NACA 63-415 AIRFOIL (n63415-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: NACA 63-415 AIRFOIL (n63415-il) Reynolds number: 1,000,000 Max Cl/Cd: 118.71 at α=5.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-n63415-il-1000000.txt Download as CSV file: xf-n63415-il-1000000.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 = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.000 -0.8646 0.12321 0.12092 -0.0296 1.0000 0.0126
-18.750 -0.9113 0.10995 0.10745 -0.0369 1.0000 0.0125
-18.500 -0.9426 0.10016 0.09750 -0.0423 1.0000 0.0125
-18.250 -0.9666 0.09203 0.08924 -0.0468 1.0000 0.0125
-18.000 -0.9822 0.08548 0.08257 -0.0505 1.0000 0.0125
-17.750 -0.9996 0.07888 0.07585 -0.0541 1.0000 0.0125
-17.500 -1.0116 0.07328 0.07015 -0.0573 1.0000 0.0126
-17.250 -1.0199 0.06841 0.06518 -0.0599 1.0000 0.0127
-17.000 -1.0288 0.06362 0.06029 -0.0625 1.0000 0.0129
-16.750 -1.0375 0.05907 0.05562 -0.0649 1.0000 0.0129
-16.500 -1.0407 0.05535 0.05182 -0.0668 1.0000 0.0130
-16.250 -1.0452 0.05161 0.04798 -0.0685 1.0000 0.0132
-16.000 -1.0464 0.04846 0.04474 -0.0699 1.0000 0.0133
-15.750 -1.0484 0.04536 0.04154 -0.0711 1.0000 0.0135
-15.500 -1.0478 0.04265 0.03874 -0.0720 1.0000 0.0136
-15.250 -1.0453 0.04022 0.03622 -0.0727 1.0000 0.0138
-15.000 -1.0394 0.03818 0.03410 -0.0733 1.0000 0.0140
-14.750 -1.0350 0.03607 0.03190 -0.0737 1.0000 0.0141
-14.500 -1.0307 0.03402 0.02976 -0.0740 1.0000 0.0142
-14.250 -1.0249 0.03218 0.02783 -0.0741 1.0000 0.0144
-14.000 -1.0280 0.02963 0.02519 -0.0738 1.0000 0.0147
-13.750 -1.0237 0.02784 0.02335 -0.0735 1.0000 0.0150
-13.500 -1.0170 0.02634 0.02179 -0.0730 1.0000 0.0152
-13.250 -1.0072 0.02517 0.02059 -0.0725 1.0000 0.0155
-13.000 -0.9986 0.02401 0.01939 -0.0716 1.0000 0.0157
-12.750 -0.9888 0.02305 0.01839 -0.0706 1.0000 0.0161
-12.500 -0.9819 0.02207 0.01736 -0.0690 1.0000 0.0164
-12.250 -0.9776 0.02126 0.01650 -0.0668 1.0000 0.0167
-12.000 -0.9689 0.02041 0.01560 -0.0653 0.9977 0.0169
-11.750 -0.9379 0.01956 0.01467 -0.0676 0.9856 0.0173
-11.500 -0.9051 0.01835 0.01338 -0.0706 0.9768 0.0179
-11.250 -0.8692 0.01745 0.01246 -0.0737 0.9670 0.0187
-11.000 -0.8331 0.01684 0.01180 -0.0764 0.9538 0.0194
-10.750 -0.8051 0.01633 0.01121 -0.0773 0.9345 0.0200
-10.500 -0.7833 0.01592 0.01069 -0.0767 0.9163 0.0207
-10.250 -0.7617 0.01559 0.01026 -0.0760 0.9015 0.0211
-10.000 -0.7450 0.01485 0.00942 -0.0748 0.8876 0.0219
-9.750 -0.7235 0.01444 0.00896 -0.0742 0.8760 0.0228
-9.500 -0.7004 0.01410 0.00856 -0.0737 0.8660 0.0236
-9.250 -0.6764 0.01383 0.00822 -0.0733 0.8564 0.0246
-9.000 -0.6513 0.01359 0.00793 -0.0730 0.8475 0.0253
-8.750 -0.6298 0.01299 0.00725 -0.0725 0.8388 0.0267
-8.500 -0.6049 0.01266 0.00690 -0.0722 0.8303 0.0279
-8.250 -0.5795 0.01240 0.00658 -0.0720 0.8226 0.0290
-8.000 -0.5532 0.01216 0.00629 -0.0720 0.8151 0.0301
-7.750 -0.5287 0.01171 0.00578 -0.0717 0.8077 0.0317
-7.500 -0.5026 0.01140 0.00546 -0.0717 0.8006 0.0334
-7.250 -0.4758 0.01118 0.00519 -0.0717 0.7934 0.0350
-7.000 -0.4487 0.01100 0.00495 -0.0717 0.7868 0.0361
-6.750 -0.4225 0.01058 0.00451 -0.0717 0.7798 0.0388
-6.500 -0.3955 0.01037 0.00425 -0.0717 0.7730 0.0409
-6.250 -0.3675 0.01018 0.00404 -0.0718 0.7667 0.0427
-6.000 -0.3404 0.00987 0.00371 -0.0719 0.7600 0.0469
-5.750 -0.3126 0.00968 0.00349 -0.0720 0.7537 0.0504
-5.500 -0.2849 0.00939 0.00324 -0.0722 0.7470 0.0585
-5.250 -0.2574 0.00910 0.00298 -0.0724 0.7407 0.0751
-5.000 -0.2298 0.00870 0.00273 -0.0727 0.7345 0.1078
-4.750 -0.2022 0.00829 0.00248 -0.0730 0.7279 0.1517
-4.500 -0.1746 0.00784 0.00223 -0.0734 0.7219 0.2094
-4.250 -0.1467 0.00728 0.00197 -0.0739 0.7157 0.2880
-4.000 -0.1185 0.00686 0.00178 -0.0744 0.7094 0.3602
-3.750 -0.0897 0.00663 0.00167 -0.0748 0.7034 0.4069
-3.500 -0.0606 0.00649 0.00160 -0.0751 0.6971 0.4380
-3.250 -0.0315 0.00642 0.00154 -0.0754 0.6911 0.4593
-3.000 -0.0021 0.00636 0.00150 -0.0757 0.6852 0.4753
-2.750 0.0272 0.00633 0.00146 -0.0760 0.6789 0.4893
-2.500 0.0562 0.00631 0.00144 -0.0763 0.6729 0.5068
-2.000 0.1150 0.00626 0.00141 -0.0769 0.6611 0.5369
-1.750 0.1442 0.00626 0.00140 -0.0771 0.6554 0.5457
-1.500 0.1737 0.00626 0.00139 -0.0774 0.6493 0.5556
-1.250 0.2027 0.00626 0.00140 -0.0777 0.6434 0.5659
-1.000 0.2321 0.00629 0.00140 -0.0780 0.6380 0.5732
-0.750 0.2615 0.00627 0.00140 -0.0782 0.6320 0.5802
-0.500 0.2905 0.00632 0.00141 -0.0785 0.6260 0.5871
-0.250 0.3199 0.00632 0.00142 -0.0788 0.6206 0.5937
0.000 0.3492 0.00633 0.00144 -0.0790 0.6147 0.6007
0.250 0.3781 0.00640 0.00146 -0.0793 0.6087 0.6070
0.500 0.4075 0.00638 0.00149 -0.0796 0.6032 0.6134
0.750 0.4366 0.00643 0.00152 -0.0798 0.5970 0.6200
1.000 0.4655 0.00647 0.00155 -0.0800 0.5910 0.6260
1.250 0.4948 0.00648 0.00160 -0.0803 0.5850 0.6322
1.500 0.5237 0.00655 0.00164 -0.0805 0.5789 0.6385
1.750 0.5527 0.00658 0.00169 -0.0808 0.5732 0.6449
2.000 0.5818 0.00662 0.00175 -0.0810 0.5671 0.6515
2.250 0.6104 0.00670 0.00181 -0.0812 0.5608 0.6575
2.500 0.6394 0.00672 0.00187 -0.0814 0.5544 0.6640
2.750 0.6678 0.00680 0.00194 -0.0816 0.5458 0.6709
3.000 0.6966 0.00685 0.00201 -0.0818 0.5371 0.6773
3.250 0.7249 0.00694 0.00209 -0.0819 0.5291 0.6840
3.750 0.7816 0.00709 0.00227 -0.0821 0.5097 0.6972
4.000 0.8095 0.00721 0.00237 -0.0822 0.4970 0.7044
4.250 0.8374 0.00731 0.00247 -0.0823 0.4831 0.7109
4.500 0.8647 0.00746 0.00259 -0.0822 0.4666 0.7177
4.750 0.8923 0.00761 0.00272 -0.0823 0.4520 0.7246
5.000 0.9195 0.00775 0.00287 -0.0822 0.4371 0.7315
5.250 0.9461 0.00797 0.00304 -0.0821 0.4182 0.7387
5.500 0.9719 0.00823 0.00323 -0.0819 0.3925 0.7454
5.750 0.9960 0.00862 0.00350 -0.0814 0.3566 0.7528
6.000 1.0185 0.00916 0.00385 -0.0807 0.3119 0.7600
6.250 1.0392 0.00982 0.00429 -0.0798 0.2631 0.7675
6.500 1.0583 0.01059 0.00480 -0.0786 0.2094 0.7753
6.750 1.0769 0.01135 0.00533 -0.0774 0.1628 0.7835
7.000 1.0957 0.01206 0.00584 -0.0762 0.1257 0.7919
7.250 1.1149 0.01268 0.00634 -0.0750 0.0971 0.8007
7.500 1.1338 0.01330 0.00685 -0.0738 0.0744 0.8099
7.750 1.1524 0.01388 0.00735 -0.0725 0.0574 0.8199
8.000 1.1711 0.01442 0.00785 -0.0712 0.0467 0.8296
8.250 1.1905 0.01487 0.00831 -0.0700 0.0414 0.8404
8.500 1.2091 0.01530 0.00878 -0.0686 0.0378 0.8521
8.750 1.2265 0.01572 0.00924 -0.0671 0.0351 0.8646
9.000 1.2385 0.01621 0.00978 -0.0645 0.0325 0.8800
9.250 1.2521 0.01656 0.01022 -0.0622 0.0313 0.8995
9.500 1.2612 0.01693 0.01070 -0.0591 0.0299 0.9304
9.750 1.2714 0.01744 0.01128 -0.0566 0.0284 1.0000
10.000 1.2843 0.01817 0.01203 -0.0548 0.0269 1.0000
10.250 1.3000 0.01876 0.01266 -0.0536 0.0258 1.0000
10.500 1.3140 0.01948 0.01340 -0.0522 0.0246 1.0000
10.750 1.3241 0.02045 0.01438 -0.0504 0.0231 1.0000
11.000 1.3359 0.02137 0.01534 -0.0489 0.0222 1.0000
11.250 1.3496 0.02220 0.01621 -0.0478 0.0211 1.0000
11.500 1.3619 0.02314 0.01718 -0.0465 0.0203 1.0000
11.750 1.3703 0.02441 0.01847 -0.0451 0.0192 1.0000
12.000 1.3779 0.02579 0.01990 -0.0437 0.0184 1.0000
12.250 1.3901 0.02687 0.02103 -0.0427 0.0178 1.0000
12.500 1.4013 0.02806 0.02227 -0.0418 0.0172 1.0000
12.750 1.4120 0.02932 0.02355 -0.0409 0.0166 1.0000
13.000 1.4201 0.03083 0.02511 -0.0400 0.0160 1.0000
13.250 1.4228 0.03285 0.02718 -0.0389 0.0154 1.0000
13.500 1.4282 0.03471 0.02911 -0.0380 0.0151 1.0000
13.750 1.4362 0.03638 0.03085 -0.0374 0.0148 1.0000
14.000 1.4436 0.03815 0.03269 -0.0368 0.0145 1.0000
14.250 1.4493 0.04014 0.03474 -0.0363 0.0142 1.0000
14.500 1.4557 0.04211 0.03677 -0.0359 0.0140 1.0000
14.750 1.4609 0.04425 0.03898 -0.0356 0.0137 1.0000
15.000 1.4656 0.04654 0.04133 -0.0354 0.0134 1.0000
15.250 1.4693 0.04899 0.04384 -0.0354 0.0132 1.0000
15.500 1.4713 0.05169 0.04660 -0.0354 0.0129 1.0000
15.750 1.4711 0.05476 0.04975 -0.0356 0.0128 1.0000
16.000 1.4672 0.05838 0.05345 -0.0360 0.0125 1.0000
16.250 1.4596 0.06257 0.05774 -0.0366 0.0123 1.0000
16.500 1.4621 0.06558 0.06084 -0.0371 0.0122 1.0000
16.750 1.4631 0.06888 0.06423 -0.0379 0.0121 1.0000
17.000 1.4646 0.07218 0.06762 -0.0387 0.0120 1.0000
17.250 1.4640 0.07582 0.07136 -0.0397 0.0119 1.0000
17.500 1.4634 0.07955 0.07518 -0.0408 0.0118 1.0000
17.750 1.4626 0.08339 0.07911 -0.0421 0.0116 1.0000
18.000 1.4611 0.08742 0.08324 -0.0436 0.0115 1.0000
18.250 1.4582 0.09172 0.08764 -0.0452 0.0114 1.0000
18.500 1.4555 0.09609 0.09209 -0.0469 0.0112 1.0000
18.750 1.4518 0.10066 0.09676 -0.0488 0.0111 1.0000
19.000 1.4477 0.10540 0.10159 -0.0509 0.0110 1.0000
19.250 1.4429 0.11030 0.10659 -0.0532 0.0109 1.0000
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