SG6040 (sg6040-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: SG6040 (sg6040-il) Reynolds number: 500,000 Max Cl/Cd: 96.59 at α=6.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-sg6040-il-500000.txt Download as CSV file: xf-sg6040-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: SG6040
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
------ -------- --------- --------- -------- -------- --------
-16.000 -0.6529 0.09831 0.09528 -0.0654 1.0000 0.0175
-15.750 -0.6777 0.08939 0.08620 -0.0711 1.0000 0.0174
-15.500 -0.7019 0.08158 0.07828 -0.0752 1.0000 0.0173
-15.250 -0.7261 0.07418 0.07074 -0.0794 1.0000 0.0172
-15.000 -0.7472 0.06794 0.06434 -0.0826 1.0000 0.0171
-14.750 -0.7695 0.06224 0.05848 -0.0854 1.0000 0.0171
-14.500 -0.7844 0.05789 0.05400 -0.0866 1.0000 0.0170
-14.250 -0.8031 0.05357 0.04951 -0.0878 1.0000 0.0171
-14.000 -0.8170 0.05006 0.04586 -0.0880 1.0000 0.0171
-13.750 -0.8291 0.04692 0.04258 -0.0876 1.0000 0.0170
-13.500 -0.8400 0.04417 0.03970 -0.0867 1.0000 0.0170
-13.250 -0.8512 0.04172 0.03710 -0.0853 1.0000 0.0171
-13.000 -0.8596 0.03964 0.03490 -0.0834 1.0000 0.0170
-12.750 -0.8699 0.03784 0.03299 -0.0809 1.0000 0.0171
-12.500 -0.8821 0.03637 0.03143 -0.0775 1.0000 0.0171
-12.250 -0.8933 0.03507 0.03004 -0.0740 0.9998 0.0171
-12.000 -0.8732 0.03296 0.02771 -0.0768 0.9965 0.0173
-11.750 -0.8502 0.03116 0.02572 -0.0794 0.9933 0.0174
-11.500 -0.8284 0.02931 0.02373 -0.0809 0.9892 0.0175
-11.250 -0.8026 0.02734 0.02168 -0.0824 0.9864 0.0178
-11.000 -0.7742 0.02585 0.02015 -0.0846 0.9840 0.0181
-10.750 -0.7507 0.02460 0.01885 -0.0856 0.9788 0.0184
-10.500 -0.7236 0.02347 0.01766 -0.0871 0.9745 0.0187
-10.250 -0.6926 0.02238 0.01651 -0.0892 0.9719 0.0192
-10.000 -0.6682 0.02138 0.01545 -0.0898 0.9660 0.0197
-9.750 -0.6393 0.02040 0.01441 -0.0912 0.9617 0.0201
-9.500 -0.6067 0.01953 0.01346 -0.0931 0.9593 0.0207
-9.250 -0.5747 0.01833 0.01221 -0.0953 0.9573 0.0212
-9.000 -0.5557 0.01740 0.01126 -0.0947 0.9484 0.0218
-8.750 -0.5247 0.01655 0.01038 -0.0962 0.9446 0.0224
-8.500 -0.4989 0.01589 0.00968 -0.0965 0.9379 0.0233
-8.250 -0.4708 0.01525 0.00897 -0.0972 0.9315 0.0244
-8.000 -0.4428 0.01450 0.00818 -0.0980 0.9255 0.0256
-7.750 -0.4185 0.01395 0.00760 -0.0977 0.9168 0.0274
-7.500 -0.3910 0.01336 0.00696 -0.0982 0.9100 0.0306
-7.250 -0.3691 0.01280 0.00641 -0.0974 0.9006 0.0374
-7.000 -0.3465 0.01208 0.00587 -0.0970 0.8926 0.0664
-6.750 -0.3222 0.01178 0.00560 -0.0966 0.8839 0.0836
-6.500 -0.2956 0.01150 0.00531 -0.0966 0.8768 0.0952
-6.250 -0.2716 0.01124 0.00506 -0.0961 0.8682 0.1055
-6.000 -0.2446 0.01100 0.00479 -0.0961 0.8614 0.1163
-5.750 -0.2206 0.01076 0.00457 -0.0955 0.8531 0.1284
-5.500 -0.1945 0.01047 0.00430 -0.0954 0.8461 0.1461
-5.250 -0.1704 0.01017 0.00408 -0.0950 0.8384 0.1709
-5.000 -0.1460 0.00976 0.00380 -0.0947 0.8311 0.2094
-4.750 -0.1224 0.00927 0.00353 -0.0943 0.8239 0.2691
-4.500 -0.1000 0.00865 0.00324 -0.0938 0.8162 0.3534
-4.250 -0.0760 0.00814 0.00303 -0.0935 0.8095 0.4438
-4.000 -0.0507 0.00794 0.00300 -0.0930 0.8017 0.5000
-3.750 -0.0228 0.00793 0.00297 -0.0930 0.7949 0.5310
-3.500 0.0046 0.00794 0.00296 -0.0928 0.7874 0.5507
-3.250 0.0325 0.00796 0.00293 -0.0927 0.7802 0.5643
-3.000 0.0606 0.00799 0.00291 -0.0927 0.7732 0.5757
-2.750 0.0883 0.00803 0.00289 -0.0925 0.7655 0.5865
-2.500 0.1166 0.00807 0.00288 -0.0925 0.7588 0.5948
-2.250 0.1441 0.00809 0.00287 -0.0924 0.7508 0.6027
-2.000 0.1723 0.00813 0.00284 -0.0924 0.7438 0.6099
-1.750 0.1998 0.00816 0.00287 -0.0922 0.7360 0.6173
-1.500 0.2277 0.00822 0.00286 -0.0921 0.7286 0.6257
-1.250 0.2551 0.00829 0.00293 -0.0919 0.7209 0.6343
-1.000 0.2828 0.00836 0.00293 -0.0918 0.7130 0.6422
-0.750 0.3102 0.00839 0.00298 -0.0916 0.7056 0.6485
-0.500 0.3377 0.00845 0.00301 -0.0915 0.6974 0.6551
-0.250 0.3654 0.00850 0.00300 -0.0914 0.6898 0.6604
0.000 0.3925 0.00852 0.00302 -0.0912 0.6815 0.6648
0.250 0.4201 0.00857 0.00303 -0.0911 0.6737 0.6689
0.500 0.4475 0.00860 0.00304 -0.0910 0.6651 0.6728
0.750 0.4753 0.00868 0.00304 -0.0910 0.6573 0.6763
1.000 0.5022 0.00867 0.00305 -0.0908 0.6487 0.6797
1.250 0.5294 0.00873 0.00308 -0.0907 0.6411 0.6831
1.500 0.5565 0.00876 0.00312 -0.0905 0.6326 0.6867
1.750 0.5837 0.00885 0.00315 -0.0904 0.6248 0.6904
2.000 0.6109 0.00890 0.00319 -0.0903 0.6162 0.6938
2.250 0.6376 0.00896 0.00323 -0.0901 0.6086 0.6973
2.500 0.6642 0.00900 0.00330 -0.0899 0.6000 0.7007
2.750 0.6908 0.00911 0.00336 -0.0897 0.5921 0.7044
3.000 0.7176 0.00916 0.00344 -0.0895 0.5836 0.7084
3.500 0.7699 0.00932 0.00360 -0.0889 0.5663 0.7159
3.750 0.7954 0.00943 0.00370 -0.0885 0.5570 0.7199
4.000 0.8207 0.00952 0.00379 -0.0880 0.5460 0.7245
4.250 0.8460 0.00963 0.00389 -0.0876 0.5353 0.7291
4.500 0.8702 0.00974 0.00399 -0.0869 0.5249 0.7334
4.750 0.8948 0.00983 0.00412 -0.0863 0.5135 0.7381
5.000 0.9190 0.00997 0.00424 -0.0857 0.5019 0.7434
5.250 0.9425 0.01012 0.00438 -0.0849 0.4908 0.7488
5.500 0.9663 0.01024 0.00454 -0.0842 0.4799 0.7544
5.750 0.9900 0.01039 0.00470 -0.0835 0.4691 0.7607
6.000 1.0122 0.01056 0.00487 -0.0824 0.4568 0.7667
6.500 1.0548 0.01094 0.00526 -0.0801 0.4286 0.7812
6.750 1.0751 0.01113 0.00547 -0.0788 0.4141 0.7893
7.000 1.0951 0.01136 0.00570 -0.0774 0.3996 0.7985
7.250 1.1124 0.01157 0.00594 -0.0755 0.3844 0.8083
7.500 1.1285 0.01183 0.00620 -0.0733 0.3683 0.8194
7.750 1.1436 0.01213 0.00650 -0.0711 0.3507 0.8326
8.000 1.1565 0.01250 0.00686 -0.0684 0.3312 0.8486
8.250 1.1679 0.01287 0.00724 -0.0655 0.3106 0.8693
8.500 1.1756 0.01323 0.00763 -0.0619 0.2888 0.9054
8.750 1.1897 0.01376 0.00812 -0.0600 0.2599 1.0000
9.000 1.1995 0.01456 0.00874 -0.0575 0.2301 1.0000
9.250 1.2077 0.01544 0.00946 -0.0548 0.2024 1.0000
9.500 1.2163 0.01633 0.01022 -0.0523 0.1784 1.0000
9.750 1.2244 0.01727 0.01104 -0.0499 0.1580 1.0000
10.000 1.2335 0.01819 0.01188 -0.0476 0.1403 1.0000
10.250 1.2423 0.01916 0.01277 -0.0455 0.1250 1.0000
10.500 1.2509 0.02017 0.01373 -0.0434 0.1116 1.0000
10.750 1.2590 0.02125 0.01475 -0.0414 0.1001 1.0000
11.000 1.2666 0.02240 0.01586 -0.0394 0.0904 1.0000
11.250 1.2747 0.02358 0.01702 -0.0376 0.0822 1.0000
11.500 1.2833 0.02475 0.01820 -0.0360 0.0755 1.0000
11.750 1.2885 0.02620 0.01962 -0.0342 0.0695 1.0000
12.000 1.2982 0.02739 0.02085 -0.0329 0.0650 1.0000
12.250 1.3032 0.02896 0.02241 -0.0313 0.0607 1.0000
12.500 1.3108 0.03039 0.02389 -0.0301 0.0573 1.0000
12.750 1.3177 0.03193 0.02546 -0.0289 0.0543 1.0000
13.000 1.3198 0.03390 0.02744 -0.0275 0.0515 1.0000
13.250 1.3263 0.03557 0.02919 -0.0266 0.0495 1.0000
13.500 1.3331 0.03728 0.03096 -0.0257 0.0475 1.0000
13.750 1.3372 0.03928 0.03300 -0.0249 0.0457 1.0000
14.000 1.3354 0.04190 0.03565 -0.0240 0.0438 1.0000
14.250 1.3402 0.04398 0.03781 -0.0234 0.0426 1.0000
14.500 1.3461 0.04602 0.03993 -0.0230 0.0412 1.0000
14.750 1.3511 0.04819 0.04217 -0.0227 0.0398 1.0000
15.000 1.3530 0.05075 0.04476 -0.0225 0.0386 1.0000
15.250 1.3498 0.05393 0.04799 -0.0223 0.0374 1.0000
15.500 1.3507 0.05674 0.05088 -0.0223 0.0365 1.0000
15.750 1.3546 0.05928 0.05353 -0.0224 0.0356 1.0000
16.000 1.3575 0.06200 0.05633 -0.0226 0.0347 1.0000
16.250 1.3599 0.06483 0.05923 -0.0229 0.0339 1.0000
16.500 1.3617 0.06779 0.06226 -0.0233 0.0332 1.0000
16.750 1.3613 0.07107 0.06559 -0.0239 0.0325 1.0000
17.000 1.3577 0.07474 0.06930 -0.0245 0.0316 1.0000
17.250 1.3574 0.07806 0.07270 -0.0251 0.0310 1.0000
17.500 1.3601 0.08114 0.07588 -0.0258 0.0305 1.0000
17.750 1.3618 0.08440 0.07925 -0.0267 0.0299 1.0000
18.000 1.3632 0.08769 0.08263 -0.0277 0.0293 1.0000
18.250 1.3644 0.09109 0.08611 -0.0288 0.0287 1.0000
18.500 1.3648 0.09461 0.08970 -0.0300 0.0281 1.0000
18.750 1.3656 0.09809 0.09324 -0.0312 0.0277 1.0000
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