NASA/LANGLEY MS(1)-0317 AIRFOIL (ms317-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: NASA/LANGLEY MS(1)-0317 AIRFOIL (ms317-il) Reynolds number: 500,000 Max Cl/Cd: 69.9 at α=2.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-ms317-il-500000.txt Download as CSV file: xf-ms317-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: NASA/LANGLEY MS(1)-0317 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 -1.0041 0.09878 0.09489 -0.0460 1.0000 0.0248
-18.500 -1.0236 0.09139 0.08732 -0.0504 1.0000 0.0249
-18.250 -1.0387 0.08501 0.08079 -0.0540 1.0000 0.0250
-18.000 -1.0509 0.07935 0.07498 -0.0571 1.0000 0.0252
-17.750 -1.0601 0.07434 0.06983 -0.0597 1.0000 0.0253
-17.500 -1.0672 0.06981 0.06517 -0.0618 1.0000 0.0255
-17.250 -1.0728 0.06569 0.06091 -0.0636 1.0000 0.0257
-17.000 -1.0769 0.06190 0.05699 -0.0651 1.0000 0.0259
-16.750 -1.0797 0.05841 0.05336 -0.0664 1.0000 0.0262
-16.500 -1.0813 0.05521 0.05003 -0.0673 1.0000 0.0264
-16.250 -1.0817 0.05227 0.04695 -0.0681 1.0000 0.0267
-16.000 -1.0810 0.04959 0.04413 -0.0686 1.0000 0.0269
-15.750 -1.0796 0.04715 0.04154 -0.0689 1.0000 0.0271
-15.500 -1.0742 0.04499 0.03936 -0.0684 1.0000 0.0275
-15.250 -1.0668 0.04318 0.03752 -0.0682 1.0000 0.0279
-15.000 -1.0586 0.04149 0.03581 -0.0681 1.0000 0.0283
-14.750 -1.0502 0.03984 0.03412 -0.0680 1.0000 0.0287
-14.500 -1.0412 0.03826 0.03248 -0.0678 1.0000 0.0291
-14.250 -1.0320 0.03672 0.03087 -0.0675 1.0000 0.0296
-14.000 -1.0219 0.03527 0.02933 -0.0671 1.0000 0.0301
-13.750 -1.0111 0.03390 0.02786 -0.0666 1.0000 0.0305
-13.500 -0.9996 0.03263 0.02650 -0.0662 1.0000 0.0309
-13.250 -0.9889 0.03120 0.02505 -0.0653 1.0000 0.0315
-13.000 -0.9771 0.02999 0.02385 -0.0645 1.0000 0.0320
-12.750 -0.9646 0.02891 0.02276 -0.0638 1.0000 0.0326
-12.500 -0.9519 0.02790 0.02173 -0.0630 1.0000 0.0332
-12.250 -0.9398 0.02696 0.02076 -0.0620 1.0000 0.0338
-12.000 -0.9298 0.02613 0.01988 -0.0605 1.0000 0.0345
-11.750 -0.9297 0.02554 0.01925 -0.0571 1.0000 0.0350
-11.500 -0.9116 0.02441 0.01811 -0.0574 0.9963 0.0359
-11.250 -0.8820 0.02332 0.01704 -0.0597 0.9922 0.0370
-11.000 -0.8529 0.02240 0.01610 -0.0616 0.9856 0.0381
-10.750 -0.8216 0.02154 0.01517 -0.0637 0.9802 0.0393
-10.500 -0.7974 0.02053 0.01413 -0.0646 0.9695 0.0405
-10.250 -0.7749 0.01968 0.01329 -0.0650 0.9582 0.0418
-10.000 -0.7516 0.01903 0.01259 -0.0652 0.9478 0.0434
-9.750 -0.7295 0.01850 0.01198 -0.0649 0.9368 0.0449
-9.500 -0.7105 0.01769 0.01118 -0.0646 0.9258 0.0467
-9.250 -0.6880 0.01719 0.01062 -0.0643 0.9170 0.0487
-9.000 -0.6646 0.01671 0.01009 -0.0641 0.9080 0.0509
-8.750 -0.6421 0.01613 0.00950 -0.0639 0.9001 0.0536
-8.500 -0.6165 0.01577 0.00909 -0.0639 0.8932 0.0568
-8.250 -0.5921 0.01522 0.00858 -0.0640 0.8860 0.0610
-8.000 -0.5666 0.01480 0.00813 -0.0640 0.8799 0.0659
-7.750 -0.5397 0.01446 0.00777 -0.0643 0.8740 0.0715
-7.500 -0.5130 0.01403 0.00738 -0.0646 0.8679 0.0783
-7.250 -0.4860 0.01364 0.00701 -0.0649 0.8624 0.0858
-7.000 -0.4583 0.01330 0.00667 -0.0653 0.8571 0.0939
-6.750 -0.4300 0.01295 0.00636 -0.0658 0.8515 0.1028
-6.500 -0.4015 0.01262 0.00605 -0.0662 0.8463 0.1132
-6.250 -0.3729 0.01228 0.00575 -0.0668 0.8417 0.1266
-6.000 -0.3437 0.01192 0.00548 -0.0675 0.8369 0.1445
-5.500 -0.2843 0.01113 0.00493 -0.0692 0.8272 0.2013
-5.250 -0.2539 0.01066 0.00463 -0.0703 0.8230 0.2432
-5.000 -0.2226 0.01014 0.00434 -0.0717 0.8187 0.3009
-4.750 -0.1894 0.00934 0.00396 -0.0739 0.8143 0.3957
-4.500 -0.1552 0.00862 0.00374 -0.0760 0.8099 0.5133
-4.250 -0.1234 0.00848 0.00376 -0.0769 0.8059 0.5650
-4.000 -0.0924 0.00852 0.00380 -0.0774 0.8021 0.5915
-3.750 -0.0613 0.00859 0.00386 -0.0780 0.7983 0.6094
-3.500 -0.0302 0.00865 0.00391 -0.0786 0.7942 0.6233
-3.250 0.0002 0.00872 0.00399 -0.0789 0.7900 0.6331
-3.000 0.0314 0.00881 0.00400 -0.0795 0.7860 0.6428
-2.750 0.0614 0.00892 0.00409 -0.0797 0.7820 0.6495
-2.500 0.0918 0.00902 0.00419 -0.0800 0.7780 0.6566
-2.250 0.1229 0.00911 0.00424 -0.0806 0.7737 0.6642
-2.000 0.1520 0.00925 0.00443 -0.0805 0.7695 0.6710
-1.750 0.1822 0.00937 0.00451 -0.0808 0.7656 0.6772
-1.500 0.2134 0.00952 0.00457 -0.0814 0.7613 0.6826
-1.250 0.2420 0.00954 0.00467 -0.0813 0.7555 0.6874
-1.000 0.2702 0.00961 0.00470 -0.0808 0.7450 0.6933
-0.750 0.2998 0.00970 0.00474 -0.0809 0.7327 0.7004
-0.500 0.3288 0.00969 0.00469 -0.0808 0.7241 0.7045
-0.250 0.3582 0.00969 0.00471 -0.0810 0.7168 0.7070
0.000 0.3878 0.00968 0.00469 -0.0812 0.7085 0.7094
0.250 0.4176 0.00970 0.00467 -0.0815 0.7004 0.7121
0.500 0.4479 0.00969 0.00465 -0.0819 0.6913 0.7149
0.750 0.4783 0.00972 0.00461 -0.0823 0.6832 0.7176
1.000 0.5092 0.00971 0.00461 -0.0830 0.6740 0.7201
1.250 0.5392 0.00971 0.00455 -0.0834 0.6644 0.7225
1.500 0.5685 0.00968 0.00454 -0.0835 0.6523 0.7245
1.750 0.5976 0.00970 0.00455 -0.0837 0.6392 0.7264
2.000 0.6264 0.00976 0.00457 -0.0838 0.6240 0.7285
2.250 0.6551 0.00984 0.00461 -0.0839 0.6051 0.7308
2.500 0.6834 0.00996 0.00465 -0.0840 0.5802 0.7332
2.750 0.7109 0.01017 0.00471 -0.0839 0.5440 0.7355
3.000 0.7354 0.01063 0.00485 -0.0835 0.4814 0.7378
3.250 0.7570 0.01139 0.00519 -0.0826 0.4004 0.7400
3.500 0.7788 0.01209 0.00553 -0.0819 0.3351 0.7422
3.750 0.8012 0.01265 0.00586 -0.0812 0.2860 0.7442
4.000 0.8242 0.01317 0.00619 -0.0805 0.2484 0.7463
4.250 0.8478 0.01364 0.00651 -0.0799 0.2197 0.7484
4.500 0.8719 0.01406 0.00681 -0.0794 0.1980 0.7506
4.750 0.8964 0.01446 0.00712 -0.0790 0.1816 0.7527
5.000 0.9210 0.01484 0.00742 -0.0786 0.1689 0.7549
5.250 0.9448 0.01527 0.00776 -0.0782 0.1582 0.7570
5.500 0.9702 0.01558 0.00804 -0.0779 0.1508 0.7593
5.750 0.9929 0.01603 0.00842 -0.0772 0.1435 0.7614
6.000 1.0173 0.01627 0.00870 -0.0767 0.1391 0.7635
6.250 1.0400 0.01664 0.00906 -0.0760 0.1346 0.7654
6.500 1.0597 0.01718 0.00956 -0.0747 0.1300 0.7675
6.750 1.0832 0.01746 0.00989 -0.0741 0.1276 0.7696
7.000 1.1056 0.01781 0.01027 -0.0733 0.1249 0.7719
7.250 1.1265 0.01822 0.01068 -0.0723 0.1223 0.7743
7.500 1.1449 0.01873 0.01117 -0.0709 0.1197 0.7769
7.750 1.1567 0.01939 0.01182 -0.0684 0.1172 0.7793
8.000 1.1759 0.01973 0.01223 -0.0671 0.1159 0.7818
8.250 1.1950 0.02019 0.01274 -0.0659 0.1144 0.7841
8.500 1.2138 0.02070 0.01330 -0.0647 0.1128 0.7865
8.750 1.2321 0.02125 0.01390 -0.0635 0.1113 0.7891
9.000 1.2500 0.02187 0.01453 -0.0623 0.1098 0.7920
9.250 1.2667 0.02259 0.01526 -0.0611 0.1082 0.7950
9.500 1.2811 0.02354 0.01620 -0.0596 0.1064 0.7976
9.750 1.2977 0.02431 0.01702 -0.0584 0.1053 0.8002
10.000 1.3160 0.02491 0.01770 -0.0574 0.1044 0.8028
10.250 1.3338 0.02556 0.01842 -0.0565 0.1033 0.8056
10.500 1.3512 0.02627 0.01919 -0.0555 0.1021 0.8086
10.750 1.3683 0.02701 0.01998 -0.0545 0.1008 0.8118
11.000 1.3852 0.02780 0.02080 -0.0537 0.0995 0.8153
11.250 1.4012 0.02861 0.02164 -0.0527 0.0982 0.8185
11.500 1.4152 0.02958 0.02263 -0.0515 0.0967 0.8216
11.750 1.4283 0.03077 0.02383 -0.0501 0.0950 0.8248
12.000 1.4444 0.03158 0.02473 -0.0493 0.0943 0.8285
12.250 1.4600 0.03247 0.02571 -0.0485 0.0934 0.8323
12.500 1.4751 0.03340 0.02673 -0.0477 0.0923 0.8360
12.750 1.4891 0.03438 0.02779 -0.0467 0.0913 0.8397
13.000 1.5029 0.03541 0.02889 -0.0458 0.0902 0.8438
13.250 1.5162 0.03651 0.03004 -0.0450 0.0891 0.8483
13.500 1.5290 0.03765 0.03122 -0.0442 0.0881 0.8528
13.750 1.5400 0.03888 0.03249 -0.0431 0.0870 0.8575
14.000 1.5517 0.04022 0.03384 -0.0418 0.0854 0.8625
14.250 1.5631 0.04150 0.03523 -0.0411 0.0848 0.8681
14.500 1.5730 0.04283 0.03670 -0.0402 0.0840 0.8734
14.750 1.5827 0.04423 0.03822 -0.0394 0.0830 0.8795
15.000 1.5921 0.04570 0.03979 -0.0387 0.0820 0.8860
15.250 1.6006 0.04720 0.04139 -0.0379 0.0809 0.8929
15.500 1.6093 0.04878 0.04304 -0.0373 0.0799 0.9010
15.750 1.6164 0.05042 0.04475 -0.0366 0.0789 0.9102
16.000 1.6229 0.05209 0.04647 -0.0357 0.0778 0.9218
16.250 1.6277 0.05369 0.04813 -0.0342 0.0765 0.9404
16.500 1.6293 0.05564 0.05024 -0.0334 0.0759 1.0000
16.750 1.6354 0.05796 0.05269 -0.0336 0.0749 1.0000
17.000 1.6412 0.06031 0.05513 -0.0338 0.0738 1.0000
17.250 1.6466 0.06270 0.05761 -0.0341 0.0728 1.0000
17.500 1.6513 0.06520 0.06017 -0.0344 0.0717 1.0000
17.750 1.6555 0.06776 0.06278 -0.0347 0.0708 1.0000
18.000 1.6588 0.07041 0.06546 -0.0350 0.0698 1.0000
18.250 1.6602 0.07314 0.06820 -0.0350 0.0685 1.0000
18.500 1.6593 0.07662 0.07185 -0.0359 0.0677 1.0000
18.750 1.6582 0.08012 0.07549 -0.0368 0.0667 1.0000
19.000 1.6570 0.08365 0.07912 -0.0378 0.0656 1.0000
19.250 1.6557 0.08724 0.08280 -0.0389 0.0646 1.0000
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