NACA 63-215 AIRFOIL (n63215-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: NACA 63-215 AIRFOIL (n63215-il) Reynolds number: 1,000,000 Max Cl/Cd: 98.92 at α=5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-n63215-il-1000000.txt Download as CSV file: xf-n63215-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: NACA 63-215 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
------ -------- --------- --------- -------- -------- --------
-19.750 -1.0256 0.12210 0.11948 -0.0120 1.0000 0.0124
-19.500 -1.0434 0.11429 0.11155 -0.0167 1.0000 0.0124
-19.250 -1.0621 0.10660 0.10373 -0.0212 1.0000 0.0125
-19.000 -1.0750 0.10015 0.09718 -0.0249 1.0000 0.0126
-18.750 -1.0873 0.09395 0.09088 -0.0285 1.0000 0.0126
-18.500 -1.0987 0.08810 0.08492 -0.0317 1.0000 0.0127
-18.250 -1.1104 0.08239 0.07911 -0.0348 1.0000 0.0128
-18.000 -1.1174 0.07754 0.07417 -0.0374 1.0000 0.0129
-17.750 -1.1238 0.07295 0.06949 -0.0397 1.0000 0.0130
-17.500 -1.1319 0.06828 0.06471 -0.0419 1.0000 0.0130
-17.250 -1.1346 0.06444 0.06079 -0.0438 1.0000 0.0132
-17.000 -1.1398 0.06048 0.05673 -0.0455 1.0000 0.0132
-16.750 -1.1417 0.05700 0.05316 -0.0469 1.0000 0.0134
-16.500 -1.1425 0.05378 0.04985 -0.0482 1.0000 0.0135
-16.250 -1.1420 0.05082 0.04680 -0.0492 1.0000 0.0137
-16.000 -1.1409 0.04802 0.04391 -0.0501 1.0000 0.0139
-15.750 -1.1419 0.04513 0.04093 -0.0507 1.0000 0.0140
-15.500 -1.1375 0.04290 0.03861 -0.0512 1.0000 0.0142
-15.250 -1.1341 0.04063 0.03626 -0.0516 1.0000 0.0143
-15.000 -1.1265 0.03882 0.03437 -0.0519 1.0000 0.0145
-14.750 -1.1221 0.03675 0.03222 -0.0520 1.0000 0.0147
-14.500 -1.1261 0.03401 0.02938 -0.0518 1.0000 0.0150
-14.250 -1.1229 0.03198 0.02729 -0.0515 1.0000 0.0152
-14.000 -1.1174 0.03020 0.02547 -0.0513 1.0000 0.0155
-13.750 -1.1098 0.02866 0.02387 -0.0509 1.0000 0.0157
-13.500 -1.0993 0.02739 0.02256 -0.0505 1.0000 0.0160
-13.250 -1.0891 0.02615 0.02128 -0.0500 1.0000 0.0163
-13.000 -1.0785 0.02497 0.02005 -0.0493 1.0000 0.0166
-12.750 -1.0680 0.02383 0.01886 -0.0486 1.0000 0.0170
-12.500 -1.0571 0.02277 0.01774 -0.0477 1.0000 0.0172
-12.250 -1.0441 0.02190 0.01682 -0.0469 1.0000 0.0175
-12.000 -1.0309 0.02109 0.01595 -0.0459 1.0000 0.0178
-11.750 -1.0251 0.01992 0.01472 -0.0442 1.0000 0.0182
-11.500 -1.0212 0.01886 0.01362 -0.0419 1.0000 0.0186
-11.250 -1.0136 0.01816 0.01291 -0.0396 1.0000 0.0191
-11.000 -0.9967 0.01770 0.01244 -0.0384 1.0000 0.0197
-10.750 -0.9597 0.01702 0.01171 -0.0414 0.9706 0.0204
-10.500 -0.9259 0.01645 0.01107 -0.0435 0.9461 0.0212
-10.250 -0.9048 0.01613 0.01063 -0.0427 0.9216 0.0217
-10.000 -0.8912 0.01543 0.00982 -0.0409 0.9016 0.0225
-9.750 -0.8726 0.01495 0.00929 -0.0397 0.8872 0.0234
-9.500 -0.8512 0.01462 0.00888 -0.0389 0.8751 0.0243
-9.250 -0.8286 0.01430 0.00851 -0.0383 0.8639 0.0253
-9.000 -0.8046 0.01406 0.00820 -0.0378 0.8542 0.0261
-8.500 -0.7607 0.01310 0.00714 -0.0365 0.8354 0.0290
-8.250 -0.7363 0.01282 0.00680 -0.0361 0.8271 0.0303
-8.000 -0.7105 0.01258 0.00652 -0.0360 0.8190 0.0313
-7.500 -0.6617 0.01180 0.00566 -0.0353 0.8035 0.0353
-7.250 -0.6356 0.01157 0.00538 -0.0352 0.7961 0.0370
-7.000 -0.6099 0.01123 0.00501 -0.0350 0.7890 0.0395
-6.750 -0.5838 0.01094 0.00471 -0.0349 0.7816 0.0424
-6.500 -0.5569 0.01074 0.00446 -0.0349 0.7749 0.0447
-6.250 -0.5307 0.01039 0.00413 -0.0348 0.7678 0.0508
-5.750 -0.4779 0.00972 0.00355 -0.0347 0.7543 0.0784
-5.500 -0.4519 0.00929 0.00324 -0.0347 0.7475 0.1093
-5.250 -0.4259 0.00882 0.00295 -0.0348 0.7411 0.1508
-5.000 -0.3997 0.00832 0.00265 -0.0349 0.7342 0.2020
-4.750 -0.3739 0.00778 0.00234 -0.0349 0.7278 0.2664
-4.500 -0.3474 0.00723 0.00208 -0.0351 0.7216 0.3365
-4.250 -0.3199 0.00689 0.00191 -0.0353 0.7149 0.3917
-4.000 -0.2916 0.00671 0.00180 -0.0355 0.7087 0.4234
-3.750 -0.2628 0.00658 0.00171 -0.0358 0.7022 0.4454
-3.500 -0.2341 0.00650 0.00164 -0.0360 0.6960 0.4637
-3.250 -0.2050 0.00643 0.00158 -0.0363 0.6899 0.4793
-3.000 -0.1759 0.00637 0.00153 -0.0365 0.6833 0.4940
-2.750 -0.1470 0.00633 0.00149 -0.0367 0.6772 0.5105
-2.500 -0.1177 0.00628 0.00146 -0.0370 0.6712 0.5258
-2.250 -0.0885 0.00627 0.00143 -0.0373 0.6650 0.5365
-2.000 -0.0593 0.00624 0.00140 -0.0375 0.6590 0.5446
-1.750 -0.0299 0.00624 0.00138 -0.0378 0.6526 0.5545
-1.500 -0.0009 0.00623 0.00137 -0.0380 0.6467 0.5643
-1.250 0.0286 0.00623 0.00135 -0.0383 0.6410 0.5713
-1.000 0.0578 0.00621 0.00134 -0.0386 0.6348 0.5781
-0.750 0.0870 0.00624 0.00133 -0.0388 0.6287 0.5847
-0.500 0.1165 0.00622 0.00133 -0.0391 0.6231 0.5910
-0.250 0.1457 0.00622 0.00134 -0.0394 0.6171 0.5978
0.000 0.1750 0.00626 0.00134 -0.0396 0.6112 0.6040
0.250 0.2043 0.00624 0.00136 -0.0399 0.6053 0.6104
0.500 0.2335 0.00628 0.00137 -0.0402 0.5990 0.6168
0.750 0.2627 0.00629 0.00139 -0.0404 0.5931 0.6227
1.000 0.2920 0.00630 0.00142 -0.0407 0.5867 0.6290
1.250 0.3210 0.00637 0.00145 -0.0409 0.5804 0.6350
1.500 0.3503 0.00636 0.00149 -0.0412 0.5746 0.6412
1.750 0.3794 0.00639 0.00153 -0.0415 0.5682 0.6478
2.000 0.4085 0.00645 0.00157 -0.0417 0.5619 0.6538
2.250 0.4376 0.00646 0.00162 -0.0419 0.5540 0.6600
2.500 0.4664 0.00652 0.00167 -0.0421 0.5448 0.6667
2.750 0.4953 0.00656 0.00172 -0.0423 0.5361 0.6730
3.000 0.5242 0.00661 0.00180 -0.0425 0.5285 0.6797
3.250 0.5530 0.00669 0.00186 -0.0427 0.5183 0.6859
3.500 0.5814 0.00674 0.00193 -0.0429 0.5050 0.6925
3.750 0.6098 0.00684 0.00201 -0.0430 0.4904 0.6994
4.000 0.6380 0.00695 0.00210 -0.0431 0.4748 0.7059
4.250 0.6661 0.00706 0.00220 -0.0432 0.4601 0.7126
4.500 0.6942 0.00720 0.00232 -0.0433 0.4435 0.7193
4.750 0.7217 0.00735 0.00245 -0.0433 0.4244 0.7261
5.000 0.7488 0.00757 0.00261 -0.0433 0.4006 0.7332
5.250 0.7749 0.00788 0.00281 -0.0432 0.3661 0.7398
5.500 0.7988 0.00839 0.00312 -0.0428 0.3142 0.7469
5.750 0.8215 0.00903 0.00350 -0.0422 0.2567 0.7540
6.000 0.8434 0.00969 0.00393 -0.0416 0.2039 0.7612
6.250 0.8654 0.01035 0.00436 -0.0409 0.1569 0.7686
6.500 0.8870 0.01097 0.00479 -0.0402 0.1172 0.7758
6.750 0.9091 0.01154 0.00522 -0.0395 0.0877 0.7838
7.000 0.9314 0.01205 0.00564 -0.0389 0.0668 0.7913
7.250 0.9541 0.01250 0.00604 -0.0382 0.0533 0.7996
7.500 0.9769 0.01291 0.00644 -0.0376 0.0455 0.8076
7.750 0.9997 0.01331 0.00683 -0.0370 0.0409 0.8164
8.000 1.0224 0.01366 0.00722 -0.0363 0.0377 0.8249
8.250 1.0449 0.01402 0.00761 -0.0356 0.0354 0.8345
8.500 1.0646 0.01451 0.00813 -0.0345 0.0326 0.8446
8.750 1.0867 0.01481 0.00850 -0.0337 0.0314 0.8550
9.000 1.1073 0.01517 0.00891 -0.0327 0.0298 0.8670
9.250 1.1245 0.01564 0.00943 -0.0312 0.0281 0.8810
9.500 1.1402 0.01611 0.00998 -0.0293 0.0267 0.8979
9.750 1.1542 0.01639 0.01037 -0.0271 0.0256 0.9211
10.000 1.1689 0.01670 0.01079 -0.0251 0.0244 1.0000
10.250 1.1806 0.01739 0.01148 -0.0231 0.0230 1.0000
10.500 1.1933 0.01808 0.01220 -0.0214 0.0221 1.0000
10.750 1.2084 0.01867 0.01283 -0.0200 0.0212 1.0000
11.000 1.2225 0.01934 0.01353 -0.0187 0.0204 1.0000
11.250 1.2352 0.02013 0.01433 -0.0173 0.0197 1.0000
11.500 1.2411 0.02138 0.01562 -0.0154 0.0186 1.0000
11.750 1.2520 0.02239 0.01668 -0.0141 0.0183 1.0000
12.000 1.2646 0.02332 0.01767 -0.0131 0.0179 1.0000
12.250 1.2767 0.02433 0.01872 -0.0121 0.0174 1.0000
12.500 1.2874 0.02547 0.01990 -0.0111 0.0170 1.0000
12.750 1.2981 0.02665 0.02112 -0.0102 0.0165 1.0000
13.000 1.3071 0.02800 0.02251 -0.0093 0.0160 1.0000
13.250 1.3142 0.02954 0.02409 -0.0084 0.0157 1.0000
13.500 1.3152 0.03166 0.02628 -0.0073 0.0153 1.0000
13.750 1.3197 0.03354 0.02823 -0.0066 0.0150 1.0000
14.000 1.3265 0.03528 0.03004 -0.0061 0.0149 1.0000
14.250 1.3357 0.03685 0.03167 -0.0057 0.0146 1.0000
14.500 1.3421 0.03870 0.03360 -0.0054 0.0144 1.0000
14.750 1.3481 0.04066 0.03561 -0.0051 0.0141 1.0000
15.000 1.3519 0.04288 0.03792 -0.0050 0.0139 1.0000
15.250 1.3572 0.04503 0.04012 -0.0050 0.0136 1.0000
15.500 1.3605 0.04746 0.04263 -0.0051 0.0135 1.0000
15.750 1.3641 0.04995 0.04518 -0.0053 0.0133 1.0000
16.000 1.3676 0.05251 0.04781 -0.0057 0.0132 1.0000
16.250 1.3684 0.05545 0.05083 -0.0062 0.0130 1.0000
16.500 1.3687 0.05856 0.05400 -0.0068 0.0128 1.0000
16.750 1.3668 0.06204 0.05757 -0.0077 0.0127 1.0000
17.000 1.3611 0.06609 0.06170 -0.0088 0.0125 1.0000
17.250 1.3550 0.07033 0.06603 -0.0101 0.0123 1.0000
17.500 1.3454 0.07516 0.07099 -0.0117 0.0121 1.0000
17.750 1.3444 0.07898 0.07490 -0.0132 0.0121 1.0000
18.000 1.3420 0.08306 0.07908 -0.0148 0.0120 1.0000
18.250 1.3397 0.08728 0.08340 -0.0167 0.0120 1.0000
18.500 1.3356 0.09183 0.08806 -0.0187 0.0119 1.0000
18.750 1.3320 0.09642 0.09275 -0.0209 0.0118 1.0000
19.000 1.3257 0.10153 0.09797 -0.0234 0.0118 1.0000
19.250 1.3204 0.10660 0.10314 -0.0260 0.0117 1.0000
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