SELIG 3002-099-83 (s3002-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: SELIG 3002-099-83 (s3002-il) Reynolds number: 200,000 Max Cl/Cd: 70.81 at α=4.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-s3002-il-200000-n5.txt Download as CSV file: xf-s3002-il-200000-n5.csv |
XFOIL Version 6.96
Calculated polar for: SELIG 3002-099-83
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-8.750 -0.3651 0.08756 0.08397 -0.0358 1.0000 0.0161
-8.500 -0.3679 0.08371 0.08018 -0.0370 1.0000 0.0158
-8.000 -0.4098 0.07096 0.06763 -0.0416 1.0000 0.0140
-7.750 -0.4237 0.06835 0.06512 -0.0413 1.0000 0.0139
-7.500 -0.4103 0.06044 0.05713 -0.0532 0.9913 0.0138
-7.250 -0.3916 0.05166 0.04812 -0.0641 0.9818 0.0137
-6.750 -0.3511 0.03644 0.03202 -0.0772 0.9641 0.0146
-6.500 -0.3223 0.03358 0.02888 -0.0803 0.9588 0.0153
-6.250 -0.2983 0.02880 0.02350 -0.0824 0.9505 0.0155
-6.000 -0.2688 0.02502 0.01911 -0.0843 0.9448 0.0159
-5.750 -0.2405 0.02236 0.01594 -0.0851 0.9381 0.0165
-5.500 -0.2106 0.02026 0.01338 -0.0858 0.9318 0.0173
-5.250 -0.1793 0.01872 0.01154 -0.0867 0.9269 0.0183
-5.000 -0.1517 0.01804 0.01081 -0.0869 0.9191 0.0199
-4.750 -0.1209 0.01707 0.00964 -0.0874 0.9136 0.0217
-4.500 -0.0934 0.01605 0.00847 -0.0873 0.9061 0.0229
-4.250 -0.0648 0.01523 0.00765 -0.0875 0.8995 0.0244
-4.000 -0.0368 0.01468 0.00702 -0.0875 0.8922 0.0272
-3.750 -0.0091 0.01403 0.00633 -0.0875 0.8847 0.0300
-3.500 0.0188 0.01354 0.00580 -0.0874 0.8774 0.0330
-3.250 0.0463 0.01307 0.00528 -0.0873 0.8693 0.0371
-3.000 0.0741 0.01269 0.00484 -0.0872 0.8615 0.0417
-2.750 0.1017 0.01232 0.00445 -0.0870 0.8531 0.0497
-2.500 0.1293 0.01195 0.00409 -0.0869 0.8444 0.0660
-2.250 0.1568 0.01147 0.00381 -0.0868 0.8359 0.1216
-2.000 0.1838 0.01100 0.00361 -0.0869 0.8263 0.2033
-1.750 0.2109 0.01039 0.00342 -0.0870 0.8176 0.3368
-1.500 0.2337 0.00951 0.00355 -0.0861 0.8073 0.6083
-1.250 0.2576 0.00948 0.00372 -0.0846 0.7973 0.7061
-1.000 0.2838 0.00952 0.00370 -0.0837 0.7878 0.7395
-0.750 0.3101 0.00956 0.00368 -0.0830 0.7767 0.7621
-0.500 0.3366 0.00958 0.00364 -0.0824 0.7660 0.7797
-0.250 0.3618 0.00959 0.00361 -0.0813 0.7554 0.7984
0.000 0.3861 0.00960 0.00360 -0.0801 0.7435 0.8197
0.250 0.4107 0.00960 0.00357 -0.0790 0.7311 0.8372
0.500 0.4359 0.00959 0.00352 -0.0780 0.7182 0.8489
0.750 0.4621 0.00959 0.00346 -0.0774 0.7044 0.8577
1.000 0.4882 0.00960 0.00340 -0.0768 0.6897 0.8656
1.250 0.5143 0.00963 0.00336 -0.0763 0.6738 0.8731
1.500 0.5403 0.00966 0.00333 -0.0757 0.6565 0.8810
1.750 0.5661 0.00971 0.00331 -0.0750 0.6379 0.8889
2.000 0.5919 0.00978 0.00330 -0.0744 0.6181 0.8981
2.250 0.6174 0.00986 0.00330 -0.0737 0.5961 0.9082
2.750 0.6704 0.01008 0.00336 -0.0729 0.5486 0.9386
3.000 0.7019 0.01024 0.00342 -0.0737 0.5227 0.9821
3.250 0.7292 0.01051 0.00355 -0.0738 0.4971 1.0000
3.500 0.7561 0.01080 0.00372 -0.0737 0.4715 1.0000
3.750 0.7825 0.01111 0.00390 -0.0736 0.4465 1.0000
4.000 0.8086 0.01145 0.00411 -0.0735 0.4217 1.0000
4.250 0.8346 0.01179 0.00435 -0.0733 0.3982 1.0000
4.500 0.8602 0.01216 0.00461 -0.0731 0.3754 1.0000
4.750 0.8858 0.01251 0.00488 -0.0729 0.3544 1.0000
5.000 0.9113 0.01288 0.00518 -0.0726 0.3340 1.0000
5.250 0.9363 0.01328 0.00549 -0.0723 0.3144 1.0000
5.500 0.9613 0.01367 0.00582 -0.0720 0.2955 1.0000
5.750 0.9861 0.01407 0.00618 -0.0716 0.2769 1.0000
6.000 1.0106 0.01450 0.00655 -0.0712 0.2588 1.0000
6.250 1.0346 0.01495 0.00694 -0.0708 0.2409 1.0000
6.500 1.0583 0.01543 0.00736 -0.0703 0.2239 1.0000
6.750 1.0819 0.01590 0.00781 -0.0698 0.2072 1.0000
7.000 1.1053 0.01640 0.00827 -0.0693 0.1915 1.0000
7.250 1.1282 0.01692 0.00876 -0.0688 0.1763 1.0000
7.500 1.1507 0.01746 0.00929 -0.0681 0.1621 1.0000
7.750 1.1727 0.01804 0.00984 -0.0675 0.1492 1.0000
8.000 1.1943 0.01864 0.01042 -0.0667 0.1370 1.0000
8.250 1.2156 0.01924 0.01102 -0.0660 0.1254 1.0000
8.500 1.2366 0.01986 0.01167 -0.0651 0.1149 1.0000
8.750 1.2568 0.02052 0.01235 -0.0642 0.1059 1.0000
9.000 1.2757 0.02126 0.01308 -0.0632 0.0974 1.0000
9.250 1.2950 0.02195 0.01382 -0.0622 0.0895 1.0000
9.500 1.3126 0.02273 0.01465 -0.0610 0.0828 1.0000
9.750 1.3296 0.02352 0.01548 -0.0597 0.0766 1.0000
10.000 1.3448 0.02438 0.01639 -0.0582 0.0715 1.0000
10.250 1.3588 0.02520 0.01728 -0.0564 0.0668 1.0000
10.500 1.3692 0.02623 0.01833 -0.0544 0.0628 1.0000
10.750 1.3817 0.02714 0.01937 -0.0526 0.0596 1.0000
11.000 1.3928 0.02816 0.02048 -0.0508 0.0563 1.0000
11.250 1.4009 0.02939 0.02176 -0.0488 0.0535 1.0000
11.500 1.4087 0.03071 0.02316 -0.0470 0.0512 1.0000
11.750 1.4180 0.03198 0.02457 -0.0455 0.0490 1.0000
12.000 1.4258 0.03339 0.02610 -0.0440 0.0469 1.0000
12.250 1.4314 0.03502 0.02781 -0.0425 0.0450 1.0000
12.500 1.4335 0.03703 0.02990 -0.0411 0.0433 1.0000
12.750 1.4394 0.03883 0.03184 -0.0400 0.0419 1.0000
13.000 1.4446 0.04074 0.03392 -0.0390 0.0403 1.0000
13.250 1.4482 0.04288 0.03619 -0.0382 0.0389 1.0000
13.500 1.4507 0.04519 0.03863 -0.0376 0.0376 1.0000
13.750 1.4511 0.04783 0.04137 -0.0373 0.0365 1.0000
14.000 1.4484 0.05091 0.04453 -0.0371 0.0354 1.0000
14.250 1.4472 0.05399 0.04774 -0.0371 0.0345 1.0000
14.500 1.4470 0.05707 0.05102 -0.0373 0.0336 1.0000
14.750 1.4452 0.06047 0.05461 -0.0378 0.0327 1.0000
15.000 1.4421 0.06414 0.05845 -0.0386 0.0318 1.0000
15.250 1.4382 0.06810 0.06256 -0.0397 0.0310 1.0000
15.500 1.4330 0.07238 0.06698 -0.0411 0.0303 1.0000
15.750 1.4269 0.07698 0.07171 -0.0429 0.0296 1.0000
16.000 1.4197 0.08192 0.07676 -0.0449 0.0290 1.0000
16.250 1.4115 0.08712 0.08206 -0.0471 0.0284 1.0000
16.500 1.4033 0.09251 0.08760 -0.0495 0.0279 1.0000
16.750 1.3944 0.09830 0.09360 -0.0523 0.0275 1.0000
17.000 1.3846 0.10441 0.09990 -0.0554 0.0270 1.0000
17.250 1.3738 0.11082 0.10650 -0.0588 0.0265 1.0000
17.500 1.3623 0.11755 0.11341 -0.0626 0.0261 1.0000
17.750 1.3504 0.12454 0.12057 -0.0667 0.0256 1.0000
18.000 1.3377 0.13185 0.12804 -0.0711 0.0252 1.0000
18.250 1.3244 0.13943 0.13578 -0.0758 0.0249 1.0000
18.500 1.3104 0.14743 0.14392 -0.0809 0.0245 1.0000
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Polar data table (+)
Polar graphs
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