NACA 63 (naca633418-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 63 (naca633418-il) Reynolds number: 200,000 Max Cl/Cd: 67.79 at α=7.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-naca633418-il-200000-n5.txt Download as CSV file: xf-naca633418-il-200000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NACA 63
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
------ -------- --------- --------- -------- -------- --------
-18.500 -0.7562 0.12045 0.11584 -0.0421 1.0000 0.0276
-18.250 -0.7999 0.10742 0.10252 -0.0501 1.0000 0.0276
-18.000 -0.8259 0.09869 0.09354 -0.0553 1.0000 0.0277
-17.750 -0.8448 0.09158 0.08622 -0.0595 1.0000 0.0279
-17.500 -0.8565 0.08604 0.08051 -0.0625 1.0000 0.0280
-17.250 -0.8572 0.08251 0.07694 -0.0642 1.0000 0.0284
-17.000 -0.8597 0.07872 0.07308 -0.0660 1.0000 0.0286
-16.750 -0.8618 0.07507 0.06935 -0.0678 1.0000 0.0289
-16.500 -0.8634 0.07158 0.06577 -0.0693 1.0000 0.0292
-16.250 -0.8646 0.06823 0.06232 -0.0708 1.0000 0.0295
-16.000 -0.8650 0.06505 0.05904 -0.0720 1.0000 0.0299
-15.750 -0.8650 0.06203 0.05592 -0.0731 1.0000 0.0303
-15.500 -0.8638 0.05922 0.05299 -0.0740 1.0000 0.0307
-15.250 -0.8628 0.05645 0.05008 -0.0748 1.0000 0.0314
-15.000 -0.8599 0.05399 0.04748 -0.0754 1.0000 0.0319
-14.750 -0.8565 0.05165 0.04502 -0.0758 1.0000 0.0325
-14.500 -0.8506 0.04972 0.04308 -0.0759 1.0000 0.0330
-14.250 -0.8450 0.04782 0.04116 -0.0761 1.0000 0.0336
-14.000 -0.8390 0.04600 0.03930 -0.0762 1.0000 0.0342
-13.750 -0.8326 0.04424 0.03748 -0.0761 1.0000 0.0350
-13.500 -0.8254 0.04258 0.03576 -0.0759 1.0000 0.0356
-13.250 -0.8180 0.04100 0.03409 -0.0756 1.0000 0.0365
-13.000 -0.8098 0.03951 0.03251 -0.0752 1.0000 0.0373
-12.750 -0.8031 0.03800 0.03100 -0.0746 1.0000 0.0380
-12.500 -0.7964 0.03656 0.02956 -0.0741 1.0000 0.0388
-12.250 -0.7895 0.03522 0.02821 -0.0734 1.0000 0.0398
-12.000 -0.7828 0.03396 0.02693 -0.0725 1.0000 0.0409
-11.750 -0.7742 0.03276 0.02568 -0.0718 0.9987 0.0421
-11.500 -0.7469 0.03113 0.02400 -0.0750 0.9658 0.0438
-11.250 -0.7180 0.02962 0.02243 -0.0784 0.9451 0.0456
-11.000 -0.6893 0.02829 0.02099 -0.0814 0.9270 0.0480
-10.750 -0.6660 0.02704 0.01964 -0.0832 0.9095 0.0501
-10.500 -0.6486 0.02588 0.01841 -0.0839 0.8930 0.0523
-10.250 -0.6325 0.02490 0.01734 -0.0839 0.8789 0.0549
-10.000 -0.6190 0.02397 0.01631 -0.0833 0.8662 0.0573
-9.750 -0.6090 0.02302 0.01532 -0.0822 0.8541 0.0599
-9.500 -0.5975 0.02222 0.01443 -0.0809 0.8436 0.0631
-9.250 -0.5882 0.02143 0.01356 -0.0793 0.8335 0.0661
-9.000 -0.5813 0.02072 0.01282 -0.0772 0.8239 0.0694
-8.750 -0.5683 0.02014 0.01214 -0.0758 0.8156 0.0738
-8.500 -0.5548 0.01948 0.01147 -0.0745 0.8075 0.0791
-8.250 -0.5379 0.01895 0.01087 -0.0734 0.7999 0.0855
-8.000 -0.5209 0.01836 0.01027 -0.0724 0.7934 0.0939
-7.750 -0.5026 0.01780 0.00973 -0.0716 0.7858 0.1041
-7.500 -0.4832 0.01725 0.00917 -0.0708 0.7793 0.1172
-7.250 -0.4631 0.01670 0.00866 -0.0702 0.7729 0.1347
-7.000 -0.4426 0.01612 0.00815 -0.0697 0.7661 0.1570
-6.750 -0.4217 0.01551 0.00763 -0.0693 0.7604 0.1870
-6.500 -0.4005 0.01487 0.00714 -0.0689 0.7542 0.2254
-6.250 -0.3787 0.01422 0.00669 -0.0687 0.7476 0.2724
-6.000 -0.3556 0.01368 0.00632 -0.0685 0.7421 0.3228
-5.750 -0.3306 0.01333 0.00611 -0.0684 0.7365 0.3681
-5.500 -0.3042 0.01313 0.00597 -0.0684 0.7302 0.4019
-5.250 -0.2771 0.01300 0.00585 -0.0683 0.7247 0.4269
-5.000 -0.2495 0.01293 0.00575 -0.0683 0.7194 0.4470
-4.750 -0.2217 0.01287 0.00568 -0.0684 0.7134 0.4635
-4.500 -0.1937 0.01284 0.00559 -0.0684 0.7080 0.4781
-4.250 -0.1654 0.01282 0.00549 -0.0685 0.7031 0.4919
-4.000 -0.1372 0.01282 0.00546 -0.0686 0.6970 0.5050
-3.750 -0.1091 0.01283 0.00546 -0.0686 0.6917 0.5161
-3.500 -0.0805 0.01283 0.00536 -0.0687 0.6871 0.5266
-3.250 -0.0523 0.01284 0.00537 -0.0688 0.6814 0.5348
-3.000 -0.0236 0.01282 0.00527 -0.0690 0.6758 0.5428
-2.750 0.0048 0.01282 0.00525 -0.0690 0.6711 0.5486
-2.500 0.0335 0.01282 0.00518 -0.0692 0.6666 0.5552
-2.250 0.0622 0.01280 0.00512 -0.0694 0.6609 0.5612
-2.000 0.0905 0.01280 0.00511 -0.0695 0.6557 0.5661
-1.750 0.1193 0.01281 0.00504 -0.0696 0.6514 0.5716
-1.500 0.1482 0.01281 0.00499 -0.0700 0.6464 0.5776
-1.250 0.1764 0.01281 0.00502 -0.0700 0.6414 0.5818
-1.000 0.2050 0.01283 0.00501 -0.0701 0.6368 0.5866
-0.750 0.2339 0.01285 0.00496 -0.0704 0.6326 0.5921
-0.500 0.2624 0.01287 0.00497 -0.0706 0.6271 0.5971
-0.250 0.2906 0.01289 0.00502 -0.0707 0.6223 0.6013
0.000 0.3193 0.01293 0.00504 -0.0708 0.6182 0.6064
0.250 0.3482 0.01298 0.00503 -0.0711 0.6141 0.6119
0.500 0.3764 0.01301 0.00511 -0.0713 0.6088 0.6163
0.750 0.4044 0.01306 0.00518 -0.0713 0.6040 0.6209
1.000 0.4331 0.01312 0.00521 -0.0715 0.6000 0.6263
1.250 0.4619 0.01318 0.00526 -0.0718 0.5959 0.6319
1.500 0.4896 0.01324 0.00538 -0.0718 0.5908 0.6359
1.750 0.5176 0.01331 0.00548 -0.0719 0.5861 0.6408
2.000 0.5462 0.01339 0.00553 -0.0721 0.5821 0.6465
2.250 0.5745 0.01348 0.00564 -0.0723 0.5776 0.6520
2.500 0.6018 0.01356 0.00581 -0.0722 0.5725 0.6564
2.750 0.6297 0.01364 0.00592 -0.0723 0.5678 0.6615
3.000 0.6584 0.01374 0.00598 -0.0725 0.5638 0.6675
3.250 0.6853 0.01384 0.00618 -0.0724 0.5585 0.6725
3.500 0.7124 0.01394 0.00635 -0.0723 0.5531 0.6777
3.750 0.7403 0.01404 0.00645 -0.0724 0.5484 0.6835
4.000 0.7680 0.01416 0.00661 -0.0725 0.5434 0.6891
4.250 0.7942 0.01427 0.00683 -0.0723 0.5376 0.6940
4.500 0.8213 0.01438 0.00698 -0.0722 0.5322 0.7001
4.750 0.8489 0.01451 0.00712 -0.0723 0.5269 0.7066
5.000 0.8742 0.01463 0.00737 -0.0719 0.5202 0.7114
5.250 0.9006 0.01474 0.00751 -0.0716 0.5138 0.7172
5.500 0.9264 0.01488 0.00771 -0.0714 0.5059 0.7240
5.750 0.9513 0.01499 0.00788 -0.0709 0.4976 0.7294
6.000 0.9759 0.01513 0.00811 -0.0704 0.4894 0.7356
6.250 1.0009 0.01528 0.00829 -0.0701 0.4802 0.7424
6.500 1.0236 0.01542 0.00853 -0.0692 0.4692 0.7481
6.750 1.0455 0.01559 0.00873 -0.0682 0.4555 0.7550
7.000 1.0666 0.01579 0.00894 -0.0672 0.4400 0.7621
7.250 1.0860 0.01602 0.00921 -0.0658 0.4244 0.7684
7.500 1.1054 0.01631 0.00952 -0.0646 0.4086 0.7761
7.750 1.1226 0.01662 0.00986 -0.0629 0.3910 0.7832
8.000 1.1375 0.01701 0.01026 -0.0610 0.3704 0.7913
8.250 1.1477 0.01752 0.01071 -0.0584 0.3468 0.7995
8.500 1.1516 0.01811 0.01126 -0.0547 0.3222 0.8088
8.750 1.1522 0.01896 0.01202 -0.0509 0.2972 0.8189
9.000 1.1528 0.01997 0.01295 -0.0475 0.2716 0.8306
9.250 1.1507 0.02117 0.01408 -0.0440 0.2476 0.8431
9.500 1.1496 0.02245 0.01532 -0.0409 0.2240 0.8578
9.750 1.1476 0.02387 0.01670 -0.0380 0.2028 0.8765
10.000 1.1457 0.02536 0.01816 -0.0353 0.1833 0.9032
10.250 1.1464 0.02680 0.01962 -0.0334 0.1650 1.0000
10.500 1.1496 0.02864 0.02138 -0.0323 0.1473 1.0000
10.750 1.1532 0.03052 0.02318 -0.0314 0.1321 1.0000
11.000 1.1567 0.03245 0.02506 -0.0305 0.1186 1.0000
11.250 1.1604 0.03442 0.02699 -0.0297 0.1069 1.0000
11.500 1.1642 0.03643 0.02898 -0.0290 0.0972 1.0000
11.750 1.1673 0.03855 0.03107 -0.0284 0.0890 1.0000
12.000 1.1726 0.04053 0.03306 -0.0279 0.0818 1.0000
12.250 1.1764 0.04272 0.03525 -0.0275 0.0759 1.0000
12.500 1.1811 0.04488 0.03744 -0.0272 0.0708 1.0000
12.750 1.1851 0.04717 0.03975 -0.0270 0.0665 1.0000
13.000 1.1901 0.04942 0.04204 -0.0269 0.0625 1.0000
13.250 1.1927 0.05199 0.04462 -0.0268 0.0594 1.0000
13.500 1.1986 0.05425 0.04695 -0.0268 0.0565 1.0000
13.750 1.2028 0.05674 0.04950 -0.0270 0.0539 1.0000
14.000 1.2044 0.05960 0.05237 -0.0272 0.0516 1.0000
14.250 1.2103 0.06201 0.05487 -0.0274 0.0494 1.0000
14.500 1.2143 0.06468 0.05761 -0.0277 0.0474 1.0000
14.750 1.2169 0.06758 0.06055 -0.0282 0.0458 1.0000
15.000 1.2191 0.07056 0.06356 -0.0287 0.0443 1.0000
15.250 1.2238 0.07330 0.06641 -0.0292 0.0427 1.0000
15.500 1.2278 0.07616 0.06935 -0.0298 0.0411 1.0000
15.750 1.2302 0.07927 0.07252 -0.0306 0.0399 1.0000
16.000 1.2313 0.08259 0.07586 -0.0314 0.0389 1.0000
16.250 1.2354 0.08555 0.07892 -0.0322 0.0377 1.0000
16.500 1.2393 0.08857 0.08203 -0.0330 0.0366 1.0000
16.750 1.2422 0.09177 0.08532 -0.0340 0.0355 1.0000
17.000 1.2446 0.09506 0.08867 -0.0351 0.0346 1.0000
17.250 1.2461 0.09852 0.09217 -0.0363 0.0338 1.0000
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