NASA SC(2)-0614 AIRFOIL (sc20614-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: NASA SC(2)-0614 AIRFOIL (sc20614-il) Reynolds number: 500,000 Max Cl/Cd: 64.29 at α=6.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-sc20614-il-500000-n5.txt Download as CSV file: xf-sc20614-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NASA SC(2)-0614 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.0726 0.11154 0.10754 -0.0362 1.0000 0.0236
-19.500 -1.0931 0.10386 0.09971 -0.0405 1.0000 0.0237
-19.250 -1.1110 0.09680 0.09250 -0.0443 1.0000 0.0238
-19.000 -1.1263 0.09033 0.08590 -0.0478 1.0000 0.0238
-18.750 -1.1388 0.08444 0.07986 -0.0509 1.0000 0.0240
-18.500 -1.1491 0.07904 0.07433 -0.0538 1.0000 0.0241
-18.250 -1.1570 0.07414 0.06930 -0.0563 1.0000 0.0242
-18.000 -1.1630 0.06963 0.06467 -0.0585 1.0000 0.0243
-17.750 -1.1693 0.06529 0.06024 -0.0605 1.0000 0.0244
-17.500 -1.1740 0.06131 0.05617 -0.0622 1.0000 0.0246
-17.250 -1.1765 0.05772 0.05249 -0.0637 1.0000 0.0248
-17.000 -1.1772 0.05450 0.04919 -0.0649 1.0000 0.0250
-16.750 -1.1763 0.05157 0.04619 -0.0658 1.0000 0.0252
-16.500 -1.1738 0.04893 0.04347 -0.0666 1.0000 0.0255
-16.250 -1.1701 0.04652 0.04098 -0.0672 1.0000 0.0257
-16.000 -1.1655 0.04428 0.03867 -0.0676 1.0000 0.0260
-15.750 -1.1596 0.04226 0.03658 -0.0678 1.0000 0.0262
-15.500 -1.1531 0.04039 0.03464 -0.0679 1.0000 0.0266
-15.250 -1.1462 0.03865 0.03282 -0.0679 1.0000 0.0269
-15.000 -1.1383 0.03704 0.03114 -0.0677 1.0000 0.0273
-14.750 -1.1298 0.03554 0.02957 -0.0674 1.0000 0.0276
-14.500 -1.1208 0.03415 0.02810 -0.0669 1.0000 0.0280
-14.250 -1.1121 0.03281 0.02669 -0.0663 1.0000 0.0283
-14.000 -1.1059 0.03137 0.02522 -0.0655 1.0000 0.0287
-13.750 -1.0988 0.03014 0.02396 -0.0644 1.0000 0.0290
-13.500 -1.0922 0.02904 0.02284 -0.0629 1.0000 0.0294
-13.250 -1.0865 0.02805 0.02182 -0.0611 1.0000 0.0298
-13.000 -1.0828 0.02715 0.02089 -0.0588 1.0000 0.0302
-12.750 -1.0831 0.02634 0.02005 -0.0556 1.0000 0.0306
-12.500 -1.0907 0.02564 0.01931 -0.0510 1.0000 0.0309
-12.250 -1.0692 0.02469 0.01832 -0.0518 0.9979 0.0315
-12.000 -1.0425 0.02378 0.01735 -0.0535 0.9956 0.0322
-11.750 -1.0152 0.02285 0.01638 -0.0553 0.9936 0.0330
-11.500 -0.9883 0.02201 0.01554 -0.0569 0.9916 0.0340
-11.250 -0.9614 0.02128 0.01479 -0.0583 0.9889 0.0351
-11.000 -0.9326 0.02059 0.01406 -0.0599 0.9865 0.0363
-10.750 -0.9022 0.01990 0.01333 -0.0618 0.9845 0.0375
-10.500 -0.8709 0.01920 0.01265 -0.0639 0.9829 0.0389
-10.250 -0.8385 0.01860 0.01203 -0.0660 0.9817 0.0404
-10.000 -0.8053 0.01804 0.01144 -0.0682 0.9807 0.0420
-9.750 -0.7777 0.01747 0.01086 -0.0692 0.9769 0.0435
-9.500 -0.7464 0.01694 0.01033 -0.0709 0.9744 0.0454
-9.250 -0.7138 0.01647 0.00984 -0.0727 0.9724 0.0475
-9.000 -0.6808 0.01597 0.00933 -0.0747 0.9707 0.0495
-8.750 -0.6472 0.01548 0.00885 -0.0767 0.9691 0.0518
-8.500 -0.6132 0.01506 0.00841 -0.0787 0.9677 0.0540
-8.250 -0.5833 0.01465 0.00800 -0.0798 0.9641 0.0560
-8.000 -0.5522 0.01424 0.00761 -0.0811 0.9610 0.0584
-7.750 -0.5198 0.01390 0.00726 -0.0826 0.9585 0.0611
-7.500 -0.4868 0.01352 0.00690 -0.0842 0.9562 0.0639
-7.250 -0.4532 0.01316 0.00655 -0.0859 0.9542 0.0672
-7.000 -0.4210 0.01288 0.00625 -0.0872 0.9515 0.0702
-6.750 -0.3904 0.01254 0.00595 -0.0882 0.9474 0.0742
-6.500 -0.3586 0.01224 0.00567 -0.0895 0.9440 0.0788
-6.250 -0.3258 0.01191 0.00539 -0.0909 0.9412 0.0847
-6.000 -0.2925 0.01162 0.00512 -0.0924 0.9386 0.0914
-5.750 -0.2608 0.01133 0.00488 -0.0935 0.9348 0.1002
-5.500 -0.2290 0.01104 0.00464 -0.0947 0.9305 0.1108
-5.250 -0.1962 0.01073 0.00441 -0.0961 0.9270 0.1257
-5.000 -0.1629 0.01043 0.00419 -0.0976 0.9241 0.1451
-4.750 -0.1289 0.01006 0.00395 -0.0993 0.9211 0.1722
-4.500 -0.0954 0.00970 0.00375 -0.1010 0.9170 0.2069
-4.250 -0.0608 0.00930 0.00352 -0.1029 0.9130 0.2493
-4.000 -0.0240 0.00880 0.00326 -0.1055 0.9097 0.3132
-3.750 0.0153 0.00816 0.00295 -0.1087 0.9070 0.3978
-3.500 0.0538 0.00765 0.00280 -0.1117 0.9039 0.4898
-3.250 0.0863 0.00753 0.00283 -0.1127 0.8992 0.5325
-3.000 0.1177 0.00750 0.00287 -0.1133 0.8944 0.5598
-2.750 0.1488 0.00751 0.00287 -0.1138 0.8900 0.5770
-2.500 0.1789 0.00753 0.00291 -0.1141 0.8828 0.5887
-2.250 0.2092 0.00754 0.00287 -0.1143 0.8742 0.5973
-2.000 0.2385 0.00757 0.00292 -0.1143 0.8629 0.6056
-1.750 0.2681 0.00761 0.00290 -0.1144 0.8492 0.6147
-1.500 0.2969 0.00768 0.00295 -0.1142 0.8345 0.6218
-1.250 0.3265 0.00776 0.00294 -0.1142 0.8169 0.6288
-1.000 0.3545 0.00784 0.00298 -0.1139 0.7911 0.6335
-0.750 0.3826 0.00797 0.00299 -0.1136 0.7616 0.6370
-0.500 0.4108 0.00812 0.00301 -0.1134 0.7285 0.6403
-0.250 0.4377 0.00839 0.00302 -0.1129 0.6698 0.6434
0.000 0.4603 0.00911 0.00315 -0.1118 0.5464 0.6456
0.250 0.4836 0.00981 0.00340 -0.1110 0.4466 0.6471
0.500 0.5087 0.01036 0.00362 -0.1106 0.3672 0.6484
0.750 0.5343 0.01089 0.00383 -0.1102 0.2961 0.6499
1.000 0.5604 0.01134 0.00404 -0.1099 0.2405 0.6514
1.250 0.5875 0.01170 0.00422 -0.1098 0.2034 0.6531
1.500 0.6148 0.01202 0.00440 -0.1097 0.1724 0.6551
1.750 0.6423 0.01233 0.00458 -0.1096 0.1493 0.6571
2.000 0.6700 0.01260 0.00475 -0.1095 0.1314 0.6589
2.250 0.6977 0.01288 0.00493 -0.1095 0.1146 0.6607
2.500 0.7252 0.01315 0.00512 -0.1094 0.1019 0.6622
2.750 0.7525 0.01340 0.00534 -0.1092 0.0925 0.6636
3.000 0.7799 0.01364 0.00556 -0.1090 0.0855 0.6651
3.250 0.8069 0.01392 0.00580 -0.1088 0.0792 0.6666
3.500 0.8341 0.01418 0.00604 -0.1086 0.0739 0.6683
3.750 0.8611 0.01446 0.00629 -0.1083 0.0696 0.6701
4.000 0.8883 0.01471 0.00653 -0.1081 0.0660 0.6719
4.250 0.9150 0.01502 0.00681 -0.1078 0.0627 0.6738
4.500 0.9420 0.01528 0.00707 -0.1076 0.0603 0.6757
4.750 0.9688 0.01556 0.00733 -0.1073 0.0578 0.6776
5.000 0.9947 0.01588 0.00765 -0.1069 0.0557 0.6791
5.250 1.0207 0.01617 0.00797 -0.1064 0.0540 0.6806
5.500 1.0466 0.01647 0.00830 -0.1060 0.0522 0.6824
5.750 1.0721 0.01681 0.00865 -0.1055 0.0504 0.6846
6.000 1.0970 0.01721 0.00904 -0.1049 0.0486 0.6870
6.250 1.1226 0.01752 0.00938 -0.1044 0.0471 0.6894
6.500 1.1479 0.01786 0.00975 -0.1038 0.0456 0.6916
6.750 1.1727 0.01824 0.01012 -0.1033 0.0441 0.6935
7.000 1.1964 0.01867 0.01056 -0.1025 0.0427 0.6952
7.250 1.2206 0.01904 0.01098 -0.1017 0.0416 0.6969
7.500 1.2445 0.01942 0.01142 -0.1009 0.0403 0.6988
7.750 1.2680 0.01983 0.01185 -0.1001 0.0390 0.7009
8.000 1.2909 0.02028 0.01231 -0.0992 0.0378 0.7032
8.250 1.3134 0.02075 0.01281 -0.0982 0.0367 0.7057
8.500 1.3361 0.02118 0.01329 -0.0973 0.0355 0.7082
8.750 1.3580 0.02164 0.01379 -0.0962 0.0345 0.7102
9.000 1.3791 0.02213 0.01432 -0.0950 0.0335 0.7120
9.250 1.3990 0.02267 0.01489 -0.0937 0.0327 0.7139
9.500 1.4183 0.02323 0.01551 -0.0922 0.0320 0.7160
9.750 1.4371 0.02379 0.01613 -0.0906 0.0314 0.7182
10.000 1.4549 0.02437 0.01678 -0.0889 0.0307 0.7205
10.250 1.4702 0.02496 0.01742 -0.0868 0.0301 0.7228
10.500 1.4847 0.02559 0.01810 -0.0845 0.0295 0.7250
10.750 1.4998 0.02628 0.01885 -0.0825 0.0290 0.7270
11.000 1.5142 0.02705 0.01967 -0.0804 0.0285 0.7291
11.250 1.5275 0.02792 0.02060 -0.0783 0.0280 0.7315
11.500 1.5417 0.02874 0.02151 -0.0763 0.0276 0.7341
11.750 1.5553 0.02960 0.02246 -0.0744 0.0272 0.7366
12.000 1.5683 0.03052 0.02346 -0.0724 0.0267 0.7390
12.250 1.5804 0.03151 0.02453 -0.0705 0.0264 0.7413
12.500 1.5918 0.03257 0.02568 -0.0685 0.0260 0.7434
12.750 1.6023 0.03369 0.02689 -0.0665 0.0257 0.7454
13.000 1.6119 0.03490 0.02819 -0.0646 0.0254 0.7476
13.250 1.6204 0.03624 0.02961 -0.0626 0.0251 0.7500
13.500 1.6275 0.03771 0.03117 -0.0607 0.0248 0.7524
13.750 1.6331 0.03936 0.03289 -0.0588 0.0245 0.7549
14.000 1.6366 0.04125 0.03487 -0.0569 0.0243 0.7572
14.250 1.6402 0.04319 0.03691 -0.0552 0.0241 0.7593
14.500 1.6440 0.04515 0.03900 -0.0537 0.0239 0.7613
14.750 1.6467 0.04729 0.04129 -0.0523 0.0238 0.7634
15.000 1.6481 0.04965 0.04378 -0.0511 0.0236 0.7656
15.250 1.6480 0.05223 0.04650 -0.0501 0.0234 0.7679
15.500 1.6463 0.05510 0.04949 -0.0493 0.0232 0.7701
15.750 1.6433 0.05824 0.05277 -0.0488 0.0231 0.7724
16.000 1.6393 0.06170 0.05636 -0.0487 0.0229 0.7745
16.250 1.6336 0.06553 0.06034 -0.0489 0.0227 0.7764
16.500 1.6261 0.06983 0.06479 -0.0497 0.0226 0.7782
16.750 1.6168 0.07466 0.06978 -0.0510 0.0224 0.7802
17.000 1.6057 0.08006 0.07535 -0.0529 0.0223 0.7822
17.250 1.5914 0.08625 0.08170 -0.0555 0.0222 0.7841
17.500 1.5743 0.09323 0.08885 -0.0589 0.0221 0.7859
17.750 1.5542 0.10103 0.09683 -0.0630 0.0220 0.7875
18.000 1.5304 0.10971 0.10569 -0.0678 0.0219 0.7889
18.250 1.5035 0.11919 0.11535 -0.0733 0.0219 0.7900
18.500 1.4742 0.12940 0.12575 -0.0796 0.0218 0.7909
18.750 1.4432 0.14024 0.13677 -0.0866 0.0218 0.7917
19.000 1.4105 0.15177 0.14848 -0.0944 0.0217 0.7923
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