NASA/LANGLEY LS(1)-0417MOD AIRFOIL (ls417mod-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: NASA/LANGLEY LS(1)-0417MOD AIRFOIL (ls417mod-il) Reynolds number: 1,000,000 Max Cl/Cd: 102.96 at α=8.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-ls417mod-il-1000000.txt Download as CSV file: xf-ls417mod-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: NASA/LANGLEY LS(1)-0417MOD 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
------ -------- --------- --------- -------- -------- --------
-19.500 -0.9388 0.12166 0.11873 -0.0313 1.0000 0.0146
-19.250 -0.9663 0.11230 0.10920 -0.0368 1.0000 0.0146
-19.000 -0.9902 0.10388 0.10064 -0.0416 1.0000 0.0147
-18.750 -1.0107 0.09637 0.09298 -0.0459 1.0000 0.0147
-18.500 -1.0285 0.08951 0.08599 -0.0497 1.0000 0.0147
-18.250 -1.0437 0.08320 0.07956 -0.0531 1.0000 0.0148
-18.000 -1.0558 0.07755 0.07381 -0.0560 1.0000 0.0149
-17.750 -1.0657 0.07234 0.06849 -0.0587 1.0000 0.0149
-17.500 -1.0728 0.06766 0.06371 -0.0611 1.0000 0.0150
-17.250 -1.0777 0.06342 0.05939 -0.0631 1.0000 0.0151
-17.000 -1.0808 0.05956 0.05544 -0.0649 1.0000 0.0151
-16.750 -1.0821 0.05604 0.05184 -0.0663 1.0000 0.0152
-16.500 -1.0818 0.05286 0.04859 -0.0675 1.0000 0.0153
-16.250 -1.0806 0.04993 0.04559 -0.0685 1.0000 0.0154
-16.000 -1.0777 0.04728 0.04287 -0.0692 1.0000 0.0155
-15.750 -1.0742 0.04484 0.04035 -0.0698 1.0000 0.0157
-15.500 -1.0701 0.04258 0.03803 -0.0701 1.0000 0.0158
-15.250 -1.0651 0.04050 0.03588 -0.0702 1.0000 0.0159
-15.000 -1.0590 0.03859 0.03391 -0.0701 1.0000 0.0161
-14.750 -1.0523 0.03678 0.03203 -0.0700 1.0000 0.0162
-14.500 -1.0445 0.03512 0.03030 -0.0697 1.0000 0.0164
-14.250 -1.0361 0.03356 0.02868 -0.0693 1.0000 0.0166
-14.000 -1.0271 0.03211 0.02716 -0.0689 1.0000 0.0167
-13.750 -1.0170 0.03079 0.02579 -0.0682 1.0000 0.0169
-13.500 -1.0068 0.02956 0.02450 -0.0675 1.0000 0.0171
-13.250 -0.9960 0.02846 0.02334 -0.0666 1.0000 0.0172
-13.000 -0.9853 0.02748 0.02230 -0.0654 1.0000 0.0173
-12.750 -0.9797 0.02629 0.02106 -0.0636 1.0000 0.0175
-12.500 -0.9812 0.02490 0.01964 -0.0608 1.0000 0.0178
-12.250 -0.9832 0.02396 0.01868 -0.0573 1.0000 0.0180
-12.000 -0.9818 0.02315 0.01785 -0.0544 0.9992 0.0181
-11.750 -0.9540 0.02218 0.01686 -0.0562 0.9963 0.0184
-11.500 -0.9233 0.02129 0.01596 -0.0583 0.9935 0.0188
-11.250 -0.8922 0.02044 0.01509 -0.0603 0.9904 0.0192
-11.000 -0.8619 0.01966 0.01427 -0.0620 0.9859 0.0196
-10.750 -0.8291 0.01898 0.01355 -0.0641 0.9824 0.0200
-10.500 -0.7955 0.01838 0.01292 -0.0662 0.9782 0.0204
-10.250 -0.7675 0.01728 0.01177 -0.0678 0.9685 0.0210
-10.000 -0.7373 0.01652 0.01101 -0.0693 0.9578 0.0215
-9.750 -0.7083 0.01598 0.01042 -0.0702 0.9457 0.0220
-9.500 -0.6814 0.01551 0.00990 -0.0705 0.9327 0.0225
-9.250 -0.6556 0.01510 0.00943 -0.0705 0.9200 0.0231
-9.000 -0.6292 0.01474 0.00900 -0.0706 0.9085 0.0235
-8.750 -0.6034 0.01426 0.00845 -0.0707 0.8968 0.0240
-8.500 -0.5772 0.01372 0.00789 -0.0709 0.8869 0.0248
-8.250 -0.5498 0.01338 0.00750 -0.0711 0.8778 0.0255
-8.000 -0.5217 0.01306 0.00715 -0.0715 0.8705 0.0262
-7.750 -0.4933 0.01278 0.00683 -0.0718 0.8622 0.0270
-7.500 -0.4653 0.01240 0.00639 -0.0721 0.8537 0.0280
-7.250 -0.4362 0.01207 0.00607 -0.0726 0.8478 0.0290
-7.000 -0.4069 0.01180 0.00578 -0.0731 0.8413 0.0301
-6.750 -0.3777 0.01156 0.00548 -0.0734 0.8337 0.0312
-6.500 -0.3480 0.01122 0.00516 -0.0740 0.8268 0.0328
-6.250 -0.3180 0.01099 0.00491 -0.0745 0.8203 0.0345
-6.000 -0.2880 0.01072 0.00463 -0.0751 0.8141 0.0369
-5.750 -0.2578 0.01049 0.00439 -0.0757 0.8074 0.0404
-5.500 -0.2271 0.01020 0.00414 -0.0764 0.8008 0.0466
-5.250 -0.1963 0.00987 0.00388 -0.0772 0.7934 0.0616
-5.000 -0.1652 0.00951 0.00363 -0.0781 0.7860 0.0891
-4.750 -0.1333 0.00914 0.00341 -0.0793 0.7794 0.1222
-4.500 -0.1014 0.00878 0.00320 -0.0804 0.7703 0.1583
-4.250 -0.0689 0.00840 0.00298 -0.0817 0.7610 0.2078
-4.000 -0.0351 0.00792 0.00276 -0.0834 0.7512 0.2744
-3.750 -0.0018 0.00755 0.00258 -0.0848 0.7383 0.3365
-3.500 0.0321 0.00718 0.00239 -0.0864 0.7214 0.4044
-3.250 0.0664 0.00681 0.00222 -0.0881 0.7004 0.4778
-3.000 0.0996 0.00661 0.00213 -0.0894 0.6666 0.5501
-2.750 0.1270 0.00703 0.00221 -0.0894 0.5552 0.5908
-2.500 0.1544 0.00754 0.00240 -0.0894 0.4703 0.6137
-2.000 0.2138 0.00794 0.00259 -0.0899 0.4230 0.6371
-1.750 0.2439 0.00809 0.00266 -0.0902 0.4098 0.6441
-1.500 0.2740 0.00825 0.00272 -0.0906 0.3975 0.6492
-1.250 0.3041 0.00833 0.00278 -0.0909 0.3885 0.6552
-1.000 0.3338 0.00847 0.00288 -0.0911 0.3801 0.6617
-0.750 0.3635 0.00863 0.00298 -0.0913 0.3709 0.6667
-0.500 0.3939 0.00872 0.00303 -0.0917 0.3655 0.6701
-0.250 0.4240 0.00884 0.00309 -0.0921 0.3584 0.6722
0.000 0.4536 0.00892 0.00312 -0.0924 0.3504 0.6755
0.250 0.4838 0.00896 0.00315 -0.0927 0.3462 0.6780
0.500 0.5137 0.00904 0.00321 -0.0930 0.3408 0.6804
0.750 0.5431 0.00917 0.00330 -0.0932 0.3347 0.6832
1.000 0.5724 0.00932 0.00341 -0.0934 0.3285 0.6867
1.250 0.6024 0.00941 0.00349 -0.0937 0.3249 0.6902
1.500 0.6321 0.00953 0.00358 -0.0940 0.3200 0.6929
1.750 0.6616 0.00966 0.00366 -0.0942 0.3147 0.6951
2.000 0.6907 0.00976 0.00373 -0.0945 0.3089 0.6982
2.250 0.7205 0.00981 0.00379 -0.0948 0.3057 0.7001
2.500 0.7500 0.00989 0.00387 -0.0951 0.3015 0.7019
2.750 0.7791 0.01002 0.00397 -0.0953 0.2967 0.7036
3.000 0.8076 0.01020 0.00409 -0.0954 0.2906 0.7052
3.250 0.8372 0.01026 0.00418 -0.0957 0.2880 0.7067
3.500 0.8665 0.01036 0.00427 -0.0959 0.2841 0.7084
3.750 0.8954 0.01049 0.00437 -0.0961 0.2795 0.7102
4.000 0.9237 0.01068 0.00451 -0.0962 0.2741 0.7119
4.250 0.9528 0.01079 0.00462 -0.0964 0.2707 0.7133
4.500 0.9818 0.01089 0.00473 -0.0967 0.2671 0.7146
4.750 1.0104 0.01104 0.00485 -0.0968 0.2627 0.7156
5.000 1.0384 0.01122 0.00499 -0.0969 0.2576 0.7171
5.250 1.0668 0.01133 0.00511 -0.0970 0.2540 0.7195
5.500 1.0953 0.01143 0.00524 -0.0972 0.2504 0.7217
5.750 1.1232 0.01159 0.00539 -0.0972 0.2461 0.7237
6.000 1.1503 0.01181 0.00558 -0.0971 0.2410 0.7256
6.250 1.1782 0.01196 0.00575 -0.0971 0.2376 0.7274
6.500 1.2061 0.01210 0.00591 -0.0972 0.2337 0.7293
6.750 1.2332 0.01230 0.00609 -0.0971 0.2291 0.7312
7.000 1.2596 0.01256 0.00631 -0.0969 0.2241 0.7331
7.250 1.2873 0.01270 0.00648 -0.0969 0.2209 0.7349
7.500 1.3142 0.01289 0.00667 -0.0968 0.2166 0.7365
7.750 1.3401 0.01317 0.00691 -0.0966 0.2115 0.7378
8.000 1.3667 0.01334 0.00711 -0.0965 0.2077 0.7405
8.250 1.3930 0.01353 0.00732 -0.0963 0.2034 0.7433
8.500 1.4180 0.01381 0.00759 -0.0959 0.1984 0.7458
8.750 1.4434 0.01405 0.00785 -0.0955 0.1942 0.7483
9.000 1.4688 0.01429 0.00810 -0.0952 0.1899 0.7507
9.250 1.4928 0.01461 0.00840 -0.0946 0.1848 0.7531
9.500 1.5173 0.01488 0.00869 -0.0942 0.1806 0.7555
9.750 1.5414 0.01517 0.00898 -0.0936 0.1759 0.7576
10.000 1.5635 0.01557 0.00935 -0.0928 0.1705 0.7594
10.250 1.5873 0.01581 0.00963 -0.0922 0.1666 0.7630
10.500 1.6088 0.01617 0.01000 -0.0913 0.1617 0.7660
10.750 1.6297 0.01654 0.01039 -0.0903 0.1572 0.7689
11.000 1.6504 0.01690 0.01077 -0.0892 0.1527 0.7718
11.250 1.6680 0.01739 0.01124 -0.0876 0.1478 0.7748
11.500 1.6850 0.01775 0.01163 -0.0858 0.1441 0.7777
11.750 1.7009 0.01826 0.01214 -0.0840 0.1395 0.7800
12.000 1.7181 0.01876 0.01267 -0.0825 0.1353 0.7840
12.250 1.7346 0.01930 0.01324 -0.0809 0.1306 0.7876
12.500 1.7498 0.01994 0.01389 -0.0793 0.1258 0.7912
12.750 1.7653 0.02059 0.01455 -0.0777 0.1210 0.7948
13.000 1.7792 0.02134 0.01530 -0.0760 0.1165 0.7981
13.250 1.7933 0.02209 0.01607 -0.0744 0.1119 0.8015
13.500 1.8061 0.02294 0.01695 -0.0728 0.1076 0.8054
13.750 1.8188 0.02380 0.01785 -0.0712 0.1037 0.8092
14.000 1.8299 0.02482 0.01889 -0.0695 0.1002 0.8130
14.250 1.8425 0.02576 0.01987 -0.0681 0.0969 0.8166
14.500 1.8512 0.02699 0.02111 -0.0664 0.0935 0.8203
14.750 1.8623 0.02807 0.02227 -0.0651 0.0906 0.8245
15.000 1.8707 0.02940 0.02364 -0.0636 0.0874 0.8287
15.250 1.8784 0.03083 0.02511 -0.0622 0.0847 0.8330
15.500 1.8860 0.03230 0.02663 -0.0609 0.0820 0.8369
15.750 1.8901 0.03408 0.02847 -0.0595 0.0794 0.8416
16.000 1.8966 0.03572 0.03019 -0.0583 0.0772 0.8464
16.250 1.9001 0.03766 0.03219 -0.0572 0.0749 0.8515
16.500 1.8996 0.04003 0.03462 -0.0560 0.0727 0.8565
16.750 1.9024 0.04217 0.03685 -0.0551 0.0709 0.8623
17.000 1.9022 0.04469 0.03946 -0.0544 0.0689 0.8684
17.250 1.8974 0.04778 0.04263 -0.0537 0.0671 0.8743
17.500 1.8937 0.05090 0.04585 -0.0533 0.0656 0.8813
17.750 1.8891 0.05428 0.04935 -0.0532 0.0640 0.8885
18.000 1.8793 0.05842 0.05360 -0.0534 0.0625 0.8972
18.250 1.8635 0.06352 0.05883 -0.0541 0.0612 0.9072
18.500 1.8474 0.06880 0.06429 -0.0550 0.0602 0.9234
18.750 1.8265 0.07442 0.07010 -0.0558 0.0592 1.0000
19.000 1.8032 0.08131 0.07713 -0.0580 0.0583 1.0000
19.250 1.7749 0.08893 0.08488 -0.0604 0.0575 1.0000
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