NASA/LANGLEY MS(1)-0317 AIRFOIL (ms317-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: NASA/LANGLEY MS(1)-0317 AIRFOIL (ms317-il) Reynolds number: 1,000,000 Max Cl/Cd: 80.67 at α=7.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-ms317-il-1000000-n5.txt Download as CSV file: xf-ms317-il-1000000-n5.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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.2481 0.07949 0.07540 -0.0493 1.0000 0.0149
-19.500 -1.2623 0.07376 0.06955 -0.0521 1.0000 0.0150
-19.250 -1.2722 0.06882 0.06450 -0.0544 1.0000 0.0151
-19.000 -1.2794 0.06437 0.05996 -0.0564 1.0000 0.0152
-18.750 -1.2838 0.06046 0.05595 -0.0579 1.0000 0.0153
-18.500 -1.2860 0.05695 0.05236 -0.0592 1.0000 0.0154
-18.250 -1.2862 0.05377 0.04910 -0.0603 1.0000 0.0156
-18.000 -1.2849 0.05086 0.04612 -0.0612 1.0000 0.0157
-17.750 -1.2824 0.04819 0.04337 -0.0618 1.0000 0.0159
-17.500 -1.2784 0.04576 0.04087 -0.0624 1.0000 0.0160
-17.250 -1.2730 0.04354 0.03859 -0.0627 1.0000 0.0162
-17.000 -1.2669 0.04147 0.03646 -0.0629 1.0000 0.0163
-16.750 -1.2603 0.03953 0.03445 -0.0631 1.0000 0.0165
-16.500 -1.2523 0.03779 0.03265 -0.0630 1.0000 0.0167
-16.250 -1.2439 0.03614 0.03094 -0.0629 1.0000 0.0168
-16.000 -1.2344 0.03461 0.02935 -0.0628 1.0000 0.0170
-15.750 -1.2238 0.03320 0.02788 -0.0626 1.0000 0.0171
-15.500 -1.2150 0.03165 0.02629 -0.0623 1.0000 0.0174
-15.250 -1.2044 0.03028 0.02488 -0.0619 1.0000 0.0176
-15.000 -1.1927 0.02901 0.02358 -0.0616 1.0000 0.0179
-14.750 -1.1796 0.02788 0.02242 -0.0612 1.0000 0.0182
-14.500 -1.1661 0.02680 0.02131 -0.0608 1.0000 0.0185
-14.250 -1.1515 0.02581 0.02030 -0.0604 1.0000 0.0188
-14.000 -1.1367 0.02487 0.01932 -0.0599 1.0000 0.0191
-13.750 -1.1213 0.02399 0.01841 -0.0594 1.0000 0.0195
-13.500 -1.1028 0.02314 0.01753 -0.0595 0.9924 0.0198
-13.250 -1.0788 0.02231 0.01665 -0.0605 0.9732 0.0201
-12.750 -1.0432 0.02068 0.01489 -0.0598 0.9305 0.0209
-12.500 -1.0267 0.01998 0.01412 -0.0590 0.9139 0.0213
-12.250 -1.0091 0.01933 0.01340 -0.0583 0.9001 0.0217
-12.000 -0.9914 0.01870 0.01271 -0.0577 0.8885 0.0222
-11.750 -0.9742 0.01815 0.01209 -0.0568 0.8774 0.0226
-11.500 -0.9525 0.01761 0.01149 -0.0568 0.8677 0.0231
-11.250 -0.9297 0.01712 0.01093 -0.0568 0.8585 0.0235
-11.000 -0.9065 0.01654 0.01032 -0.0570 0.8504 0.0243
-10.750 -0.8822 0.01606 0.00980 -0.0572 0.8423 0.0250
-10.500 -0.8572 0.01564 0.00933 -0.0574 0.8354 0.0257
-10.250 -0.8316 0.01525 0.00891 -0.0576 0.8282 0.0264
-10.000 -0.8056 0.01492 0.00852 -0.0578 0.8217 0.0270
-9.750 -0.7795 0.01452 0.00810 -0.0580 0.8164 0.0279
-9.500 -0.7528 0.01415 0.00772 -0.0583 0.8110 0.0289
-9.250 -0.7257 0.01383 0.00738 -0.0586 0.8055 0.0299
-8.750 -0.6705 0.01320 0.00671 -0.0594 0.7961 0.0327
-8.500 -0.6424 0.01290 0.00641 -0.0598 0.7915 0.0344
-8.250 -0.6141 0.01262 0.00611 -0.0602 0.7869 0.0362
-8.000 -0.5857 0.01235 0.00583 -0.0606 0.7824 0.0385
-7.750 -0.5569 0.01208 0.00557 -0.0611 0.7784 0.0412
-7.500 -0.5278 0.01182 0.00532 -0.0617 0.7741 0.0448
-7.250 -0.4986 0.01155 0.00507 -0.0622 0.7696 0.0492
-7.000 -0.4693 0.01131 0.00484 -0.0628 0.7654 0.0537
-6.750 -0.4398 0.01111 0.00463 -0.0633 0.7612 0.0583
-6.250 -0.3798 0.01065 0.00423 -0.0647 0.7537 0.0697
-6.000 -0.3497 0.01045 0.00405 -0.0653 0.7497 0.0755
-5.750 -0.3195 0.01026 0.00388 -0.0660 0.7456 0.0815
-5.500 -0.2892 0.01009 0.00371 -0.0666 0.7415 0.0889
-5.250 -0.2585 0.00988 0.00355 -0.0674 0.7383 0.0973
-5.000 -0.2277 0.00968 0.00339 -0.0682 0.7349 0.1068
-4.750 -0.1969 0.00947 0.00324 -0.0690 0.7313 0.1200
-4.500 -0.1659 0.00927 0.00310 -0.0698 0.7277 0.1365
-4.250 -0.1348 0.00904 0.00295 -0.0707 0.7241 0.1572
-4.000 -0.1031 0.00874 0.00279 -0.0718 0.7211 0.1913
-3.750 -0.0712 0.00847 0.00265 -0.0729 0.7179 0.2238
-3.500 -0.0391 0.00819 0.00252 -0.0741 0.7142 0.2607
-3.250 -0.0068 0.00791 0.00238 -0.0753 0.7101 0.3015
-3.000 0.0259 0.00760 0.00224 -0.0766 0.7060 0.3535
-2.750 0.0596 0.00718 0.00207 -0.0783 0.7024 0.4270
-2.500 0.0931 0.00687 0.00197 -0.0798 0.6992 0.4866
-2.250 0.1257 0.00668 0.00192 -0.0809 0.6952 0.5292
-2.000 0.1573 0.00661 0.00190 -0.0817 0.6892 0.5549
-1.750 0.1885 0.00657 0.00189 -0.0824 0.6764 0.5780
-1.500 0.2191 0.00660 0.00190 -0.0829 0.6562 0.5996
-1.250 0.2494 0.00667 0.00190 -0.0834 0.6378 0.6100
-1.000 0.2798 0.00673 0.00192 -0.0838 0.6235 0.6185
-0.750 0.3100 0.00683 0.00194 -0.0843 0.6063 0.6265
-0.500 0.3399 0.00694 0.00200 -0.0846 0.5842 0.6352
-0.250 0.3697 0.00710 0.00205 -0.0850 0.5604 0.6427
0.000 0.3992 0.00726 0.00213 -0.0853 0.5354 0.6485
0.250 0.4278 0.00752 0.00223 -0.0855 0.4953 0.6520
0.500 0.4548 0.00797 0.00240 -0.0855 0.4324 0.6546
0.750 0.4820 0.00840 0.00258 -0.0855 0.3781 0.6570
1.000 0.5096 0.00877 0.00274 -0.0856 0.3353 0.6591
1.250 0.5373 0.00911 0.00290 -0.0858 0.2982 0.6611
1.500 0.5652 0.00941 0.00305 -0.0859 0.2672 0.6628
1.750 0.5931 0.00969 0.00320 -0.0860 0.2406 0.6648
2.000 0.6210 0.00995 0.00336 -0.0861 0.2167 0.6668
2.250 0.6488 0.01022 0.00353 -0.0862 0.1959 0.6689
2.500 0.6767 0.01046 0.00369 -0.0863 0.1798 0.6709
2.750 0.7048 0.01068 0.00384 -0.0864 0.1676 0.6729
3.000 0.7327 0.01090 0.00400 -0.0865 0.1571 0.6747
3.250 0.7608 0.01110 0.00415 -0.0866 0.1486 0.6765
3.500 0.7887 0.01131 0.00431 -0.0867 0.1412 0.6785
3.750 0.8165 0.01152 0.00448 -0.0868 0.1344 0.6805
4.000 0.8441 0.01173 0.00465 -0.0868 0.1284 0.6819
4.250 0.8718 0.01192 0.00482 -0.0868 0.1232 0.6838
4.500 0.8988 0.01216 0.00502 -0.0868 0.1174 0.6856
4.750 0.9263 0.01234 0.00520 -0.0868 0.1137 0.6873
5.000 0.9532 0.01257 0.00541 -0.0867 0.1097 0.6891
5.250 0.9798 0.01281 0.00563 -0.0866 0.1059 0.6910
5.500 1.0068 0.01301 0.00583 -0.0865 0.1038 0.6931
5.750 1.0334 0.01323 0.00604 -0.0864 0.1015 0.6949
6.000 1.0595 0.01347 0.00628 -0.0861 0.0991 0.6966
6.250 1.0852 0.01374 0.00652 -0.0859 0.0967 0.6982
6.500 1.1108 0.01399 0.00677 -0.0856 0.0948 0.6997
6.750 1.1366 0.01422 0.00701 -0.0853 0.0936 0.7010
7.000 1.1619 0.01447 0.00727 -0.0849 0.0922 0.7026
7.250 1.1866 0.01473 0.00754 -0.0845 0.0906 0.7046
7.500 1.2108 0.01501 0.00783 -0.0840 0.0891 0.7067
7.750 1.2344 0.01531 0.00814 -0.0834 0.0877 0.7088
8.000 1.2573 0.01564 0.00848 -0.0826 0.0862 0.7110
8.250 1.2798 0.01596 0.00882 -0.0818 0.0852 0.7130
8.500 1.3023 0.01625 0.00914 -0.0810 0.0846 0.7151
8.750 1.3240 0.01656 0.00948 -0.0801 0.0838 0.7172
9.000 1.3439 0.01688 0.00983 -0.0788 0.0829 0.7192
9.250 1.3605 0.01724 0.01021 -0.0769 0.0821 0.7209
9.500 1.3791 0.01764 0.01064 -0.0756 0.0812 0.7229
9.750 1.3980 0.01808 0.01111 -0.0743 0.0803 0.7252
10.000 1.4165 0.01856 0.01161 -0.0730 0.0790 0.7274
10.250 1.4339 0.01912 0.01218 -0.0717 0.0774 0.7297
10.500 1.4522 0.01964 0.01274 -0.0705 0.0762 0.7321
10.750 1.4712 0.02013 0.01328 -0.0695 0.0756 0.7347
11.000 1.4894 0.02068 0.01387 -0.0684 0.0749 0.7373
11.250 1.5073 0.02126 0.01449 -0.0673 0.0742 0.7396
11.500 1.5248 0.02189 0.01515 -0.0663 0.0734 0.7419
11.750 1.5420 0.02254 0.01585 -0.0652 0.0725 0.7447
12.000 1.5584 0.02326 0.01660 -0.0641 0.0716 0.7475
12.250 1.5745 0.02401 0.01740 -0.0630 0.0706 0.7504
12.500 1.5897 0.02485 0.01827 -0.0619 0.0697 0.7534
12.750 1.6038 0.02578 0.01923 -0.0607 0.0687 0.7563
13.000 1.6197 0.02658 0.02009 -0.0598 0.0683 0.7591
13.250 1.6353 0.02742 0.02099 -0.0589 0.0677 0.7619
13.500 1.6505 0.02831 0.02194 -0.0579 0.0670 0.7653
13.750 1.6652 0.02924 0.02294 -0.0570 0.0661 0.7689
14.000 1.6792 0.03024 0.02398 -0.0561 0.0651 0.7728
14.250 1.6923 0.03131 0.02509 -0.0551 0.0641 0.7766
14.750 1.7161 0.03369 0.02756 -0.0532 0.0622 0.7841
15.000 1.7274 0.03496 0.02889 -0.0522 0.0613 0.7882
15.250 1.7393 0.03618 0.03018 -0.0514 0.0607 0.7924
15.500 1.7506 0.03744 0.03152 -0.0506 0.0599 0.7964
15.750 1.7610 0.03882 0.03296 -0.0497 0.0589 0.8002
16.000 1.7711 0.04025 0.03445 -0.0489 0.0578 0.8047
16.250 1.7798 0.04184 0.03610 -0.0482 0.0567 0.8094
16.500 1.7878 0.04352 0.03781 -0.0474 0.0555 0.8140
16.750 1.7955 0.04526 0.03962 -0.0467 0.0545 0.8184
17.000 1.8039 0.04694 0.04139 -0.0461 0.0534 0.8235
17.250 1.8106 0.04885 0.04336 -0.0456 0.0521 0.8288
17.500 1.8165 0.05086 0.04543 -0.0450 0.0509 0.8339
17.750 1.8206 0.05310 0.04773 -0.0446 0.0497 0.8391
18.000 1.8246 0.05538 0.05009 -0.0442 0.0487 0.8454
18.250 1.8289 0.05765 0.05244 -0.0439 0.0476 0.8516
18.500 1.8310 0.06022 0.05510 -0.0436 0.0465 0.8584
18.750 1.8317 0.06299 0.05795 -0.0435 0.0454 0.8657
19.000 1.8307 0.06600 0.06103 -0.0434 0.0443 0.8730
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