NACA 63-415 AIRFOIL (n63415-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 63-415 AIRFOIL (n63415-il) Reynolds number: 500,000 Max Cl/Cd: 90.74 at α=4.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-n63415-il-500000-n5.txt Download as CSV file: xf-n63415-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NACA 63-415 AIRFOIL
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
------ -------- --------- --------- -------- -------- --------
-18.250 -0.8075 0.12235 0.11935 -0.0302 1.0000 0.0130
-18.000 -0.8547 0.10829 0.10508 -0.0381 1.0000 0.0130
-17.750 -0.8829 0.09863 0.09526 -0.0436 1.0000 0.0130
-17.500 -0.9059 0.09028 0.08675 -0.0485 1.0000 0.0130
-17.250 -0.9249 0.08295 0.07928 -0.0527 1.0000 0.0131
-17.000 -0.9403 0.07656 0.07274 -0.0564 1.0000 0.0131
-16.750 -0.9529 0.07082 0.06685 -0.0597 1.0000 0.0132
-16.500 -0.9624 0.06581 0.06171 -0.0624 1.0000 0.0133
-16.250 -0.9698 0.06130 0.05706 -0.0648 1.0000 0.0134
-16.000 -0.9761 0.05714 0.05276 -0.0668 1.0000 0.0135
-15.750 -0.9821 0.05325 0.04878 -0.0687 1.0000 0.0137
-15.500 -0.9856 0.04985 0.04529 -0.0701 1.0000 0.0138
-15.250 -0.9878 0.04675 0.04213 -0.0713 1.0000 0.0140
-15.000 -0.9877 0.04400 0.03930 -0.0722 1.0000 0.0141
-14.750 -0.9859 0.04154 0.03675 -0.0729 1.0000 0.0143
-14.500 -0.9832 0.03923 0.03437 -0.0735 1.0000 0.0145
-14.250 -0.9793 0.03713 0.03219 -0.0738 1.0000 0.0147
-14.000 -0.9730 0.03533 0.03031 -0.0740 1.0000 0.0150
-13.750 -0.9665 0.03361 0.02851 -0.0740 1.0000 0.0153
-13.500 -0.9608 0.03188 0.02670 -0.0738 1.0000 0.0156
-13.250 -0.9540 0.03032 0.02505 -0.0734 1.0000 0.0159
-13.000 -0.9461 0.02892 0.02357 -0.0729 1.0000 0.0162
-12.750 -0.9381 0.02762 0.02217 -0.0722 1.0000 0.0165
-12.500 -0.9329 0.02622 0.02075 -0.0712 1.0000 0.0169
-12.250 -0.9266 0.02506 0.01954 -0.0700 1.0000 0.0171
-12.000 -0.9212 0.02404 0.01849 -0.0683 1.0000 0.0174
-11.750 -0.9013 0.02306 0.01746 -0.0690 0.9877 0.0179
-11.500 -0.8695 0.02198 0.01630 -0.0721 0.9686 0.0185
-11.250 -0.8356 0.02099 0.01521 -0.0752 0.9517 0.0192
-11.000 -0.8052 0.02015 0.01423 -0.0773 0.9334 0.0199
-10.750 -0.7837 0.01936 0.01335 -0.0777 0.9138 0.0206
-10.500 -0.7647 0.01880 0.01270 -0.0771 0.8977 0.0212
-10.250 -0.7458 0.01829 0.01211 -0.0762 0.8839 0.0218
-10.000 -0.7265 0.01780 0.01151 -0.0754 0.8719 0.0226
-9.500 -0.6856 0.01684 0.01036 -0.0740 0.8506 0.0241
-9.250 -0.6649 0.01634 0.00980 -0.0733 0.8414 0.0250
-9.000 -0.6421 0.01595 0.00936 -0.0729 0.8323 0.0262
-8.750 -0.6191 0.01556 0.00888 -0.0724 0.8242 0.0272
-8.500 -0.5954 0.01519 0.00843 -0.0721 0.8159 0.0282
-8.250 -0.5722 0.01475 0.00792 -0.0717 0.8085 0.0293
-8.000 -0.5481 0.01433 0.00746 -0.0714 0.8007 0.0305
-7.750 -0.5232 0.01401 0.00709 -0.0712 0.7934 0.0320
-7.500 -0.4976 0.01370 0.00671 -0.0711 0.7865 0.0334
-7.250 -0.4723 0.01335 0.00631 -0.0710 0.7793 0.0349
-7.000 -0.4467 0.01301 0.00593 -0.0709 0.7728 0.0366
-6.750 -0.4205 0.01272 0.00559 -0.0708 0.7658 0.0385
-6.500 -0.3939 0.01248 0.00528 -0.0708 0.7593 0.0405
-6.250 -0.3674 0.01215 0.00495 -0.0708 0.7528 0.0435
-6.000 -0.3405 0.01190 0.00467 -0.0709 0.7460 0.0470
-5.750 -0.3135 0.01164 0.00438 -0.0709 0.7400 0.0515
-5.500 -0.2862 0.01137 0.00411 -0.0710 0.7333 0.0582
-5.250 -0.2591 0.01110 0.00385 -0.0712 0.7268 0.0692
-5.000 -0.2317 0.01080 0.00359 -0.0713 0.7210 0.0859
-4.750 -0.2043 0.01046 0.00334 -0.0716 0.7144 0.1108
-4.250 -0.1494 0.00970 0.00284 -0.0722 0.7022 0.1906
-4.000 -0.1219 0.00925 0.00259 -0.0726 0.6959 0.2479
-3.750 -0.0942 0.00883 0.00236 -0.0730 0.6902 0.3111
-3.500 -0.0659 0.00846 0.00220 -0.0734 0.6838 0.3738
-3.250 -0.0373 0.00828 0.00211 -0.0738 0.6777 0.4130
-3.000 -0.0085 0.00815 0.00205 -0.0741 0.6723 0.4466
-2.750 0.0204 0.00804 0.00202 -0.0743 0.6660 0.4790
-2.500 0.0492 0.00800 0.00199 -0.0746 0.6600 0.5023
-2.250 0.0783 0.00797 0.00196 -0.0748 0.6545 0.5162
-2.000 0.1074 0.00794 0.00195 -0.0751 0.6487 0.5298
-1.750 0.1363 0.00795 0.00193 -0.0753 0.6430 0.5419
-1.500 0.1655 0.00795 0.00191 -0.0755 0.6373 0.5504
-1.250 0.1946 0.00795 0.00190 -0.0757 0.6313 0.5574
-1.000 0.2234 0.00797 0.00189 -0.0759 0.6260 0.5646
-0.500 0.2816 0.00799 0.00190 -0.0764 0.6146 0.5783
-0.250 0.3104 0.00803 0.00191 -0.0766 0.6091 0.5851
0.000 0.3396 0.00804 0.00193 -0.0769 0.6039 0.5910
0.250 0.3686 0.00806 0.00196 -0.0771 0.5983 0.5969
0.500 0.3973 0.00812 0.00198 -0.0773 0.5928 0.6032
0.750 0.4263 0.00814 0.00203 -0.0775 0.5873 0.6090
1.000 0.4552 0.00817 0.00207 -0.0777 0.5816 0.6150
1.500 0.5127 0.00827 0.00218 -0.0781 0.5701 0.6269
1.750 0.5413 0.00833 0.00225 -0.0783 0.5637 0.6334
2.000 0.5699 0.00840 0.00232 -0.0784 0.5579 0.6397
2.250 0.5985 0.00844 0.00240 -0.0786 0.5517 0.6453
2.500 0.6269 0.00852 0.00249 -0.0787 0.5455 0.6519
2.750 0.6554 0.00859 0.00258 -0.0789 0.5395 0.6583
3.000 0.6837 0.00866 0.00269 -0.0790 0.5325 0.6648
3.250 0.7118 0.00875 0.00279 -0.0791 0.5245 0.6713
3.500 0.7394 0.00885 0.00289 -0.0791 0.5130 0.6775
3.750 0.7672 0.00895 0.00302 -0.0791 0.5018 0.6845
4.000 0.7947 0.00908 0.00314 -0.0791 0.4915 0.6914
4.250 0.8216 0.00922 0.00329 -0.0790 0.4771 0.6976
4.500 0.8480 0.00940 0.00344 -0.0788 0.4569 0.7047
4.750 0.8738 0.00963 0.00361 -0.0785 0.4341 0.7114
5.000 0.8984 0.00993 0.00383 -0.0781 0.4038 0.7184
5.250 0.9216 0.01037 0.00411 -0.0775 0.3659 0.7255
5.500 0.9437 0.01087 0.00446 -0.0767 0.3244 0.7323
5.750 0.9646 0.01147 0.00488 -0.0758 0.2816 0.7398
6.000 0.9849 0.01212 0.00535 -0.0749 0.2404 0.7466
6.250 1.0047 0.01276 0.00584 -0.0738 0.2015 0.7542
6.500 1.0239 0.01343 0.00635 -0.0727 0.1670 0.7618
6.750 1.0429 0.01406 0.00687 -0.0715 0.1377 0.7696
7.000 1.0616 0.01469 0.00739 -0.0704 0.1120 0.7777
7.250 1.0799 0.01528 0.00792 -0.0690 0.0918 0.7863
7.500 1.0971 0.01590 0.00847 -0.0676 0.0735 0.7955
7.750 1.1133 0.01652 0.00904 -0.0660 0.0588 0.8052
8.000 1.1290 0.01709 0.00960 -0.0643 0.0487 0.8152
8.250 1.1427 0.01762 0.01014 -0.0622 0.0427 0.8267
8.500 1.1559 0.01814 0.01070 -0.0600 0.0389 0.8387
8.750 1.1689 0.01868 0.01130 -0.0579 0.0362 0.8516
9.000 1.1814 0.01923 0.01193 -0.0558 0.0340 0.8665
9.250 1.1917 0.01985 0.01263 -0.0534 0.0321 0.8851
9.500 1.2003 0.02046 0.01334 -0.0507 0.0308 0.9126
9.750 1.2120 0.02104 0.01404 -0.0489 0.0295 1.0000
10.000 1.2257 0.02189 0.01491 -0.0477 0.0280 1.0000
10.250 1.2378 0.02287 0.01591 -0.0464 0.0266 1.0000
10.500 1.2501 0.02387 0.01695 -0.0452 0.0257 1.0000
10.750 1.2632 0.02485 0.01798 -0.0442 0.0246 1.0000
11.000 1.2753 0.02593 0.01910 -0.0431 0.0234 1.0000
11.250 1.2860 0.02714 0.02035 -0.0421 0.0224 1.0000
11.500 1.2955 0.02849 0.02173 -0.0411 0.0214 1.0000
11.750 1.3070 0.02971 0.02303 -0.0402 0.0206 1.0000
12.000 1.3175 0.03105 0.02443 -0.0394 0.0196 1.0000
12.250 1.3268 0.03252 0.02594 -0.0387 0.0189 1.0000
12.500 1.3350 0.03414 0.02760 -0.0379 0.0181 1.0000
12.750 1.3424 0.03586 0.02938 -0.0372 0.0176 1.0000
13.000 1.3506 0.03755 0.03114 -0.0366 0.0170 1.0000
13.250 1.3580 0.03935 0.03302 -0.0361 0.0164 1.0000
13.500 1.3651 0.04124 0.03498 -0.0357 0.0159 1.0000
13.750 1.3710 0.04326 0.03706 -0.0353 0.0154 1.0000
14.000 1.3763 0.04543 0.03929 -0.0350 0.0151 1.0000
14.250 1.3803 0.04782 0.04173 -0.0349 0.0147 1.0000
14.500 1.3837 0.05032 0.04431 -0.0348 0.0144 1.0000
14.750 1.3877 0.05283 0.04691 -0.0349 0.0142 1.0000
15.000 1.3912 0.05548 0.04966 -0.0350 0.0139 1.0000
15.250 1.3941 0.05826 0.05253 -0.0353 0.0136 1.0000
15.500 1.3968 0.06114 0.05550 -0.0357 0.0134 1.0000
15.750 1.3990 0.06413 0.05858 -0.0362 0.0131 1.0000
16.000 1.4005 0.06732 0.06186 -0.0368 0.0129 1.0000
16.250 1.4016 0.07062 0.06525 -0.0376 0.0128 1.0000
16.500 1.4017 0.07413 0.06885 -0.0385 0.0126 1.0000
16.750 1.4019 0.07771 0.07252 -0.0396 0.0123 1.0000
17.000 1.4005 0.08160 0.07650 -0.0408 0.0122 1.0000
17.250 1.3980 0.08574 0.08073 -0.0422 0.0120 1.0000
17.500 1.3944 0.09013 0.08521 -0.0438 0.0119 1.0000
17.750 1.3902 0.09469 0.08987 -0.0456 0.0117 1.0000
18.000 1.3875 0.09911 0.09441 -0.0474 0.0116 1.0000
18.250 1.3845 0.10366 0.09908 -0.0493 0.0115 1.0000
18.500 1.3805 0.10843 0.10396 -0.0515 0.0114 1.0000
18.750 1.3762 0.11332 0.10896 -0.0537 0.0113 1.0000
19.000 1.3714 0.11836 0.11412 -0.0562 0.0112 1.0000
19.250 1.3665 0.12349 0.11936 -0.0588 0.0111 1.0000
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