NACA 64(1)-212 MOD A (n64212ma-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 64(1)-212 MOD A (n64212ma-il) Reynolds number: 200,000 Max Cl/Cd: 48.4 at α=7.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-n64212ma-il-200000-n5.txt Download as CSV file: xf-n64212ma-il-200000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NACA 64(1)-212 MOD A
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-10.250 -0.3926 0.10319 0.09934 -0.0290 1.0000 0.0357
-10.000 -0.3972 0.09820 0.09439 -0.0326 1.0000 0.0358
-9.750 -0.4025 0.09299 0.08921 -0.0363 1.0000 0.0359
-9.500 -0.4012 0.08900 0.08527 -0.0380 1.0000 0.0360
-9.250 -0.3890 0.08743 0.08374 -0.0363 1.0000 0.0365
-9.000 -0.3876 0.08393 0.08028 -0.0378 1.0000 0.0367
-8.750 -0.3845 0.08107 0.07746 -0.0387 1.0000 0.0377
-8.500 -0.3911 0.07652 0.07297 -0.0420 1.0000 0.0381
-8.250 -0.4076 0.07200 0.06850 -0.0453 1.0000 0.0386
-8.000 -0.4264 0.06478 0.06101 -0.0540 0.9718 0.0403
-7.500 -0.4076 0.05169 0.04738 -0.0614 0.9385 0.0314
-7.250 -0.3914 0.04848 0.04399 -0.0626 0.9225 0.0311
-7.000 -0.3780 0.04505 0.04030 -0.0629 0.9069 0.0309
-6.750 -0.3642 0.04191 0.03690 -0.0626 0.8924 0.0308
-6.500 -0.3546 0.03690 0.03121 -0.0612 0.8793 0.0317
-5.750 -0.2995 0.03012 0.02364 -0.0584 0.8420 0.0319
-5.250 -0.2554 0.02694 0.02005 -0.0570 0.8213 0.0323
-5.000 -0.2322 0.02546 0.01834 -0.0562 0.8112 0.0326
-4.750 -0.2081 0.02419 0.01688 -0.0556 0.8003 0.0331
-4.500 -0.1835 0.02308 0.01556 -0.0549 0.7894 0.0341
-4.250 -0.1582 0.02176 0.01398 -0.0543 0.7792 0.0349
-4.000 -0.1324 0.02052 0.01249 -0.0536 0.7691 0.0352
-3.750 -0.1062 0.01944 0.01119 -0.0529 0.7593 0.0356
-3.500 -0.0799 0.01851 0.01008 -0.0523 0.7487 0.0360
-3.250 -0.0539 0.01779 0.00931 -0.0518 0.7377 0.0364
-3.000 -0.0279 0.01718 0.00865 -0.0513 0.7242 0.0370
-2.750 -0.0019 0.01666 0.00807 -0.0507 0.7106 0.0379
-2.500 0.0241 0.01618 0.00749 -0.0501 0.6973 0.0392
-2.250 0.0504 0.01567 0.00689 -0.0495 0.6839 0.0403
-2.000 0.0761 0.01517 0.00637 -0.0490 0.6717 0.0409
-1.750 0.1019 0.01475 0.00595 -0.0484 0.6576 0.0418
-1.500 0.1278 0.01439 0.00556 -0.0479 0.6416 0.0427
-1.250 0.1534 0.01408 0.00517 -0.0473 0.6216 0.0439
-1.000 0.1793 0.01381 0.00482 -0.0468 0.6023 0.0454
-0.750 0.2051 0.01358 0.00456 -0.0464 0.5811 0.0474
-0.500 0.2310 0.01344 0.00431 -0.0459 0.5529 0.0500
-0.250 0.2564 0.01333 0.00406 -0.0454 0.5165 0.0523
0.000 0.2768 0.01376 0.00390 -0.0441 0.3890 0.0550
0.250 0.2959 0.01455 0.00405 -0.0430 0.2554 0.0585
0.500 0.3211 0.01469 0.00404 -0.0426 0.2223 0.0657
0.750 0.3464 0.01479 0.00403 -0.0423 0.1936 0.0813
1.000 0.3671 0.01326 0.00409 -0.0421 0.1760 0.6097
1.250 0.3900 0.01328 0.00434 -0.0408 0.1604 0.6975
1.500 0.4132 0.01343 0.00455 -0.0395 0.1447 0.7440
1.750 0.4362 0.01363 0.00475 -0.0383 0.1339 0.7805
2.000 0.4581 0.01380 0.00495 -0.0367 0.1285 0.8099
2.250 0.4811 0.01398 0.00512 -0.0354 0.1256 0.8303
2.500 0.5054 0.01415 0.00526 -0.0346 0.1237 0.8419
2.750 0.5303 0.01432 0.00540 -0.0339 0.1222 0.8511
3.000 0.5542 0.01449 0.00556 -0.0330 0.1211 0.8614
3.250 0.5780 0.01468 0.00573 -0.0322 0.1201 0.8721
3.500 0.6014 0.01487 0.00591 -0.0312 0.1194 0.8839
3.750 0.6245 0.01506 0.00610 -0.0302 0.1188 0.8958
4.000 0.6478 0.01526 0.00630 -0.0293 0.1181 0.9092
4.250 0.6710 0.01546 0.00650 -0.0284 0.1170 0.9248
4.500 0.6960 0.01569 0.00673 -0.0278 0.1155 0.9424
4.750 0.7252 0.01600 0.00702 -0.0284 0.1136 0.9626
5.000 0.7566 0.01638 0.00734 -0.0295 0.1118 1.0000
5.250 0.7819 0.01672 0.00766 -0.0294 0.1102 1.0000
5.500 0.8067 0.01709 0.00800 -0.0292 0.1089 1.0000
5.750 0.8311 0.01748 0.00837 -0.0289 0.1078 1.0000
6.000 0.8549 0.01789 0.00875 -0.0285 0.1069 1.0000
6.250 0.8782 0.01835 0.00917 -0.0280 0.1060 1.0000
6.500 0.9013 0.01881 0.00961 -0.0275 0.1054 1.0000
6.750 0.9251 0.01919 0.01002 -0.0271 0.1045 1.0000
7.000 0.9483 0.01960 0.01045 -0.0266 0.1033 1.0000
7.250 0.9709 0.02006 0.01090 -0.0260 0.1021 1.0000
7.500 0.9927 0.02056 0.01141 -0.0254 0.1008 1.0000
7.750 1.0137 0.02114 0.01195 -0.0247 0.0997 1.0000
8.000 1.0358 0.02158 0.01244 -0.0240 0.0985 1.0000
8.250 1.0575 0.02202 0.01294 -0.0233 0.0972 1.0000
8.500 1.0779 0.02254 0.01349 -0.0225 0.0953 1.0000
8.750 1.0966 0.02314 0.01406 -0.0215 0.0938 1.0000
9.000 1.1164 0.02351 0.01457 -0.0205 0.0921 1.0000
9.250 1.1347 0.02398 0.01513 -0.0194 0.0899 1.0000
9.500 1.1524 0.02450 0.01569 -0.0182 0.0880 1.0000
9.750 1.1717 0.02488 0.01623 -0.0172 0.0853 1.0000
10.000 1.1908 0.02529 0.01677 -0.0163 0.0822 1.0000
10.250 1.2120 0.02565 0.01733 -0.0155 0.0768 1.0000
10.500 1.2322 0.02584 0.01744 -0.0149 0.0574 1.0000
10.750 1.2455 0.02674 0.01821 -0.0137 0.0541 1.0000
11.000 1.2560 0.02793 0.01941 -0.0122 0.0519 1.0000
11.250 1.2648 0.02925 0.02079 -0.0108 0.0502 1.0000
11.500 1.2747 0.03050 0.02213 -0.0095 0.0487 1.0000
11.750 1.2837 0.03184 0.02356 -0.0083 0.0474 1.0000
12.000 1.2911 0.03332 0.02512 -0.0071 0.0465 1.0000
12.250 1.3009 0.03465 0.02658 -0.0062 0.0453 1.0000
12.500 1.3084 0.03620 0.02823 -0.0053 0.0445 1.0000
12.750 1.3142 0.03794 0.03006 -0.0045 0.0438 1.0000
13.000 1.3200 0.03973 0.03195 -0.0038 0.0432 1.0000
13.250 1.3261 0.04155 0.03389 -0.0032 0.0425 1.0000
13.500 1.3306 0.04357 0.03603 -0.0028 0.0419 1.0000
13.750 1.3339 0.04579 0.03837 -0.0026 0.0414 1.0000
14.000 1.3358 0.04822 0.04091 -0.0025 0.0410 1.0000
14.250 1.3362 0.05090 0.04369 -0.0026 0.0406 1.0000
14.500 1.3356 0.05379 0.04669 -0.0029 0.0403 1.0000
14.750 1.3354 0.05674 0.04977 -0.0034 0.0400 1.0000
15.000 1.3341 0.05996 0.05312 -0.0041 0.0395 1.0000
15.250 1.3316 0.06348 0.05678 -0.0051 0.0390 1.0000
15.500 1.3277 0.06734 0.06077 -0.0064 0.0386 1.0000
15.750 1.3226 0.07155 0.06511 -0.0081 0.0382 1.0000
16.000 1.3161 0.07616 0.06985 -0.0101 0.0379 1.0000
16.250 1.3084 0.08116 0.07497 -0.0124 0.0376 1.0000
16.500 1.2998 0.08651 0.08044 -0.0151 0.0374 1.0000
16.750 1.2904 0.09227 0.08635 -0.0182 0.0370 1.0000
17.000 1.2807 0.09827 0.09250 -0.0215 0.0368 1.0000
17.250 1.2703 0.10451 0.09888 -0.0250 0.0365 1.0000
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