NACA 63(2)-215 MOD B (n63215b-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: NACA 63(2)-215 MOD B (n63215b-il) Reynolds number: 500,000 Max Cl/Cd: 66.36 at α=8.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-n63215b-il-500000.txt Download as CSV file: xf-n63215b-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: NACA 63(2)-215 MOD B
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-17.500 -0.9222 0.09850 0.09497 -0.0290 1.0000 0.0181
-17.250 -0.9430 0.09053 0.08685 -0.0341 1.0000 0.0182
-17.000 -0.9625 0.08323 0.07936 -0.0385 1.0000 0.0182
-16.750 -0.9800 0.07667 0.07262 -0.0423 1.0000 0.0182
-16.500 -0.9920 0.07130 0.06711 -0.0452 1.0000 0.0183
-16.250 -0.9993 0.06689 0.06258 -0.0474 1.0000 0.0184
-16.000 -1.0064 0.06269 0.05825 -0.0493 1.0000 0.0185
-15.750 -1.0116 0.05890 0.05435 -0.0508 1.0000 0.0186
-15.500 -1.0147 0.05556 0.05090 -0.0520 1.0000 0.0187
-15.250 -1.0169 0.05249 0.04772 -0.0529 1.0000 0.0189
-15.000 -1.0183 0.04958 0.04470 -0.0536 1.0000 0.0191
-14.750 -1.0175 0.04702 0.04203 -0.0540 1.0000 0.0193
-14.500 -1.0152 0.04473 0.03965 -0.0543 1.0000 0.0197
-14.250 -1.0128 0.04247 0.03728 -0.0544 1.0000 0.0200
-14.000 -1.0087 0.04040 0.03510 -0.0543 1.0000 0.0202
-13.750 -1.0041 0.03840 0.03298 -0.0540 1.0000 0.0205
-13.500 -0.9984 0.03660 0.03105 -0.0536 1.0000 0.0208
-13.250 -0.9916 0.03495 0.02928 -0.0531 1.0000 0.0211
-13.000 -0.9839 0.03314 0.02738 -0.0523 1.0000 0.0214
-12.750 -0.9746 0.03148 0.02569 -0.0514 1.0000 0.0219
-12.500 -0.9642 0.03019 0.02439 -0.0506 1.0000 0.0223
-12.250 -0.9531 0.02903 0.02321 -0.0499 1.0000 0.0228
-12.000 -0.9418 0.02790 0.02204 -0.0490 1.0000 0.0233
-11.750 -0.9301 0.02681 0.02089 -0.0480 1.0000 0.0238
-11.500 -0.9179 0.02578 0.01981 -0.0469 1.0000 0.0244
-11.250 -0.9054 0.02485 0.01881 -0.0458 1.0000 0.0251
-11.000 -0.8947 0.02370 0.01759 -0.0443 1.0000 0.0259
-10.750 -0.8851 0.02262 0.01654 -0.0428 1.0000 0.0267
-10.500 -0.8740 0.02184 0.01577 -0.0411 1.0000 0.0273
-10.250 -0.8639 0.02121 0.01512 -0.0391 1.0000 0.0283
-10.000 -0.8553 0.02064 0.01452 -0.0367 1.0000 0.0291
-9.750 -0.8364 0.02014 0.01398 -0.0359 0.9955 0.0301
-9.500 -0.8032 0.01887 0.01269 -0.0384 0.9795 0.0315
-9.250 -0.7678 0.01812 0.01196 -0.0408 0.9649 0.0330
-9.000 -0.7352 0.01752 0.01130 -0.0424 0.9502 0.0345
-8.750 -0.7104 0.01712 0.01082 -0.0421 0.9329 0.0357
-8.500 -0.6936 0.01649 0.01011 -0.0405 0.9170 0.0368
-8.250 -0.6771 0.01589 0.00946 -0.0389 0.9037 0.0382
-8.000 -0.6572 0.01547 0.00900 -0.0376 0.8921 0.0395
-7.750 -0.6358 0.01508 0.00856 -0.0366 0.8815 0.0410
-7.500 -0.6135 0.01475 0.00815 -0.0356 0.8725 0.0423
-7.250 -0.5927 0.01418 0.00755 -0.0346 0.8631 0.0443
-7.000 -0.5700 0.01377 0.00710 -0.0338 0.8554 0.0466
-6.750 -0.5456 0.01343 0.00673 -0.0333 0.8473 0.0490
-6.500 -0.5218 0.01305 0.00630 -0.0326 0.8405 0.0521
-6.250 -0.4970 0.01266 0.00593 -0.0321 0.8328 0.0570
-6.000 -0.4725 0.01225 0.00552 -0.0315 0.8260 0.0651
-5.750 -0.4484 0.01171 0.00511 -0.0311 0.8190 0.0877
-5.500 -0.4249 0.01105 0.00468 -0.0306 0.8122 0.1351
-5.250 -0.4012 0.01039 0.00427 -0.0302 0.8060 0.1932
-5.000 -0.3774 0.00961 0.00386 -0.0300 0.7988 0.2740
-4.750 -0.3529 0.00897 0.00354 -0.0297 0.7922 0.3583
-4.500 -0.3261 0.00862 0.00337 -0.0296 0.7836 0.4110
-4.250 -0.2987 0.00844 0.00323 -0.0293 0.7752 0.4452
-4.000 -0.2704 0.00830 0.00314 -0.0292 0.7663 0.4716
-3.500 -0.2132 0.00816 0.00298 -0.0290 0.7501 0.5070
-3.250 -0.1845 0.00812 0.00293 -0.0290 0.7440 0.5217
-3.000 -0.1555 0.00809 0.00291 -0.0290 0.7374 0.5368
-2.750 -0.1266 0.00806 0.00288 -0.0289 0.7301 0.5511
-2.500 -0.0976 0.00806 0.00285 -0.0289 0.7232 0.5631
-2.250 -0.0684 0.00806 0.00282 -0.0289 0.7150 0.5752
-2.000 -0.0398 0.00806 0.00282 -0.0287 0.7067 0.5884
-1.750 -0.0109 0.00802 0.00279 -0.0286 0.6973 0.5975
-1.500 0.0183 0.00802 0.00275 -0.0286 0.6888 0.6047
-1.250 0.0474 0.00800 0.00272 -0.0286 0.6802 0.6118
-1.000 0.0765 0.00799 0.00271 -0.0286 0.6713 0.6186
-0.750 0.1057 0.00800 0.00265 -0.0286 0.6608 0.6251
-0.500 0.1346 0.00796 0.00264 -0.0286 0.6493 0.6309
-0.250 0.1637 0.00798 0.00262 -0.0286 0.6375 0.6374
0.000 0.1925 0.00799 0.00259 -0.0286 0.6238 0.6436
0.250 0.2211 0.00801 0.00259 -0.0285 0.6066 0.6501
0.500 0.2498 0.00807 0.00257 -0.0284 0.5844 0.6569
0.750 0.2772 0.00816 0.00257 -0.0282 0.5506 0.6624
1.000 0.3028 0.00847 0.00261 -0.0277 0.4748 0.6686
1.250 0.3243 0.00932 0.00285 -0.0269 0.3532 0.6748
1.500 0.3508 0.00961 0.00305 -0.0266 0.3247 0.6807
2.000 0.4055 0.01006 0.00333 -0.0264 0.2849 0.6940
2.250 0.4328 0.01026 0.00348 -0.0263 0.2693 0.7007
2.500 0.4605 0.01046 0.00360 -0.0262 0.2555 0.7077
2.750 0.4878 0.01061 0.00375 -0.0261 0.2434 0.7139
3.000 0.5152 0.01082 0.00391 -0.0260 0.2329 0.7214
3.250 0.5421 0.01101 0.00408 -0.0258 0.2231 0.7280
3.500 0.5694 0.01119 0.00425 -0.0256 0.2149 0.7354
3.750 0.5961 0.01143 0.00444 -0.0254 0.2065 0.7424
4.000 0.6231 0.01159 0.00463 -0.0252 0.1996 0.7492
4.250 0.6501 0.01182 0.00481 -0.0251 0.1923 0.7567
4.500 0.6763 0.01201 0.00503 -0.0247 0.1861 0.7630
4.750 0.7033 0.01219 0.00522 -0.0245 0.1804 0.7704
5.000 0.7289 0.01246 0.00545 -0.0242 0.1746 0.7771
5.250 0.7552 0.01266 0.00569 -0.0239 0.1701 0.7847
5.500 0.7816 0.01284 0.00590 -0.0236 0.1653 0.7925
5.750 0.8065 0.01312 0.00615 -0.0231 0.1600 0.8006
6.000 0.8320 0.01337 0.00642 -0.0228 0.1554 0.8086
6.250 0.8577 0.01353 0.00663 -0.0224 0.1511 0.8165
6.500 0.8825 0.01380 0.00689 -0.0219 0.1466 0.8249
6.750 0.9051 0.01419 0.00728 -0.0211 0.1420 0.8335
7.000 0.9306 0.01436 0.00752 -0.0207 0.1391 0.8420
7.250 0.9547 0.01458 0.00779 -0.0200 0.1356 0.8512
7.500 0.9774 0.01488 0.00810 -0.0192 0.1318 0.8605
8.000 1.0201 0.01554 0.00885 -0.0171 0.1253 0.8829
8.250 1.0414 0.01575 0.00913 -0.0160 0.1225 0.8957
8.500 1.0605 0.01598 0.00942 -0.0144 0.1195 0.9113
8.750 1.0751 0.01625 0.00973 -0.0121 0.1167 0.9335
9.000 1.0935 0.01677 0.01027 -0.0108 0.1132 1.0000
9.250 1.1195 0.01706 0.01061 -0.0109 0.1117 1.0000
9.500 1.1436 0.01741 0.01099 -0.0107 0.1096 1.0000
9.750 1.1653 0.01779 0.01139 -0.0101 0.1074 1.0000
10.000 1.1850 0.01821 0.01181 -0.0091 0.1053 1.0000
10.250 1.2023 0.01874 0.01233 -0.0079 0.1031 1.0000
10.500 1.2161 0.01953 0.01309 -0.0063 0.1004 1.0000
10.750 1.2340 0.02006 0.01367 -0.0053 0.0989 1.0000
11.000 1.2529 0.02049 0.01416 -0.0044 0.0974 1.0000
11.250 1.2707 0.02099 0.01471 -0.0035 0.0955 1.0000
11.500 1.2881 0.02150 0.01525 -0.0025 0.0934 1.0000
11.750 1.3036 0.02216 0.01591 -0.0015 0.0915 1.0000
12.000 1.3165 0.02300 0.01674 -0.0003 0.0892 1.0000
12.250 1.3268 0.02412 0.01787 0.0010 0.0867 1.0000
12.500 1.3437 0.02473 0.01856 0.0018 0.0856 1.0000
12.750 1.3599 0.02539 0.01928 0.0025 0.0838 1.0000
13.000 1.3738 0.02626 0.02020 0.0033 0.0824 1.0000
13.250 1.3868 0.02721 0.02121 0.0041 0.0811 1.0000
13.500 1.3983 0.02830 0.02233 0.0050 0.0799 1.0000
13.750 1.4084 0.02949 0.02354 0.0058 0.0783 1.0000
14.000 1.4159 0.03097 0.02505 0.0067 0.0769 1.0000
14.250 1.4204 0.03277 0.02690 0.0076 0.0753 1.0000
14.500 1.4309 0.03407 0.02828 0.0081 0.0746 1.0000
14.750 1.4415 0.03539 0.02969 0.0086 0.0739 1.0000
15.000 1.4514 0.03677 0.03116 0.0089 0.0731 1.0000
15.250 1.4597 0.03835 0.03284 0.0092 0.0723 1.0000
15.500 1.4682 0.03994 0.03450 0.0094 0.0711 1.0000
15.750 1.4745 0.04178 0.03643 0.0095 0.0703 1.0000
16.000 1.4803 0.04371 0.03843 0.0095 0.0694 1.0000
16.250 1.4854 0.04578 0.04056 0.0094 0.0684 1.0000
16.500 1.4885 0.04812 0.04296 0.0091 0.0674 1.0000
16.750 1.4892 0.05081 0.04570 0.0085 0.0663 1.0000
17.000 1.4877 0.05385 0.04882 0.0079 0.0654 1.0000
17.250 1.4828 0.05738 0.05242 0.0071 0.0643 1.0000
17.500 1.4830 0.06047 0.05562 0.0061 0.0638 1.0000
17.750 1.4827 0.06376 0.05903 0.0049 0.0634 1.0000
18.000 1.4812 0.06735 0.06275 0.0034 0.0629 1.0000
18.250 1.4777 0.07131 0.06683 0.0016 0.0624 1.0000
18.500 1.4728 0.07563 0.07128 -0.0005 0.0618 1.0000
18.750 1.4662 0.08038 0.07615 -0.0030 0.0611 1.0000
19.000 1.4575 0.08560 0.08151 -0.0058 0.0605 1.0000
19.250 1.4475 0.09121 0.08724 -0.0090 0.0599 1.0000
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