NASA SC(2)-0414 AIRFOIL (sc20414-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: NASA SC(2)-0414 AIRFOIL (sc20414-il) Reynolds number: 500,000 Max Cl/Cd: 57.95 at α=7.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-sc20414-il-500000.txt Download as CSV file: xf-sc20414-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: NASA SC(2)-0414 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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.750 -1.0665 0.11354 0.10996 -0.0269 1.0000 0.0305
-18.500 -1.1084 0.10133 0.09749 -0.0345 1.0000 0.0305
-18.250 -1.1367 0.09224 0.08818 -0.0401 1.0000 0.0305
-18.000 -1.1580 0.08479 0.08052 -0.0444 1.0000 0.0306
-17.750 -1.1747 0.07849 0.07403 -0.0479 1.0000 0.0307
-17.500 -1.1905 0.07279 0.06816 -0.0503 1.0000 0.0309
-17.250 -1.1976 0.06857 0.06383 -0.0518 1.0000 0.0311
-17.000 -1.1997 0.06511 0.06030 -0.0529 1.0000 0.0314
-16.750 -1.2000 0.06195 0.05706 -0.0539 1.0000 0.0316
-16.500 -1.1995 0.05898 0.05402 -0.0549 1.0000 0.0319
-16.250 -1.1983 0.05619 0.05115 -0.0556 1.0000 0.0321
-16.000 -1.1964 0.05353 0.04841 -0.0562 1.0000 0.0324
-15.750 -1.1941 0.05101 0.04579 -0.0567 1.0000 0.0328
-15.500 -1.1916 0.04862 0.04330 -0.0570 1.0000 0.0331
-15.250 -1.1883 0.04638 0.04095 -0.0571 1.0000 0.0335
-15.000 -1.1839 0.04428 0.03874 -0.0571 1.0000 0.0339
-14.750 -1.1785 0.04232 0.03667 -0.0570 1.0000 0.0343
-14.500 -1.1720 0.04050 0.03473 -0.0568 1.0000 0.0347
-14.250 -1.1647 0.03882 0.03292 -0.0566 1.0000 0.0350
-14.000 -1.1564 0.03708 0.03110 -0.0559 1.0000 0.0356
-13.750 -1.1459 0.03565 0.02966 -0.0553 1.0000 0.0362
-13.500 -1.1342 0.03441 0.02841 -0.0549 1.0000 0.0367
-13.250 -1.1223 0.03321 0.02717 -0.0545 1.0000 0.0373
-13.000 -1.1099 0.03205 0.02597 -0.0539 1.0000 0.0379
-12.750 -1.0973 0.03093 0.02478 -0.0533 1.0000 0.0385
-12.500 -1.0844 0.02985 0.02362 -0.0526 1.0000 0.0392
-12.250 -1.0710 0.02886 0.02255 -0.0518 1.0000 0.0398
-12.000 -1.0579 0.02788 0.02149 -0.0508 1.0000 0.0403
-11.750 -1.0464 0.02673 0.02036 -0.0495 1.0000 0.0412
-11.500 -1.0346 0.02587 0.01950 -0.0481 1.0000 0.0419
-11.250 -1.0247 0.02511 0.01874 -0.0463 1.0000 0.0427
-11.000 -1.0183 0.02444 0.01805 -0.0438 1.0000 0.0434
-10.750 -1.0118 0.02379 0.01736 -0.0412 1.0000 0.0443
-10.250 -0.9900 0.02245 0.01591 -0.0375 1.0000 0.0460
-10.000 -0.9803 0.02156 0.01506 -0.0356 1.0000 0.0471
-9.750 -0.9665 0.02092 0.01444 -0.0343 1.0000 0.0481
-9.500 -0.9507 0.02035 0.01385 -0.0332 1.0000 0.0493
-9.250 -0.9333 0.01982 0.01328 -0.0324 1.0000 0.0506
-9.000 -0.9143 0.01939 0.01279 -0.0317 1.0000 0.0518
-8.750 -0.8968 0.01855 0.01200 -0.0311 1.0000 0.0536
-8.500 -0.8651 0.01804 0.01150 -0.0328 0.9988 0.0556
-8.250 -0.8299 0.01760 0.01102 -0.0350 0.9970 0.0579
-8.000 -0.7951 0.01688 0.01031 -0.0374 0.9953 0.0604
-7.750 -0.7590 0.01637 0.00982 -0.0399 0.9938 0.0631
-7.500 -0.7227 0.01600 0.00943 -0.0421 0.9922 0.0659
-7.250 -0.6882 0.01534 0.00881 -0.0444 0.9896 0.0695
-7.000 -0.6523 0.01493 0.00842 -0.0466 0.9872 0.0731
-6.750 -0.6155 0.01443 0.00792 -0.0491 0.9852 0.0771
-6.500 -0.5781 0.01400 0.00754 -0.0516 0.9835 0.0821
-6.250 -0.5401 0.01355 0.00712 -0.0543 0.9822 0.0880
-6.000 -0.5018 0.01318 0.00678 -0.0569 0.9812 0.0948
-5.750 -0.4674 0.01270 0.00637 -0.0588 0.9778 0.1038
-5.500 -0.4310 0.01225 0.00601 -0.0611 0.9751 0.1158
-5.250 -0.3928 0.01181 0.00566 -0.0638 0.9731 0.1337
-5.000 -0.3531 0.01125 0.00528 -0.0669 0.9717 0.1611
-4.750 -0.3124 0.01059 0.00487 -0.0705 0.9706 0.2111
-4.500 -0.2700 0.00969 0.00438 -0.0747 0.9696 0.2970
-4.250 -0.2239 0.00849 0.00379 -0.0802 0.9690 0.4339
-4.000 -0.1815 0.00791 0.00368 -0.0838 0.9679 0.5466
-3.750 -0.1493 0.00786 0.00369 -0.0846 0.9623 0.5778
-3.500 -0.1149 0.00785 0.00371 -0.0858 0.9583 0.5964
-3.250 -0.0799 0.00786 0.00369 -0.0871 0.9550 0.6113
-3.000 -0.0494 0.00793 0.00378 -0.0873 0.9492 0.6212
-2.750 -0.0180 0.00795 0.00378 -0.0877 0.9431 0.6296
-2.500 0.0127 0.00802 0.00386 -0.0879 0.9381 0.6361
-2.250 0.0420 0.00810 0.00390 -0.0879 0.9299 0.6437
-2.000 0.0706 0.00816 0.00396 -0.0875 0.9227 0.6494
-1.750 0.0971 0.00827 0.00409 -0.0867 0.9113 0.6553
-1.500 0.1259 0.00836 0.00411 -0.0864 0.9002 0.6617
-1.250 0.1525 0.00844 0.00418 -0.0855 0.8879 0.6667
-1.000 0.1780 0.00862 0.00438 -0.0842 0.8733 0.6720
-0.750 0.2059 0.00875 0.00448 -0.0838 0.8591 0.6776
-0.500 0.2361 0.00882 0.00447 -0.0840 0.8467 0.6816
-0.250 0.2632 0.00885 0.00450 -0.0833 0.8339 0.6845
0.000 0.2906 0.00895 0.00462 -0.0828 0.8207 0.6873
0.250 0.3190 0.00904 0.00469 -0.0825 0.8080 0.6901
0.500 0.3482 0.00908 0.00468 -0.0825 0.7934 0.6924
0.750 0.3778 0.00911 0.00465 -0.0826 0.7755 0.6948
1.000 0.4074 0.00914 0.00462 -0.0828 0.7535 0.6972
1.250 0.4370 0.00921 0.00457 -0.0830 0.7253 0.6991
1.500 0.4657 0.00931 0.00451 -0.0830 0.6857 0.7008
1.750 0.4918 0.00953 0.00450 -0.0824 0.6208 0.7024
2.000 0.5134 0.01030 0.00468 -0.0812 0.4863 0.7040
2.250 0.5360 0.01116 0.00498 -0.0803 0.3668 0.7056
2.500 0.5610 0.01178 0.00523 -0.0800 0.2853 0.7072
2.750 0.5867 0.01233 0.00547 -0.0797 0.2206 0.7088
3.000 0.6135 0.01277 0.00569 -0.0796 0.1777 0.7106
3.250 0.6409 0.01313 0.00590 -0.0796 0.1502 0.7125
3.500 0.6687 0.01346 0.00611 -0.0797 0.1314 0.7145
3.750 0.6969 0.01375 0.00632 -0.0798 0.1187 0.7164
4.000 0.7251 0.01405 0.00655 -0.0799 0.1090 0.7182
4.250 0.7529 0.01435 0.00677 -0.0799 0.1007 0.7198
4.500 0.7802 0.01456 0.00699 -0.0798 0.0945 0.7215
4.750 0.8059 0.01496 0.00734 -0.0793 0.0881 0.7232
5.000 0.8329 0.01520 0.00762 -0.0791 0.0839 0.7250
5.250 0.8587 0.01560 0.00798 -0.0786 0.0795 0.7271
5.500 0.8852 0.01594 0.00835 -0.0783 0.0758 0.7291
5.750 0.9124 0.01622 0.00862 -0.0782 0.0723 0.7311
6.000 0.9377 0.01672 0.00908 -0.0778 0.0689 0.7331
6.250 0.9653 0.01697 0.00936 -0.0777 0.0664 0.7351
6.500 0.9922 0.01729 0.00967 -0.0776 0.0638 0.7370
6.750 1.0166 0.01787 0.01019 -0.0771 0.0611 0.7387
7.000 1.0427 0.01811 0.01050 -0.0767 0.0591 0.7404
7.250 1.0680 0.01843 0.01086 -0.0762 0.0569 0.7421
7.500 1.0917 0.01894 0.01135 -0.0755 0.0549 0.7440
7.750 1.1151 0.01950 0.01196 -0.0747 0.0532 0.7461
8.000 1.1399 0.01992 0.01242 -0.0741 0.0516 0.7482
8.250 1.1643 0.02036 0.01288 -0.0735 0.0500 0.7504
8.500 1.1872 0.02096 0.01346 -0.0728 0.0485 0.7526
8.750 1.2097 0.02167 0.01419 -0.0720 0.0471 0.7547
9.000 1.2336 0.02211 0.01470 -0.0714 0.0458 0.7566
9.250 1.2560 0.02260 0.01525 -0.0704 0.0446 0.7584
9.500 1.2775 0.02315 0.01582 -0.0694 0.0436 0.7602
9.750 1.2969 0.02396 0.01664 -0.0682 0.0426 0.7622
10.000 1.3160 0.02487 0.01761 -0.0668 0.0417 0.7643
10.250 1.3366 0.02548 0.01832 -0.0657 0.0409 0.7666
10.500 1.3565 0.02615 0.01908 -0.0645 0.0400 0.7691
10.750 1.3758 0.02681 0.01979 -0.0633 0.0392 0.7717
11.000 1.3940 0.02747 0.02048 -0.0619 0.0384 0.7739
11.250 1.4098 0.02822 0.02125 -0.0602 0.0377 0.7759
11.500 1.4219 0.02956 0.02263 -0.0580 0.0370 0.7779
11.750 1.4322 0.03038 0.02358 -0.0553 0.0366 0.7801
12.000 1.4445 0.03126 0.02458 -0.0531 0.0361 0.7825
12.250 1.4568 0.03225 0.02570 -0.0511 0.0356 0.7851
12.500 1.4684 0.03332 0.02687 -0.0492 0.0350 0.7876
12.750 1.4794 0.03447 0.02810 -0.0473 0.0345 0.7899
13.000 1.4893 0.03561 0.02934 -0.0454 0.0341 0.7922
13.250 1.4983 0.03684 0.03066 -0.0434 0.0337 0.7944
13.500 1.5066 0.03816 0.03205 -0.0416 0.0333 0.7967
13.750 1.5140 0.03966 0.03362 -0.0399 0.0330 0.7992
14.000 1.5195 0.04152 0.03554 -0.0382 0.0326 0.8019
14.250 1.5205 0.04404 0.03818 -0.0363 0.0322 0.8045
14.500 1.5225 0.04603 0.04034 -0.0348 0.0319 0.8072
14.750 1.5228 0.04819 0.04269 -0.0335 0.0317 0.8099
15.000 1.5213 0.05071 0.04539 -0.0323 0.0314 0.8125
15.250 1.5187 0.05346 0.04832 -0.0314 0.0311 0.8151
15.500 1.5150 0.05647 0.05149 -0.0309 0.0308 0.8177
15.750 1.5095 0.05988 0.05505 -0.0307 0.0305 0.8202
16.000 1.5018 0.06373 0.05906 -0.0310 0.0303 0.8226
16.250 1.4920 0.06799 0.06349 -0.0318 0.0301 0.8247
16.500 1.4803 0.07275 0.06843 -0.0331 0.0299 0.8267
16.750 1.4665 0.07817 0.07403 -0.0351 0.0298 0.8287
17.000 1.4498 0.08441 0.08046 -0.0379 0.0297 0.8306
17.250 1.4301 0.09163 0.08787 -0.0418 0.0296 0.8325
17.500 1.4039 0.10057 0.09703 -0.0471 0.0295 0.8341
17.750 1.3658 0.11250 0.10924 -0.0549 0.0295 0.8350
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