095 0.08525 -0.0164 1.0000 0.0355
-17.750 -1.0961 0.08692 0.08103 -0.0183 1.0000 0.0363
-17.500 -1.0939 0.08380 0.07788 -0.0195 1.0000 0.0371
-17.250 -1.0928 0.08050 0.07453 -0.0210 1.0000 0.0379
-17.000 -1.0909 0.07734 0.07130 -0.0223 1.0000 0.0388
-16.750 -1.0885 0.07429 0.06815 -0.0235 1.0000 0.0399
-16.500 -1.0856 0.07135 0.06509 -0.0246 1.0000 0.0410
-16.250 -1.0823 0.06850 0.06210 -0.0256 1.0000 0.0422
-16.000 -1.0786 0.06576 0.05918 -0.0266 1.0000 0.0432
-15.750 -1.0730 0.06344 0.05687 -0.0270 1.0000 0.0444
-15.500 -1.0677 0.06105 0.05445 -0.0277 1.0000 0.0456
-15.250 -1.0616 0.05879 0.05213 -0.0283 1.0000 0.0468
-15.000 -1.0547 0.05666 0.04993 -0.0287 1.0000 0.0480
-14.750 -1.0465 0.05470 0.04787 -0.0289 1.0000 0.0491
-14.500 -1.0374 0.05287 0.04594 -0.0291 1.0000 0.0502
-14.250 -1.0279 0.05109 0.04406 -0.0292 1.0000 0.0511
-14.000 -1.0182 0.04941 0.04234 -0.0291 1.0000 0.0521
-13.750 -1.0101 0.04763 0.04056 -0.0290 1.0000 0.0532
-13.500 -1.0018 0.04587 0.03878 -0.0289 1.0000 0.0543
-13.250 -0.9929 0.04419 0.03706 -0.0288 1.0000 0.0554
-13.000 -0.9838 0.04258 0.03539 -0.0287 1.0000 0.0567
-12.750 -0.9743 0.04103 0.03378 -0.0285 1.0000 0.0580
-12.500 -0.9641 0.03955 0.03224 -0.0283 1.0000 0.0594
-12.250 -0.9537 0.03811 0.03073 -0.0280 1.0000 0.0606
-12.000 -0.9461 0.03647 0.02908 -0.0276 1.0000 0.0620
-11.750 -0.9393 0.03479 0.02739 -0.0272 1.0000 0.0635
-11.500 -0.9311 0.03325 0.02583 -0.0268 1.0000 0.0652
-11.250 -0.9218 0.03181 0.02436 -0.0264 1.0000 0.0671
-11.000 -0.9114 0.03048 0.02299 -0.0260 1.0000 0.0694
-10.750 -0.9002 0.02921 0.02168 -0.0256 1.0000 0.0718
-10.500 -0.8929 0.02774 0.02023 -0.0252 0.9601 0.0748
-10.250 -0.8709 0.02639 0.01880 -0.0271 0.9201 0.0793
-10.000 -0.8580 0.02534 0.01762 -0.0266 0.8950 0.0837
-9.500 -0.8424 0.02321 0.01538 -0.0236 0.8610 0.0953
-9.250 -0.8361 0.02216 0.01432 -0.0218 0.8476 0.1035
-9.000 -0.8296 0.02122 0.01336 -0.0198 0.8357 0.1137
-8.750 -0.8241 0.02032 0.01244 -0.0174 0.8251 0.1267
-8.500 -0.8192 0.01946 0.01160 -0.0148 0.8146 0.1418
-8.250 -0.8147 0.01872 0.01090 -0.0118 0.8054 0.1597
-8.000 -0.8058 0.01798 0.01021 -0.0095 0.7968 0.1827
-7.750 -0.7955 0.01720 0.00954 -0.0074 0.7888 0.2102
-7.500 -0.7834 0.01646 0.00891 -0.0056 0.7811 0.2424
-7.250 -0.7697 0.01575 0.00833 -0.0038 0.7741 0.2786
-7.000 -0.7540 0.01510 0.00785 -0.0024 0.7665 0.3180
-6.750 -0.7353 0.01464 0.00748 -0.0012 0.7605 0.3539
-6.500 -0.7133 0.01431 0.00723 -0.0005 0.7532 0.3828
-6.250 -0.6899 0.01408 0.00699 0.0001 0.7470 0.4054
-6.000 -0.6654 0.01390 0.00680 0.0006 0.7408 0.4247
-5.750 -0.6402 0.01375 0.00664 0.0009 0.7341 0.4432
-5.500 -0.6153 0.01365 0.00650 0.0014 0.7286 0.4635
-5.250 -0.5894 0.01358 0.00641 0.0017 0.7223 0.4814
-5.000 -0.5628 0.01351 0.00633 0.0019 0.7160 0.4929
-4.750 -0.5359 0.01345 0.00618 0.0021 0.7110 0.5019
-4.500 -0.5086 0.01339 0.00607 0.0020 0.7047 0.5124
-4.250 -0.4811 0.01335 0.00602 0.0022 0.6989 0.5213
-3.750 -0.4257 0.01323 0.00579 0.0021 0.6877 0.5353
-3.500 -0.3977 0.01317 0.00566 0.0021 0.6822 0.5415
-3.250 -0.3699 0.01311 0.00550 0.0020 0.6777 0.5475
-3.000 -0.3415 0.01306 0.00546 0.0019 0.6718 0.5526
-2.750 -0.3133 0.01300 0.00535 0.0018 0.6661 0.5584
-2.500 -0.2852 0.01295 0.00520 0.0017 0.6615 0.5637
-2.250 -0.2566 0.01291 0.00518 0.0015 0.6561 0.5681
-2.000 -0.2282 0.01287 0.00511 0.0014 0.6507 0.5733
-1.750 -0.1999 0.01283 0.00497 0.0012 0.6460 0.5788
-1.500 -0.1713 0.01279 0.00496 0.0011 0.6409 0.5828
-1.250 -0.1428 0.01277 0.00493 0.0009 0.6355 0.5875
-1.000 -0.1143 0.01274 0.00485 0.0007 0.6309 0.5929
-0.750 -0.0858 0.01272 0.00480 0.0006 0.6265 0.5973
-0.500 -0.0571 0.01271 0.00483 0.0004 0.6208 0.6016
-0.250 -0.0286 0.01270 0.00480 0.0002 0.6160 0.6068
0.000 0.0000 0.01270 0.00474 0.0000 0.6120 0.6120
0.250 0.0286 0.01270 0.00480 -0.0002 0.6068 0.6160
0.500 0.0571 0.01271 0.00483 -0.0004 0.6016 0.6209
0.750 0.0858 0.01272 0.00480 -0.0006 0.5973 0.6265
1.000 0.1143 0.01274 0.00485 -0.0007 0.5929 0.6309
1.250 0.1428 0.01277 0.00493 -0.0009 0.5875 0.6355
1.500 0.1713 0.01279 0.00496 -0.0011 0.5828 0.6409
1.750 0.1999 0.01283 0.00497 -0.0012 0.5788 0.6460
2.000 0.2282 0.01287 0.00511 -0.0014 0.5733 0.6507
2.250 0.2566 0.01291 0.00518 -0.0015 0.5681 0.6561
2.500 0.2852 0.01295 0.00520 -0.0017 0.5637 0.6615
2.750 0.3133 0.01300 0.00535 -0.0018 0.5583 0.6661
3.000 0.3415 0.01306 0.00546 -0.0019 0.5526 0.6718
3.250 0.3699 0.01311 0.00550 -0.0020 0.5475 0.6777
3.500 0.3977 0.01317 0.00566 -0.0021 0.5415 0.6822
3.750 0.4257 0.01323 0.00578 -0.0021 0.5353 0.6877
4.250 0.4811 0.01335 0.00602 -0.0022 0.5213 0.6989
4.500 0.5086 0.01339 0.00607 -0.0020 0.5124 0.7047
4.750 0.5359 0.01344 0.00617 -0.0021 0.5019 0.7109
5.000 0.5628 0.01351 0.00633 -0.0019 0.4929 0.7160
5.250 0.5894 0.01358 0.00641 -0.0017 0.4815 0.7223
5.500 0.6153 0.01365 0.00650 -0.0014 0.4636 0.7286
5.750 0.6402 0.01375 0.00664 -0.0009 0.4431 0.7341
6.000 0.6654 0.01390 0.00680 -0.0006 0.4245 0.7408
6.250 0.6900 0.01408 0.00699 -0.0001 0.4053 0.7469
6.500 0.7134 0.01431 0.00723 0.0005 0.3828 0.7532
6.750 0.7354 0.01465 0.00748 0.0012 0.3537 0.7605
7.000 0.7541 0.01510 0.00785 0.0024 0.3183 0.7665
7.250 0.7698 0.01574 0.00833 0.0038 0.2788 0.7741
7.500 0.7835 0.01646 0.00891 0.0055 0.2424 0.7811
7.750 0.7955 0.01721 0.00954 0.0074 0.2100 0.7888
8.000 0.8059 0.01798 0.01021 0.0095 0.1827 0.7969
8.250 0.8149 0.01872 0.01090 0.0118 0.1598 0.8055
8.500 0.8194 0.01946 0.01160 0.0148 0.1418 0.8146
8.750 0.8241 0.02032 0.01244 0.0174 0.1263 0.8251
9.000 0.8299 0.02122 0.01335 0.0197 0.1138 0.8357
9.250 0.8363 0.02216 0.01432 0.0218 0.1034 0.8476
9.500 0.8427 0.02320 0.01537 0.0236 0.0954 0.8611
10.000 0.8584 0.02533 0.01761 0.0265 0.0837 0.8951
10.250 0.8715 0.02637 0.01877 0.0270 0.0794 0.9200
10.500 0.8935 0.02773 0.02022 0.0250 0.0746 0.9606
10.750 0.9008 0.02920 0.02167 0.0255 0.0718 1.0000
11.000 0.9122 0.03044 0.02295 0.0259 0.0693 1.0000
11.250 0.9225 0.03179 0.02434 0.0263 0.0671 1.0000
11.500 0.9320 0.03322 0.02580 0.0267 0.0652 1.0000
11.750 0.9401 0.03476 0.02736 0.0271 0.0635 1.0000
12.000 0.9470 0.03644 0.02904 0.0275 0.0620 1.0000
12.250 0.9547 0.03807 0.03068 0.0279 0.0606 1.0000
12.500 0.9652 0.03950 0.03219 0.0282 0.0594 1.0000
12.750 0.9752 0.04099 0.03374 0.0284 0.0579 1.0000
13.000 0.9848 0.04254 0.03535 0.0286 0.0566 1.0000
13.250 0.9939 0.04415 0.03702 0.0287 0.0554 1.0000
13.500 1.0028 0.04583 0.03873 0.0288 0.0543 1.0000
13.750 1.0113 0.04757 0.04049 0.0289 0.0532 1.0000
14.000 1.0195 0.04935 0.04227 0.0290 0.0521 1.0000
14.250 1.0291 0.05104 0.04400 0.0291 0.0511 1.0000
14.500 1.0386 0.05280 0.04587 0.0290 0.0502 1.0000
14.750 1.0477 0.05464 0.04782 0.0288 0.0491 1.0000
15.000 1.0558 0.05660 0.04987 0.0286 0.0480 1.0000
15.250 1.0630 0.05869 0.05204 0.0282 0.0468 1.0000
15.500 1.0688 0.06099 0.05439 0.0276 0.0455 1.0000
15.750 1.0743 0.06334 0.05677 0.0269 0.0444 1.0000
16.000 1.0798 0.06568 0.05910 0.0264 0.0432 1.0000
16.250 1.0837 0.06842 0.06201 0.0255 0.0421 1.0000
16.500 1.0869 0.07128 0.06502 0.0245 0.0409 1.0000
16.750 1.0900 0.07419 0.06804 0.0234 0.0398 1.0000
17.000 1.0920 0.07730 0.07125 0.0221 0.0387 1.0000
17.250 1.0942 0.08042 0.07444 0.0208 0.0378 1.0000
17.500 1.0955 0.08370 0.07777 0.0194 0.0370 1.0000
17.750 1.0974 0.08688 0.08097 0.0181 0.0362 1.0000
18.000 1.0957 0.09085 0.08515 0.0163 0.0355 1.0000
18.250 1.0932 0.09497 0.08944 0.0143 0.0346 1.0000
18.500 1.0901 0.09927 0.09389 0.0122 0.0337 1.0000
18.750 1.0865 0.10373 0.09848 0.0098 0.0329 1.0000
19.000 1.0828 0.10831 0.10317 0.0073 0.0321 1.0000
19.250 1.0790 0.11295 0.10790 0.0047 0.0314 1.0000
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