NACA 63 (naca633418-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 63 (naca633418-il) Reynolds number: 500,000 Max Cl/Cd: 91.56 at α=6.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-naca633418-il-500000-n5.txt Download as CSV file: xf-naca633418-il-500000-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 = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -0.9379 0.10794 0.10395 -0.0455 1.0000 0.0184
-19.500 -0.9454 0.10294 0.09887 -0.0481 1.0000 0.0185
-19.250 -0.9530 0.09800 0.09384 -0.0507 1.0000 0.0187
-19.000 -0.9596 0.09335 0.08910 -0.0531 1.0000 0.0188
-18.750 -0.9650 0.08894 0.08459 -0.0553 1.0000 0.0189
-18.500 -0.9700 0.08466 0.08022 -0.0574 1.0000 0.0191
-18.250 -0.9739 0.08059 0.07607 -0.0593 1.0000 0.0193
-18.000 -0.9772 0.07675 0.07213 -0.0611 1.0000 0.0195
-17.750 -0.9798 0.07306 0.06836 -0.0627 1.0000 0.0196
-17.500 -0.9811 0.06961 0.06483 -0.0642 1.0000 0.0198
-17.250 -0.9817 0.06632 0.06145 -0.0655 1.0000 0.0201
-17.000 -0.9809 0.06329 0.05832 -0.0667 1.0000 0.0203
-16.750 -0.9801 0.06030 0.05525 -0.0678 1.0000 0.0205
-16.500 -0.9805 0.05726 0.05216 -0.0689 1.0000 0.0208
-16.250 -0.9801 0.05440 0.04924 -0.0698 1.0000 0.0210
-16.000 -0.9783 0.05174 0.04654 -0.0706 1.0000 0.0213
-15.750 -0.9748 0.04932 0.04407 -0.0713 1.0000 0.0216
-15.500 -0.9717 0.04694 0.04163 -0.0718 1.0000 0.0218
-15.250 -0.9670 0.04479 0.03942 -0.0722 1.0000 0.0222
-15.000 -0.9616 0.04277 0.03735 -0.0725 1.0000 0.0225
-14.750 -0.9562 0.04083 0.03534 -0.0727 1.0000 0.0229
-14.500 -0.9507 0.03899 0.03344 -0.0728 1.0000 0.0233
-14.250 -0.9442 0.03728 0.03167 -0.0727 1.0000 0.0237
-14.000 -0.9375 0.03564 0.02996 -0.0725 1.0000 0.0240
-13.750 -0.9331 0.03385 0.02815 -0.0723 1.0000 0.0244
-13.500 -0.9273 0.03224 0.02651 -0.0719 1.0000 0.0248
-13.250 -0.9205 0.03076 0.02501 -0.0714 1.0000 0.0253
-12.750 -0.8447 0.02750 0.02157 -0.0823 0.9336 0.0271
-12.500 -0.8129 0.02623 0.02014 -0.0860 0.9060 0.0281
-12.250 -0.8003 0.02503 0.01883 -0.0860 0.8820 0.0288
-12.000 -0.7896 0.02405 0.01775 -0.0852 0.8643 0.0298
-11.500 -0.7678 0.02225 0.01576 -0.0832 0.8380 0.0315
-11.250 -0.7561 0.02143 0.01484 -0.0821 0.8276 0.0323
-11.000 -0.7463 0.02052 0.01387 -0.0809 0.8170 0.0334
-10.750 -0.7350 0.01972 0.01302 -0.0797 0.8081 0.0343
-10.500 -0.7233 0.01898 0.01221 -0.0784 0.7993 0.0356
-10.250 -0.7113 0.01831 0.01146 -0.0770 0.7914 0.0368
-10.000 -0.7014 0.01765 0.01074 -0.0752 0.7830 0.0381
-9.750 -0.6924 0.01710 0.01014 -0.0731 0.7756 0.0397
-9.500 -0.6758 0.01660 0.00960 -0.0721 0.7686 0.0415
-9.250 -0.6573 0.01618 0.00911 -0.0712 0.7619 0.0434
-9.000 -0.6383 0.01572 0.00862 -0.0703 0.7556 0.0458
-8.750 -0.6171 0.01533 0.00819 -0.0697 0.7488 0.0485
-8.500 -0.5958 0.01494 0.00777 -0.0691 0.7427 0.0517
-8.250 -0.5731 0.01458 0.00738 -0.0687 0.7372 0.0555
-8.000 -0.5500 0.01420 0.00700 -0.0684 0.7309 0.0599
-7.500 -0.5023 0.01352 0.00628 -0.0678 0.7191 0.0718
-7.250 -0.4776 0.01318 0.00595 -0.0677 0.7132 0.0793
-7.000 -0.4528 0.01285 0.00562 -0.0675 0.7074 0.0887
-6.750 -0.4276 0.01251 0.00530 -0.0674 0.7019 0.1005
-6.500 -0.4021 0.01215 0.00499 -0.0674 0.6960 0.1160
-6.250 -0.3766 0.01179 0.00468 -0.0674 0.6904 0.1355
-6.000 -0.3509 0.01141 0.00437 -0.0675 0.6853 0.1594
-5.750 -0.3249 0.01098 0.00406 -0.0676 0.6796 0.1903
-5.500 -0.2989 0.01054 0.00375 -0.0678 0.6738 0.2275
-5.000 -0.2457 0.00966 0.00319 -0.0683 0.6636 0.3174
-4.750 -0.2182 0.00933 0.00299 -0.0686 0.6580 0.3586
-4.500 -0.1901 0.00914 0.00286 -0.0688 0.6527 0.3897
-4.250 -0.1614 0.00901 0.00277 -0.0692 0.6479 0.4138
-4.000 -0.1324 0.00891 0.00269 -0.0695 0.6429 0.4320
-3.750 -0.1035 0.00885 0.00262 -0.0697 0.6378 0.4469
-3.500 -0.0746 0.00881 0.00257 -0.0700 0.6329 0.4604
-3.250 -0.0452 0.00877 0.00252 -0.0703 0.6279 0.4730
-3.000 -0.0160 0.00873 0.00249 -0.0706 0.6228 0.4848
-2.750 0.0130 0.00872 0.00246 -0.0709 0.6182 0.4944
-2.500 0.0423 0.00872 0.00243 -0.0711 0.6140 0.5031
-2.250 0.0717 0.00870 0.00240 -0.0715 0.6093 0.5097
-2.000 0.1009 0.00870 0.00239 -0.0717 0.6043 0.5162
-1.750 0.1301 0.00872 0.00236 -0.0720 0.5996 0.5223
-1.500 0.1594 0.00872 0.00235 -0.0723 0.5953 0.5273
-1.250 0.1887 0.00871 0.00235 -0.0726 0.5909 0.5326
-1.000 0.2180 0.00873 0.00235 -0.0729 0.5865 0.5379
-0.750 0.2471 0.00877 0.00234 -0.0732 0.5821 0.5426
-0.500 0.2762 0.00877 0.00236 -0.0734 0.5778 0.5471
-0.250 0.3055 0.00878 0.00238 -0.0737 0.5731 0.5520
0.000 0.3347 0.00882 0.00239 -0.0740 0.5688 0.5570
0.250 0.3636 0.00887 0.00241 -0.0743 0.5647 0.5613
0.500 0.3927 0.00888 0.00245 -0.0745 0.5606 0.5657
0.750 0.4219 0.00891 0.00250 -0.0748 0.5560 0.5708
1.000 0.4509 0.00896 0.00254 -0.0751 0.5515 0.5757
1.250 0.4796 0.00902 0.00258 -0.0753 0.5474 0.5798
1.500 0.5086 0.00905 0.00265 -0.0755 0.5432 0.5844
1.750 0.5375 0.00909 0.00271 -0.0758 0.5386 0.5896
2.000 0.5663 0.00916 0.00277 -0.0760 0.5339 0.5946
2.250 0.5946 0.00924 0.00284 -0.0761 0.5292 0.5990
2.500 0.6235 0.00928 0.00294 -0.0764 0.5246 0.6037
2.750 0.6521 0.00934 0.00302 -0.0766 0.5194 0.6087
3.000 0.6804 0.00943 0.00310 -0.0767 0.5144 0.6139
3.250 0.7086 0.00951 0.00321 -0.0769 0.5097 0.6188
3.500 0.7370 0.00957 0.00332 -0.0770 0.5043 0.6239
3.750 0.7650 0.00966 0.00343 -0.0771 0.4987 0.6289
4.000 0.7928 0.00977 0.00354 -0.0772 0.4934 0.6336
4.250 0.8208 0.00984 0.00367 -0.0773 0.4868 0.6388
4.500 0.8477 0.00997 0.00380 -0.0772 0.4788 0.6444
4.750 0.8753 0.01008 0.00393 -0.0773 0.4706 0.6498
5.000 0.9020 0.01021 0.00408 -0.0772 0.4626 0.6545
5.250 0.9291 0.01032 0.00424 -0.0771 0.4542 0.6597
5.500 0.9547 0.01051 0.00440 -0.0768 0.4425 0.6654
5.750 0.9794 0.01072 0.00459 -0.0764 0.4252 0.6707
6.000 1.0033 0.01096 0.00481 -0.0759 0.4062 0.6761
6.250 1.0273 0.01122 0.00504 -0.0753 0.3902 0.6818
6.500 1.0504 0.01152 0.00530 -0.0747 0.3716 0.6871
6.750 1.0712 0.01190 0.00562 -0.0737 0.3482 0.6925
7.000 1.0890 0.01242 0.00603 -0.0723 0.3189 0.6985
7.250 1.1039 0.01306 0.00653 -0.0704 0.2868 0.7045
7.500 1.1160 0.01378 0.00711 -0.0681 0.2542 0.7099
7.750 1.1264 0.01445 0.00767 -0.0656 0.2271 0.7160
8.000 1.1329 0.01515 0.00826 -0.0623 0.2028 0.7225
8.250 1.1397 0.01590 0.00894 -0.0593 0.1816 0.7289
8.500 1.1461 0.01672 0.00971 -0.0564 0.1613 0.7359
8.750 1.1532 0.01759 0.01052 -0.0539 0.1445 0.7427
9.000 1.1600 0.01852 0.01142 -0.0515 0.1293 0.7497
9.250 1.1669 0.01952 0.01239 -0.0493 0.1154 0.7576
9.500 1.1738 0.02059 0.01344 -0.0472 0.1027 0.7652
9.750 1.1813 0.02168 0.01453 -0.0454 0.0924 0.7739
10.000 1.1888 0.02283 0.01569 -0.0437 0.0832 0.7823
10.250 1.1963 0.02403 0.01690 -0.0421 0.0755 0.7920
10.500 1.2036 0.02528 0.01819 -0.0405 0.0689 0.8018
10.750 1.2122 0.02650 0.01945 -0.0392 0.0634 0.8131
11.000 1.2191 0.02785 0.02084 -0.0378 0.0587 0.8254
11.250 1.2273 0.02911 0.02219 -0.0366 0.0549 0.8400
11.500 1.2331 0.03055 0.02369 -0.0352 0.0516 0.8585
11.750 1.2396 0.03181 0.02508 -0.0337 0.0490 0.8858
12.000 1.2497 0.03325 0.02664 -0.0333 0.0462 0.9449
12.500 1.2654 0.03650 0.02996 -0.0322 0.0414 1.0000
12.750 1.2724 0.03830 0.03178 -0.0317 0.0394 1.0000
13.000 1.2802 0.04009 0.03361 -0.0312 0.0377 1.0000
13.250 1.2879 0.04192 0.03549 -0.0309 0.0360 1.0000
13.500 1.2947 0.04389 0.03749 -0.0306 0.0345 1.0000
13.750 1.3006 0.04598 0.03961 -0.0304 0.0331 1.0000
14.000 1.3080 0.04799 0.04168 -0.0303 0.0319 1.0000
14.250 1.3145 0.05011 0.04384 -0.0302 0.0306 1.0000
14.500 1.3197 0.05243 0.04621 -0.0302 0.0296 1.0000
14.750 1.3242 0.05487 0.04869 -0.0303 0.0287 1.0000
15.000 1.3304 0.05717 0.05105 -0.0305 0.0279 1.0000
15.250 1.3356 0.05962 0.05358 -0.0307 0.0270 1.0000
15.500 1.3407 0.06215 0.05615 -0.0310 0.0261 1.0000
15.750 1.3441 0.06490 0.05896 -0.0314 0.0254 1.0000
16.000 1.3464 0.06784 0.06193 -0.0319 0.0247 1.0000
16.250 1.3505 0.07063 0.06481 -0.0324 0.0242 1.0000
16.500 1.3545 0.07346 0.06772 -0.0330 0.0236 1.0000
16.750 1.3575 0.07648 0.07081 -0.0337 0.0230 1.0000
17.000 1.3596 0.07963 0.07403 -0.0345 0.0225 1.0000
17.250 1.3617 0.08285 0.07731 -0.0354 0.0220 1.0000
17.500 1.3620 0.08640 0.08093 -0.0365 0.0215 1.0000
17.750 1.3612 0.09014 0.08473 -0.0377 0.0212 1.0000
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