NACA 63 (naca633418-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: NACA 63 (naca633418-il) Reynolds number: 1,000,000 Max Cl/Cd: 120.54 at α=6.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-naca633418-il-1000000.txt Download as CSV file: xf-naca633418-il-1000000.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 = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.0444 0.09303 0.08947 -0.0509 1.0000 0.0179
-19.500 -1.0512 0.08859 0.08496 -0.0530 1.0000 0.0181
-19.250 -1.0557 0.08443 0.08075 -0.0551 1.0000 0.0184
-19.000 -1.0629 0.08014 0.07638 -0.0569 1.0000 0.0184
-18.750 -1.0651 0.07646 0.07264 -0.0587 1.0000 0.0186
-18.500 -1.0689 0.07266 0.06877 -0.0603 1.0000 0.0187
-18.250 -1.0674 0.06952 0.06557 -0.0618 1.0000 0.0191
-18.000 -1.0669 0.06637 0.06236 -0.0631 1.0000 0.0193
-17.750 -1.0692 0.06300 0.05891 -0.0644 1.0000 0.0194
-17.500 -1.0690 0.05993 0.05577 -0.0655 1.0000 0.0195
-17.250 -1.0620 0.05762 0.05339 -0.0665 1.0000 0.0201
-17.000 -1.0580 0.05508 0.05078 -0.0674 1.0000 0.0203
-16.750 -1.0593 0.05209 0.04772 -0.0682 1.0000 0.0203
-16.500 -1.0510 0.05006 0.04562 -0.0690 1.0000 0.0206
-16.250 -1.0539 0.04704 0.04254 -0.0697 1.0000 0.0208
-16.000 -1.0550 0.04426 0.03971 -0.0703 1.0000 0.0210
-15.750 -1.0528 0.04185 0.03727 -0.0708 1.0000 0.0214
-15.500 -1.0498 0.03961 0.03496 -0.0711 1.0000 0.0216
-15.250 -1.0437 0.03772 0.03304 -0.0713 1.0000 0.0219
-15.000 -1.0372 0.03596 0.03124 -0.0714 1.0000 0.0222
-14.750 -1.0299 0.03430 0.02953 -0.0714 1.0000 0.0225
-14.500 -1.0229 0.03265 0.02783 -0.0712 1.0000 0.0229
-14.250 -1.0142 0.03118 0.02633 -0.0711 1.0000 0.0233
-14.000 -1.0055 0.02976 0.02485 -0.0708 1.0000 0.0236
-13.750 -0.9928 0.02868 0.02373 -0.0705 1.0000 0.0240
-13.500 -0.9893 0.02696 0.02196 -0.0699 1.0000 0.0243
-13.250 -0.9863 0.02528 0.02026 -0.0691 1.0000 0.0249
-13.000 -0.9666 0.02387 0.01883 -0.0706 0.9745 0.0256
-12.750 -0.9177 0.02258 0.01749 -0.0775 0.9589 0.0265
-12.500 -0.8677 0.02146 0.01628 -0.0842 0.9382 0.0275
-12.250 -0.8429 0.02051 0.01515 -0.0859 0.9025 0.0282
-12.000 -0.8377 0.01943 0.01395 -0.0843 0.8781 0.0292
-11.750 -0.8281 0.01862 0.01306 -0.0828 0.8621 0.0300
-11.500 -0.8170 0.01793 0.01228 -0.0814 0.8488 0.0308
-11.250 -0.8049 0.01726 0.01154 -0.0800 0.8374 0.0316
-11.000 -0.7918 0.01670 0.01090 -0.0786 0.8278 0.0324
-10.750 -0.7878 0.01586 0.01000 -0.0760 0.8176 0.0335
-10.500 -0.7811 0.01530 0.00939 -0.0735 0.8089 0.0346
-10.250 -0.7639 0.01488 0.00892 -0.0724 0.8010 0.0359
-10.000 -0.7441 0.01455 0.00853 -0.0716 0.7936 0.0372
-9.750 -0.7259 0.01403 0.00800 -0.0706 0.7866 0.0393
-9.500 -0.7048 0.01367 0.00759 -0.0699 0.7799 0.0412
-9.250 -0.6816 0.01338 0.00726 -0.0695 0.7738 0.0430
-9.000 -0.6599 0.01293 0.00681 -0.0690 0.7671 0.0459
-8.750 -0.6361 0.01265 0.00648 -0.0686 0.7606 0.0486
-8.500 -0.6123 0.01229 0.00612 -0.0683 0.7548 0.0522
-8.250 -0.5872 0.01200 0.00582 -0.0681 0.7486 0.0562
-8.000 -0.5628 0.01167 0.00547 -0.0679 0.7424 0.0615
-7.750 -0.5371 0.01137 0.00518 -0.0678 0.7366 0.0676
-7.500 -0.5112 0.01107 0.00490 -0.0678 0.7306 0.0751
-7.250 -0.4855 0.01076 0.00460 -0.0677 0.7247 0.0854
-7.000 -0.4595 0.01042 0.00432 -0.0677 0.7191 0.0991
-6.750 -0.4333 0.01005 0.00403 -0.0678 0.7131 0.1171
-6.500 -0.4070 0.00972 0.00375 -0.0679 0.7072 0.1387
-6.250 -0.3805 0.00933 0.00347 -0.0680 0.7019 0.1672
-6.000 -0.3540 0.00887 0.00318 -0.0683 0.6962 0.2051
-5.750 -0.3273 0.00843 0.00289 -0.0685 0.6903 0.2496
-5.500 -0.3005 0.00798 0.00262 -0.0688 0.6849 0.2998
-5.250 -0.2726 0.00759 0.00241 -0.0692 0.6798 0.3466
-5.000 -0.2441 0.00735 0.00227 -0.0695 0.6743 0.3828
-4.750 -0.2154 0.00723 0.00217 -0.0698 0.6685 0.4070
-4.500 -0.1859 0.00711 0.00209 -0.0702 0.6637 0.4255
-4.250 -0.1565 0.00704 0.00203 -0.0706 0.6582 0.4404
-4.000 -0.1272 0.00701 0.00197 -0.0709 0.6530 0.4526
-3.750 -0.0977 0.00696 0.00193 -0.0712 0.6483 0.4641
-3.500 -0.0680 0.00693 0.00189 -0.0716 0.6434 0.4737
-3.250 -0.0385 0.00690 0.00185 -0.0719 0.6381 0.4829
-3.000 -0.0092 0.00692 0.00183 -0.0722 0.6328 0.4914
-2.750 0.0206 0.00687 0.00181 -0.0726 0.6283 0.5003
-2.500 0.0504 0.00689 0.00179 -0.0729 0.6233 0.5078
-2.250 0.0797 0.00688 0.00178 -0.0732 0.6185 0.5157
-2.000 0.1093 0.00691 0.00177 -0.0736 0.6140 0.5225
-1.750 0.1391 0.00688 0.00176 -0.0740 0.6095 0.5284
-1.500 0.1686 0.00688 0.00176 -0.0743 0.6045 0.5344
-1.250 0.1979 0.00693 0.00176 -0.0746 0.5994 0.5397
-1.000 0.2277 0.00693 0.00176 -0.0750 0.5954 0.5447
-0.750 0.2573 0.00692 0.00177 -0.0753 0.5911 0.5501
-0.500 0.2868 0.00694 0.00178 -0.0756 0.5864 0.5551
-0.250 0.3160 0.00702 0.00179 -0.0759 0.5813 0.5594
0.000 0.3457 0.00700 0.00181 -0.0763 0.5774 0.5647
0.250 0.3753 0.00700 0.00183 -0.0766 0.5731 0.5695
0.500 0.4046 0.00704 0.00186 -0.0769 0.5685 0.5743
0.750 0.4336 0.00713 0.00189 -0.0772 0.5634 0.5786
1.000 0.4633 0.00711 0.00193 -0.0776 0.5596 0.5838
1.250 0.4927 0.00713 0.00197 -0.0779 0.5551 0.5887
1.500 0.5218 0.00719 0.00200 -0.0782 0.5501 0.5935
1.750 0.5507 0.00726 0.00206 -0.0784 0.5452 0.5983
2.000 0.5802 0.00726 0.00211 -0.0788 0.5409 0.6033
2.250 0.6094 0.00730 0.00216 -0.0790 0.5361 0.6083
2.500 0.6381 0.00739 0.00223 -0.0792 0.5310 0.6130
2.750 0.6671 0.00743 0.00229 -0.0795 0.5265 0.6183
3.000 0.6963 0.00746 0.00237 -0.0798 0.5216 0.6235
3.250 0.7250 0.00753 0.00244 -0.0800 0.5165 0.6285
3.500 0.7534 0.00764 0.00252 -0.0802 0.5108 0.6330
3.750 0.7824 0.00765 0.00260 -0.0805 0.5048 0.6385
4.000 0.8105 0.00774 0.00268 -0.0806 0.4980 0.6441
4.250 0.8390 0.00783 0.00278 -0.0808 0.4922 0.6492
4.500 0.8676 0.00789 0.00287 -0.0810 0.4860 0.6544
5.000 0.9233 0.00808 0.00308 -0.0811 0.4683 0.6650
5.250 0.9505 0.00822 0.00319 -0.0811 0.4574 0.6700
5.500 0.9778 0.00833 0.00333 -0.0811 0.4480 0.6759
5.750 1.0052 0.00845 0.00347 -0.0811 0.4395 0.6815
6.000 1.0318 0.00863 0.00362 -0.0810 0.4289 0.6867
6.250 1.0583 0.00878 0.00378 -0.0809 0.4159 0.6920
6.500 1.0835 0.00901 0.00397 -0.0805 0.3987 0.6978
6.750 1.1079 0.00929 0.00419 -0.0801 0.3799 0.7036
7.000 1.1310 0.00962 0.00445 -0.0795 0.3565 0.7091
7.250 1.1513 0.01009 0.00481 -0.0784 0.3260 0.7150
7.500 1.1697 0.01066 0.00523 -0.0771 0.2941 0.7209
7.750 1.1864 0.01128 0.00570 -0.0755 0.2618 0.7265
8.000 1.2010 0.01194 0.00622 -0.0735 0.2297 0.7330
8.250 1.2139 0.01262 0.00676 -0.0713 0.2009 0.7395
8.500 1.2246 0.01325 0.00728 -0.0687 0.1758 0.7458
9.000 1.2371 0.01460 0.00847 -0.0621 0.1374 0.7601
9.250 1.2433 0.01535 0.00917 -0.0590 0.1208 0.7679
9.500 1.2498 0.01617 0.00995 -0.0563 0.1066 0.7763
9.750 1.2561 0.01705 0.01080 -0.0537 0.0943 0.7847
10.000 1.2633 0.01798 0.01171 -0.0514 0.0840 0.7941
10.250 1.2701 0.01897 0.01271 -0.0492 0.0748 0.8042
10.500 1.2769 0.02004 0.01378 -0.0472 0.0672 0.8155
10.750 1.2849 0.02108 0.01486 -0.0454 0.0615 0.8283
11.000 1.2936 0.02211 0.01594 -0.0437 0.0569 0.8432
11.250 1.2999 0.02329 0.01717 -0.0419 0.0526 0.8629
11.500 1.3070 0.02432 0.01832 -0.0400 0.0495 0.8938
11.750 1.3157 0.02545 0.01960 -0.0389 0.0464 1.0000
12.000 1.3254 0.02676 0.02092 -0.0379 0.0437 1.0000
12.250 1.3347 0.02811 0.02229 -0.0370 0.0413 1.0000
12.500 1.3404 0.02978 0.02395 -0.0360 0.0388 1.0000
12.750 1.3509 0.03111 0.02533 -0.0353 0.0372 1.0000
13.000 1.3589 0.03267 0.02691 -0.0346 0.0355 1.0000
13.250 1.3640 0.03451 0.02876 -0.0338 0.0337 1.0000
13.500 1.3726 0.03612 0.03042 -0.0332 0.0326 1.0000
13.750 1.3810 0.03778 0.03211 -0.0327 0.0314 1.0000
14.000 1.3875 0.03965 0.03401 -0.0323 0.0302 1.0000
14.250 1.3899 0.04198 0.03637 -0.0318 0.0289 1.0000
14.500 1.3981 0.04382 0.03826 -0.0315 0.0282 1.0000
14.750 1.4058 0.04572 0.04022 -0.0313 0.0274 1.0000
15.000 1.4120 0.04783 0.04236 -0.0312 0.0267 1.0000
15.250 1.4164 0.05017 0.04474 -0.0311 0.0258 1.0000
15.500 1.4181 0.05286 0.04747 -0.0311 0.0250 1.0000
15.750 1.4211 0.05547 0.05014 -0.0312 0.0244 1.0000
16.000 1.4279 0.05768 0.05241 -0.0313 0.0240 1.0000
16.250 1.4333 0.06012 0.05492 -0.0316 0.0234 1.0000
16.500 1.4379 0.06268 0.05753 -0.0319 0.0228 1.0000
16.750 1.4405 0.06554 0.06043 -0.0324 0.0223 1.0000
17.000 1.4409 0.06872 0.06367 -0.0329 0.0218 1.0000
17.250 1.4383 0.07235 0.06736 -0.0336 0.0212 1.0000
17.500 1.4391 0.07564 0.07072 -0.0344 0.0208 1.0000
17.750 1.4422 0.07864 0.07380 -0.0352 0.0206 1.0000
18.000 1.4448 0.08175 0.07698 -0.0360 0.0202 1.0000
18.250 1.4464 0.08503 0.08033 -0.0370 0.0198 1.0000
18.500 1.4480 0.08838 0.08374 -0.0380 0.0195 1.0000
18.750 1.4472 0.09214 0.08758 -0.0393 0.0192 1.0000
19.000 1.4467 0.09586 0.09136 -0.0406 0.0188 1.0000
19.250 1.4443 0.09992 0.09549 -0.0421 0.0185 1.0000
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