NACA 63(3)-218 (naca633218-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 63(3)-218 (naca633218-il) Reynolds number: 200,000 Max Cl/Cd: 49.62 at α=7.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-naca633218-il-200000-n5.txt Download as CSV file: xf-naca633218-il-200000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NACA 63(3)-218
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
------ -------- --------- --------- -------- -------- --------
-19.250 -0.9017 0.12377 0.11910 -0.0205 1.0000 0.0265
-19.000 -0.9145 0.11710 0.11230 -0.0245 1.0000 0.0267
-18.750 -0.9250 0.11104 0.10611 -0.0281 1.0000 0.0270
-18.500 -0.9346 0.10527 0.10022 -0.0315 1.0000 0.0273
-18.250 -0.9432 0.09985 0.09466 -0.0345 1.0000 0.0276
-18.000 -0.9506 0.09479 0.08946 -0.0373 1.0000 0.0280
-17.750 -0.9575 0.08992 0.08445 -0.0399 1.0000 0.0285
-17.500 -0.9637 0.08528 0.07964 -0.0422 1.0000 0.0290
-17.250 -0.9681 0.08106 0.07525 -0.0442 1.0000 0.0295
-17.000 -0.9721 0.07699 0.07100 -0.0460 1.0000 0.0300
-16.750 -0.9734 0.07342 0.06728 -0.0475 1.0000 0.0305
-16.500 -0.9691 0.07080 0.06464 -0.0484 1.0000 0.0310
-16.250 -0.9654 0.06812 0.06192 -0.0493 1.0000 0.0315
-16.000 -0.9618 0.06544 0.05918 -0.0503 1.0000 0.0321
-15.750 -0.9576 0.06288 0.05655 -0.0511 1.0000 0.0326
-15.500 -0.9530 0.06042 0.05401 -0.0517 1.0000 0.0333
-15.250 -0.9480 0.05804 0.05153 -0.0523 1.0000 0.0340
-15.000 -0.9421 0.05581 0.04917 -0.0527 1.0000 0.0348
-14.750 -0.9358 0.05365 0.04689 -0.0531 1.0000 0.0356
-14.500 -0.9288 0.05170 0.04494 -0.0533 1.0000 0.0363
-14.250 -0.9221 0.04974 0.04297 -0.0536 1.0000 0.0371
-14.000 -0.9144 0.04790 0.04109 -0.0537 1.0000 0.0379
-13.750 -0.9063 0.04613 0.03927 -0.0538 1.0000 0.0389
-13.500 -0.8978 0.04447 0.03754 -0.0538 1.0000 0.0399
-13.250 -0.8885 0.04289 0.03587 -0.0536 1.0000 0.0409
-13.000 -0.8802 0.04127 0.03422 -0.0534 1.0000 0.0418
-12.750 -0.8671 0.03958 0.03250 -0.0546 0.9316 0.0429
-12.500 -0.8453 0.03789 0.03066 -0.0572 0.8893 0.0444
-12.250 -0.8323 0.03651 0.02914 -0.0574 0.8626 0.0457
-12.000 -0.8208 0.03526 0.02773 -0.0571 0.8400 0.0472
-11.750 -0.8119 0.03387 0.02625 -0.0566 0.8229 0.0486
-11.500 -0.8039 0.03247 0.02479 -0.0560 0.8080 0.0501
-11.250 -0.7946 0.03123 0.02344 -0.0553 0.7901 0.0516
-11.000 -0.7850 0.03005 0.02215 -0.0545 0.7741 0.0533
-10.750 -0.7748 0.02895 0.02094 -0.0536 0.7604 0.0551
-10.500 -0.7682 0.02765 0.01958 -0.0524 0.7478 0.0569
-10.250 -0.7600 0.02648 0.01834 -0.0514 0.7352 0.0591
-10.000 -0.7500 0.02544 0.01721 -0.0503 0.7229 0.0615
-9.750 -0.7401 0.02444 0.01611 -0.0491 0.7115 0.0642
-9.500 -0.7321 0.02336 0.01500 -0.0478 0.7003 0.0673
-9.250 -0.7222 0.02245 0.01402 -0.0464 0.6898 0.0717
-9.000 -0.7142 0.02153 0.01305 -0.0446 0.6787 0.0767
-8.750 -0.7059 0.02075 0.01222 -0.0427 0.6683 0.0834
-8.500 -0.6989 0.02004 0.01149 -0.0403 0.6583 0.0911
-8.250 -0.6865 0.01934 0.01080 -0.0388 0.6485 0.1022
-8.000 -0.6724 0.01869 0.01013 -0.0373 0.6382 0.1163
-7.750 -0.6570 0.01803 0.00951 -0.0361 0.6274 0.1345
-7.500 -0.6406 0.01738 0.00890 -0.0350 0.6170 0.1564
-7.250 -0.6240 0.01669 0.00829 -0.0339 0.6050 0.1838
-7.000 -0.6068 0.01601 0.00769 -0.0329 0.5888 0.2172
-6.750 -0.5883 0.01534 0.00715 -0.0321 0.5776 0.2562
-6.500 -0.5688 0.01473 0.00668 -0.0313 0.5658 0.2988
-6.250 -0.5474 0.01424 0.00632 -0.0307 0.5527 0.3421
-6.000 -0.5240 0.01394 0.00610 -0.0303 0.5387 0.3800
-5.750 -0.4991 0.01377 0.00592 -0.0300 0.5231 0.4113
-5.500 -0.4739 0.01368 0.00581 -0.0297 0.5024 0.4375
-5.250 -0.4502 0.01391 0.00572 -0.0292 0.4252 0.4583
-4.750 -0.3986 0.01417 0.00558 -0.0288 0.3550 0.4852
-4.500 -0.3713 0.01417 0.00552 -0.0288 0.3519 0.4958
-4.250 -0.3437 0.01416 0.00544 -0.0288 0.3494 0.5052
-4.000 -0.3161 0.01417 0.00538 -0.0288 0.3475 0.5157
-3.500 -0.2607 0.01421 0.00531 -0.0289 0.3442 0.5342
-3.250 -0.2329 0.01420 0.00523 -0.0290 0.3426 0.5402
-3.000 -0.2051 0.01420 0.00521 -0.0290 0.3410 0.5456
-2.750 -0.1772 0.01421 0.00514 -0.0291 0.3394 0.5517
-2.500 -0.1492 0.01421 0.00506 -0.0292 0.3383 0.5573
-2.250 -0.1215 0.01422 0.00507 -0.0292 0.3374 0.5620
-2.000 -0.0936 0.01423 0.00504 -0.0293 0.3367 0.5676
-1.750 -0.0654 0.01424 0.00497 -0.0295 0.3363 0.5737
-1.500 -0.0376 0.01425 0.00498 -0.0295 0.3359 0.5782
-1.250 -0.0099 0.01428 0.00499 -0.0296 0.3354 0.5829
-1.000 0.0179 0.01431 0.00499 -0.0297 0.3347 0.5883
-0.750 0.0459 0.01435 0.00496 -0.0299 0.3341 0.5936
-0.500 0.0734 0.01438 0.00500 -0.0298 0.3338 0.5974
-0.250 0.1011 0.01442 0.00504 -0.0299 0.3335 0.6020
0.000 0.1289 0.01447 0.00507 -0.0300 0.3332 0.6075
0.250 0.1566 0.01454 0.00509 -0.0301 0.3327 0.6127
0.500 0.1838 0.01461 0.00518 -0.0300 0.3322 0.6167
0.750 0.2111 0.01469 0.00526 -0.0300 0.3316 0.6213
1.000 0.2389 0.01477 0.00531 -0.0301 0.3311 0.6266
1.250 0.2667 0.01483 0.00537 -0.0303 0.3308 0.6321
1.500 0.2940 0.01490 0.00548 -0.0302 0.3306 0.6366
1.750 0.3215 0.01498 0.00558 -0.0302 0.3305 0.6418
2.000 0.3493 0.01506 0.00567 -0.0303 0.3303 0.6472
2.250 0.3768 0.01514 0.00577 -0.0304 0.3300 0.6521
2.500 0.4040 0.01523 0.00592 -0.0303 0.3298 0.6569
2.750 0.4314 0.01533 0.00605 -0.0304 0.3296 0.6627
3.000 0.4592 0.01544 0.00617 -0.0305 0.3293 0.6690
3.250 0.4861 0.01554 0.00634 -0.0304 0.3291 0.6736
3.500 0.5132 0.01565 0.00651 -0.0303 0.3288 0.6789
3.750 0.5406 0.01577 0.00667 -0.0304 0.3282 0.6851
4.000 0.5675 0.01591 0.00685 -0.0304 0.3274 0.6908
4.250 0.5940 0.01605 0.00707 -0.0302 0.3264 0.6963
4.500 0.6208 0.01620 0.00727 -0.0302 0.3253 0.7026
4.750 0.6478 0.01636 0.00747 -0.0302 0.3244 0.7087
5.000 0.6740 0.01652 0.00772 -0.0300 0.3236 0.7141
5.250 0.7004 0.01671 0.00796 -0.0298 0.3225 0.7207
5.500 0.7268 0.01699 0.00824 -0.0298 0.3201 0.7275
5.750 0.7516 0.01725 0.00858 -0.0294 0.3167 0.7330
6.000 0.7761 0.01745 0.00887 -0.0290 0.3127 0.7397
6.250 0.8013 0.01773 0.00918 -0.0288 0.3089 0.7468
6.500 0.8256 0.01804 0.00955 -0.0284 0.3055 0.7529
6.750 0.8474 0.01817 0.00984 -0.0276 0.2993 0.7601
7.000 0.8680 0.01834 0.01013 -0.0267 0.2908 0.7672
7.250 0.8889 0.01833 0.01036 -0.0256 0.2800 0.7743
7.500 0.9076 0.01829 0.01034 -0.0244 0.2167 0.7827
7.750 0.9169 0.01894 0.01087 -0.0220 0.2036 0.7902
8.000 0.9252 0.01963 0.01158 -0.0194 0.1959 0.7991
8.250 0.9379 0.02016 0.01223 -0.0174 0.1890 0.8076
8.500 0.9477 0.02086 0.01302 -0.0152 0.1825 0.8177
8.750 0.9612 0.02141 0.01369 -0.0135 0.1752 0.8273
9.000 0.9748 0.02200 0.01439 -0.0120 0.1669 0.8384
9.250 0.9877 0.02259 0.01509 -0.0104 0.1558 0.8499
9.500 0.9993 0.02329 0.01585 -0.0088 0.1402 0.8633
9.750 1.0054 0.02427 0.01681 -0.0068 0.1240 0.8800
10.000 1.0085 0.02544 0.01798 -0.0047 0.1112 0.9028
10.250 1.0146 0.02679 0.01938 -0.0037 0.1004 0.9440
10.500 1.0204 0.02835 0.02093 -0.0032 0.0915 1.0000
10.750 1.0253 0.03008 0.02265 -0.0026 0.0835 1.0000
11.000 1.0311 0.03180 0.02437 -0.0020 0.0767 1.0000
11.250 1.0351 0.03373 0.02627 -0.0015 0.0711 1.0000
11.500 1.0407 0.03558 0.02815 -0.0011 0.0661 1.0000
11.750 1.0435 0.03772 0.03028 -0.0007 0.0624 1.0000
12.000 1.0493 0.03966 0.03228 -0.0005 0.0595 1.0000
12.250 1.0528 0.04184 0.03450 -0.0003 0.0567 1.0000
12.500 1.0545 0.04425 0.03692 -0.0002 0.0546 1.0000
12.750 1.0592 0.04647 0.03920 -0.0002 0.0525 1.0000
13.000 1.0637 0.04875 0.04155 -0.0003 0.0505 1.0000
13.250 1.0671 0.05121 0.04404 -0.0005 0.0488 1.0000
13.500 1.0683 0.05398 0.04681 -0.0008 0.0472 1.0000
13.750 1.0738 0.05634 0.04925 -0.0011 0.0454 1.0000
14.000 1.0791 0.05875 0.05173 -0.0015 0.0439 1.0000
14.250 1.0835 0.06131 0.05434 -0.0019 0.0426 1.0000
14.500 1.0865 0.06410 0.05715 -0.0026 0.0412 1.0000
14.750 1.0903 0.06680 0.05988 -0.0031 0.0401 1.0000
15.000 1.0966 0.06925 0.06243 -0.0037 0.0389 1.0000
15.250 1.1023 0.07180 0.06505 -0.0043 0.0378 1.0000
15.500 1.1075 0.07447 0.06778 -0.0050 0.0368 1.0000
15.750 1.1123 0.07722 0.07057 -0.0058 0.0358 1.0000
16.000 1.1158 0.08013 0.07348 -0.0067 0.0349 1.0000
16.250 1.1219 0.08275 0.07618 -0.0074 0.0341 1.0000
16.500 1.1276 0.08546 0.07900 -0.0083 0.0331 1.0000
16.750 1.1328 0.08829 0.08191 -0.0092 0.0322 1.0000
17.000 1.1378 0.09115 0.08484 -0.0102 0.0314 1.0000
17.250 1.1421 0.09413 0.08788 -0.0114 0.0307 1.0000
17.500 1.1463 0.09712 0.09090 -0.0125 0.0301 1.0000
17.750 1.1508 0.10004 0.09385 -0.0136 0.0295 1.0000
18.000 1.1548 0.10318 0.09714 -0.0148 0.0289 1.0000
18.250 1.1581 0.10648 0.10056 -0.0162 0.0282 1.0000
18.500 1.1606 0.10988 0.10407 -0.0178 0.0276 1.0000
18.750 1.1632 0.11330 0.10759 -0.0194 0.0270 1.0000
19.000 1.1650 0.11688 0.11125 -0.0211 0.0265 1.0000
19.250 1.1671 0.12041 0.11485 -0.0229 0.0260 1.0000
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