NASA/LANGLEY MS(1)-0317 AIRFOIL (ms317-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: NASA/LANGLEY MS(1)-0317 AIRFOIL (ms317-il) Reynolds number: 1,000,000 Max Cl/Cd: 80.43 at α=1.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-ms317-il-1000000.txt Download as CSV file: xf-ms317-il-1000000.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 = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.1510 0.09368 0.09004 -0.0430 1.0000 0.0186
-19.500 -1.1630 0.08800 0.08426 -0.0459 1.0000 0.0187
-19.250 -1.1736 0.08257 0.07873 -0.0487 1.0000 0.0189
-19.000 -1.1825 0.07752 0.07357 -0.0512 1.0000 0.0190
-18.750 -1.1898 0.07285 0.06880 -0.0534 1.0000 0.0191
-18.500 -1.1954 0.06849 0.06435 -0.0554 1.0000 0.0192
-18.250 -1.1993 0.06447 0.06023 -0.0572 1.0000 0.0194
-18.000 -1.2013 0.06082 0.05649 -0.0586 1.0000 0.0195
-17.750 -1.2018 0.05748 0.05305 -0.0599 1.0000 0.0197
-17.500 -1.2007 0.05440 0.04989 -0.0609 1.0000 0.0198
-17.250 -1.1979 0.05161 0.04700 -0.0618 1.0000 0.0200
-17.000 -1.1935 0.04909 0.04441 -0.0625 1.0000 0.0201
-16.750 -1.1902 0.04656 0.04180 -0.0630 1.0000 0.0202
-16.500 -1.1944 0.04337 0.03853 -0.0634 1.0000 0.0205
-16.250 -1.1931 0.04086 0.03596 -0.0636 1.0000 0.0208
-16.000 -1.1886 0.03875 0.03380 -0.0637 1.0000 0.0210
-15.750 -1.1818 0.03691 0.03192 -0.0636 1.0000 0.0212
-15.500 -1.1730 0.03530 0.03026 -0.0635 1.0000 0.0215
-15.250 -1.1635 0.03377 0.02868 -0.0633 1.0000 0.0218
-15.000 -1.1528 0.03236 0.02724 -0.0631 1.0000 0.0221
-14.750 -1.1415 0.03103 0.02585 -0.0628 1.0000 0.0224
-14.500 -1.1294 0.02978 0.02456 -0.0624 1.0000 0.0227
-14.250 -1.1163 0.02863 0.02336 -0.0621 1.0000 0.0230
-14.000 -1.1018 0.02761 0.02229 -0.0617 1.0000 0.0233
-13.750 -1.0876 0.02659 0.02121 -0.0613 1.0000 0.0235
-13.500 -1.0811 0.02501 0.01961 -0.0605 1.0000 0.0241
-13.250 -1.0689 0.02393 0.01851 -0.0597 1.0000 0.0246
-13.000 -1.0551 0.02303 0.01759 -0.0590 1.0000 0.0250
-12.750 -1.0418 0.02223 0.01678 -0.0580 1.0000 0.0254
-12.500 -1.0300 0.02148 0.01601 -0.0567 0.9992 0.0259
-12.250 -1.0009 0.02066 0.01515 -0.0585 0.9930 0.0264
-12.000 -0.9727 0.01993 0.01438 -0.0600 0.9836 0.0269
-11.750 -0.9502 0.01889 0.01329 -0.0608 0.9694 0.0276
-11.500 -0.9335 0.01808 0.01243 -0.0602 0.9514 0.0283
-11.250 -0.9145 0.01747 0.01177 -0.0596 0.9356 0.0290
-11.000 -0.8930 0.01693 0.01118 -0.0594 0.9222 0.0298
-10.750 -0.8700 0.01646 0.01063 -0.0594 0.9109 0.0305
-10.500 -0.8470 0.01594 0.01003 -0.0594 0.8998 0.0314
-10.250 -0.8237 0.01535 0.00942 -0.0594 0.8902 0.0325
-10.000 -0.7990 0.01494 0.00897 -0.0594 0.8813 0.0336
-9.750 -0.7730 0.01458 0.00856 -0.0596 0.8738 0.0347
-9.500 -0.7472 0.01416 0.00810 -0.0598 0.8663 0.0359
-9.250 -0.7213 0.01376 0.00767 -0.0599 0.8591 0.0375
-9.000 -0.6939 0.01343 0.00732 -0.0603 0.8533 0.0392
-8.750 -0.6667 0.01305 0.00694 -0.0606 0.8470 0.0414
-8.500 -0.6392 0.01275 0.00661 -0.0609 0.8410 0.0440
-8.250 -0.6111 0.01241 0.00627 -0.0614 0.8360 0.0472
-8.000 -0.5826 0.01212 0.00598 -0.0618 0.8306 0.0508
-7.750 -0.5542 0.01181 0.00568 -0.0623 0.8252 0.0559
-7.500 -0.5255 0.01154 0.00541 -0.0628 0.8196 0.0618
-7.250 -0.4961 0.01124 0.00516 -0.0634 0.8153 0.0682
-7.000 -0.4666 0.01098 0.00493 -0.0640 0.8106 0.0746
-6.750 -0.4370 0.01077 0.00471 -0.0645 0.8057 0.0810
-6.500 -0.4074 0.01056 0.00450 -0.0651 0.8005 0.0884
-6.250 -0.3772 0.01029 0.00429 -0.0659 0.7968 0.0971
-6.000 -0.3469 0.01004 0.00409 -0.0666 0.7926 0.1070
-5.750 -0.3165 0.00979 0.00389 -0.0674 0.7881 0.1198
-5.500 -0.2860 0.00955 0.00369 -0.0682 0.7836 0.1371
-5.250 -0.2551 0.00927 0.00351 -0.0691 0.7795 0.1598
-5.000 -0.2238 0.00898 0.00333 -0.0701 0.7761 0.1866
-4.750 -0.1922 0.00866 0.00315 -0.0712 0.7723 0.2192
-4.500 -0.1602 0.00829 0.00296 -0.0725 0.7685 0.2632
-4.250 -0.1276 0.00787 0.00275 -0.0740 0.7646 0.3219
-4.000 -0.0927 0.00718 0.00247 -0.0763 0.7607 0.4327
-3.750 -0.0585 0.00672 0.00232 -0.0781 0.7575 0.5164
-3.500 -0.0260 0.00654 0.00228 -0.0791 0.7538 0.5574
-3.250 0.0056 0.00648 0.00227 -0.0799 0.7498 0.5811
-3.000 0.0369 0.00648 0.00227 -0.0805 0.7457 0.5977
-2.750 0.0680 0.00653 0.00229 -0.0811 0.7414 0.6099
-2.500 0.0992 0.00653 0.00230 -0.0817 0.7383 0.6194
-2.250 0.1304 0.00654 0.00230 -0.0823 0.7344 0.6270
-2.000 0.1612 0.00655 0.00231 -0.0828 0.7292 0.6336
-1.750 0.1917 0.00661 0.00231 -0.0832 0.7198 0.6408
-1.500 0.2221 0.00662 0.00229 -0.0835 0.7078 0.6484
-1.250 0.2525 0.00666 0.00232 -0.0839 0.6985 0.6537
-1.000 0.2831 0.00671 0.00234 -0.0844 0.6907 0.6584
-0.750 0.3138 0.00680 0.00236 -0.0848 0.6827 0.6628
-0.500 0.3440 0.00680 0.00240 -0.0852 0.6736 0.6688
-0.250 0.3740 0.00691 0.00248 -0.0854 0.6650 0.6742
0.000 0.4046 0.00698 0.00254 -0.0859 0.6575 0.6789
0.250 0.4349 0.00707 0.00257 -0.0863 0.6479 0.6814
0.500 0.4655 0.00708 0.00256 -0.0868 0.6369 0.6837
0.750 0.4954 0.00712 0.00257 -0.0872 0.6249 0.6863
1.000 0.5252 0.00720 0.00261 -0.0875 0.6105 0.6884
1.250 0.5549 0.00729 0.00265 -0.0878 0.5936 0.6905
1.500 0.5841 0.00744 0.00272 -0.0881 0.5728 0.6926
1.750 0.6129 0.00762 0.00280 -0.0883 0.5412 0.6947
2.000 0.6399 0.00801 0.00294 -0.0882 0.4868 0.6967
2.250 0.6646 0.00865 0.00320 -0.0879 0.4099 0.6985
2.500 0.6899 0.00922 0.00347 -0.0876 0.3491 0.7002
2.750 0.7158 0.00971 0.00372 -0.0875 0.3007 0.7015
3.000 0.7420 0.01008 0.00391 -0.0874 0.2626 0.7040
3.250 0.7685 0.01041 0.00411 -0.0873 0.2326 0.7061
3.750 0.8217 0.01107 0.00454 -0.0871 0.1891 0.7099
4.000 0.8484 0.01136 0.00475 -0.0870 0.1734 0.7120
4.250 0.8752 0.01164 0.00496 -0.0869 0.1611 0.7141
4.500 0.9022 0.01189 0.00517 -0.0868 0.1511 0.7160
4.750 0.9288 0.01217 0.00538 -0.0867 0.1420 0.7178
5.000 0.9555 0.01243 0.00560 -0.0866 0.1348 0.7193
5.250 0.9820 0.01270 0.00583 -0.0865 0.1285 0.7206
5.500 1.0086 0.01293 0.00603 -0.0863 0.1238 0.7224
5.750 1.0340 0.01321 0.00629 -0.0860 0.1183 0.7250
6.000 1.0603 0.01343 0.00653 -0.0858 0.1155 0.7271
6.250 1.0861 0.01367 0.00677 -0.0856 0.1128 0.7291
6.500 1.1112 0.01396 0.00705 -0.0852 0.1099 0.7309
6.750 1.1350 0.01433 0.00740 -0.0846 0.1064 0.7328
7.000 1.1601 0.01459 0.00767 -0.0842 0.1048 0.7348
7.250 1.1850 0.01484 0.00794 -0.0838 0.1033 0.7367
7.500 1.2093 0.01512 0.00824 -0.0833 0.1018 0.7385
7.750 1.2327 0.01544 0.00855 -0.0826 0.1002 0.7401
8.000 1.2552 0.01578 0.00890 -0.0818 0.0986 0.7422
8.250 1.2757 0.01618 0.00932 -0.0807 0.0968 0.7451
8.500 1.2941 0.01667 0.00984 -0.0792 0.0950 0.7475
8.750 1.3154 0.01696 0.01017 -0.0782 0.0943 0.7498
9.000 1.3322 0.01729 0.01054 -0.0764 0.0936 0.7522
9.250 1.3504 0.01768 0.01097 -0.0748 0.0928 0.7548
9.500 1.3695 0.01811 0.01143 -0.0736 0.0918 0.7572
9.750 1.3885 0.01857 0.01191 -0.0724 0.0907 0.7593
10.000 1.4072 0.01905 0.01241 -0.0712 0.0895 0.7615
10.250 1.4247 0.01961 0.01299 -0.0699 0.0880 0.7646
10.500 1.4387 0.02039 0.01380 -0.0683 0.0862 0.7674
10.750 1.4538 0.02114 0.01460 -0.0668 0.0852 0.7701
11.000 1.4727 0.02167 0.01518 -0.0658 0.0847 0.7729
11.250 1.4908 0.02227 0.01583 -0.0649 0.0841 0.7759
11.500 1.5085 0.02291 0.01650 -0.0639 0.0833 0.7787
11.750 1.5257 0.02358 0.01723 -0.0629 0.0825 0.7819
12.000 1.5427 0.02427 0.01797 -0.0619 0.0816 0.7853
12.250 1.5591 0.02502 0.01877 -0.0609 0.0807 0.7886
12.500 1.5745 0.02587 0.01965 -0.0599 0.0798 0.7920
12.750 1.5883 0.02683 0.02065 -0.0587 0.0789 0.7954
13.000 1.5992 0.02803 0.02187 -0.0574 0.0777 0.7984
13.250 1.6074 0.02945 0.02336 -0.0559 0.0766 0.8026
13.500 1.6240 0.03025 0.02424 -0.0552 0.0762 0.8066
13.750 1.6400 0.03110 0.02515 -0.0544 0.0755 0.8108
14.000 1.6551 0.03204 0.02615 -0.0536 0.0748 0.8149
14.250 1.6696 0.03302 0.02720 -0.0529 0.0739 0.8193
14.500 1.6830 0.03411 0.02835 -0.0520 0.0730 0.8243
14.750 1.6962 0.03522 0.02952 -0.0512 0.0721 0.8295
15.000 1.7074 0.03651 0.03084 -0.0504 0.0712 0.8344
15.250 1.7166 0.03796 0.03235 -0.0494 0.0702 0.8397
15.500 1.7204 0.03991 0.03436 -0.0482 0.0690 0.8452
15.750 1.7310 0.04133 0.03585 -0.0475 0.0683 0.8509
16.000 1.7438 0.04256 0.03718 -0.0470 0.0677 0.8570
16.250 1.7559 0.04387 0.03857 -0.0464 0.0668 0.8638
16.500 1.7665 0.04533 0.04010 -0.0459 0.0658 0.8705
16.750 1.7770 0.04680 0.04165 -0.0453 0.0648 0.8784
17.000 1.7852 0.04856 0.04346 -0.0448 0.0638 0.8868
17.250 1.7904 0.05058 0.04555 -0.0442 0.0626 0.8969
17.500 1.7914 0.05306 0.04811 -0.0435 0.0614 0.9091
17.750 1.8000 0.05462 0.04981 -0.0429 0.0607 0.9307
18.000 1.8045 0.05631 0.05162 -0.0420 0.0598 1.0000
18.250 1.8116 0.05839 0.05376 -0.0419 0.0587 1.0000
18.500 1.8170 0.06068 0.05609 -0.0418 0.0575 1.0000
18.750 1.8189 0.06342 0.05887 -0.0419 0.0564 1.0000
19.000 1.8151 0.06688 0.06238 -0.0420 0.0551 1.0000
19.250 1.8203 0.06924 0.06482 -0.0421 0.0542 1.0000
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