SD7034 (sd7034-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: SD7034 (sd7034-il) Reynolds number: 500,000 Max Cl/Cd: 99.48 at α=5.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-sd7034-il-500000-n5.txt Download as CSV file: xf-sd7034-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: SD7034
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-10.250 -0.6308 0.03579 0.03303 -0.0790 0.9385 0.0081
-10.000 -0.6361 0.02956 0.02622 -0.0816 0.9169 0.0081
-9.750 -0.6265 0.02621 0.02241 -0.0819 0.9039 0.0083
-9.500 -0.6107 0.02393 0.01976 -0.0818 0.8937 0.0084
-9.250 -0.5923 0.02205 0.01758 -0.0816 0.8843 0.0086
-9.000 -0.5708 0.02073 0.01608 -0.0814 0.8759 0.0089
-8.750 -0.5479 0.01974 0.01491 -0.0812 0.8678 0.0091
-8.500 -0.5236 0.01890 0.01391 -0.0810 0.8601 0.0094
-8.250 -0.4993 0.01807 0.01291 -0.0807 0.8524 0.0097
-8.000 -0.4742 0.01723 0.01191 -0.0806 0.8450 0.0101
-7.750 -0.4492 0.01644 0.01093 -0.0803 0.8376 0.0105
-7.500 -0.4234 0.01569 0.01000 -0.0801 0.8304 0.0110
-7.250 -0.3976 0.01500 0.00918 -0.0799 0.8231 0.0115
-7.000 -0.3710 0.01456 0.00866 -0.0798 0.8162 0.0121
-6.750 -0.3441 0.01416 0.00817 -0.0797 0.8088 0.0129
-6.500 -0.3172 0.01370 0.00758 -0.0795 0.8019 0.0137
-6.250 -0.2903 0.01317 0.00693 -0.0793 0.7945 0.0145
-6.000 -0.2634 0.01276 0.00644 -0.0792 0.7876 0.0153
-5.750 -0.2358 0.01239 0.00600 -0.0791 0.7800 0.0164
-5.500 -0.2085 0.01206 0.00555 -0.0789 0.7728 0.0175
-5.250 -0.1809 0.01166 0.00510 -0.0789 0.7653 0.0188
-5.000 -0.1533 0.01141 0.00478 -0.0788 0.7578 0.0204
-4.750 -0.1253 0.01115 0.00444 -0.0787 0.7502 0.0219
-4.500 -0.0978 0.01082 0.00406 -0.0786 0.7426 0.0236
-4.250 -0.0698 0.01059 0.00378 -0.0785 0.7349 0.0256
-4.000 -0.0419 0.01035 0.00348 -0.0784 0.7273 0.0278
-3.750 -0.0138 0.01013 0.00323 -0.0784 0.7195 0.0307
-3.500 0.0142 0.00994 0.00298 -0.0783 0.7117 0.0339
-3.250 0.0424 0.00975 0.00277 -0.0783 0.7039 0.0385
-3.000 0.0705 0.00958 0.00259 -0.0782 0.6958 0.0452
-2.750 0.0987 0.00943 0.00242 -0.0782 0.6876 0.0529
-2.500 0.1269 0.00933 0.00227 -0.0781 0.6794 0.0603
-2.250 0.1552 0.00919 0.00214 -0.0781 0.6706 0.0692
-2.000 0.1833 0.00909 0.00202 -0.0781 0.6621 0.0801
-1.750 0.2116 0.00898 0.00192 -0.0781 0.6527 0.0928
-1.500 0.2397 0.00887 0.00183 -0.0781 0.6436 0.1115
-1.250 0.2677 0.00873 0.00175 -0.0781 0.6340 0.1432
-1.000 0.2957 0.00858 0.00169 -0.0781 0.6244 0.1809
-0.750 0.3237 0.00844 0.00163 -0.0781 0.6147 0.2260
-0.500 0.3515 0.00828 0.00160 -0.0781 0.6045 0.2850
-0.250 0.3794 0.00814 0.00159 -0.0782 0.5946 0.3440
0.000 0.4070 0.00800 0.00159 -0.0782 0.5845 0.4125
0.250 0.4345 0.00783 0.00161 -0.0781 0.5737 0.4911
0.500 0.4618 0.00769 0.00164 -0.0780 0.5633 0.5679
0.750 0.4879 0.00747 0.00170 -0.0776 0.5527 0.6748
1.000 0.5122 0.00724 0.00177 -0.0767 0.5415 0.7858
1.250 0.5339 0.00701 0.00182 -0.0748 0.5306 0.9069
1.500 0.5731 0.00703 0.00181 -0.0771 0.5179 1.0000
1.750 0.6007 0.00716 0.00185 -0.0770 0.5058 1.0000
2.000 0.6282 0.00731 0.00191 -0.0769 0.4937 1.0000
2.250 0.6558 0.00744 0.00198 -0.0768 0.4813 1.0000
2.500 0.6832 0.00758 0.00205 -0.0767 0.4689 1.0000
2.750 0.7106 0.00774 0.00214 -0.0766 0.4566 1.0000
3.000 0.7379 0.00791 0.00224 -0.0765 0.4441 1.0000
3.250 0.7650 0.00809 0.00235 -0.0764 0.4311 1.0000
3.500 0.7920 0.00827 0.00247 -0.0763 0.4181 1.0000
3.750 0.8191 0.00846 0.00260 -0.0761 0.4048 1.0000
4.000 0.8459 0.00865 0.00274 -0.0760 0.3914 1.0000
4.250 0.8727 0.00886 0.00290 -0.0758 0.3780 1.0000
4.500 0.8992 0.00909 0.00307 -0.0756 0.3645 1.0000
4.750 0.9256 0.00932 0.00325 -0.0754 0.3508 1.0000
5.000 0.9519 0.00957 0.00344 -0.0752 0.3372 1.0000
5.250 0.9779 0.00983 0.00365 -0.0750 0.3235 1.0000
5.500 1.0038 0.01010 0.00387 -0.0748 0.3099 1.0000
6.000 1.0550 0.01067 0.00436 -0.0742 0.2832 1.0000
6.250 1.0803 0.01097 0.00462 -0.0739 0.2697 1.0000
6.500 1.1053 0.01129 0.00489 -0.0736 0.2561 1.0000
6.750 1.1299 0.01164 0.00520 -0.0732 0.2416 1.0000
7.000 1.1543 0.01200 0.00551 -0.0727 0.2273 1.0000
7.250 1.1783 0.01238 0.00584 -0.0723 0.2135 1.0000
7.500 1.2020 0.01277 0.00619 -0.0718 0.1999 1.0000
7.750 1.2253 0.01318 0.00657 -0.0713 0.1867 1.0000
8.000 1.2483 0.01361 0.00696 -0.0707 0.1742 1.0000
8.250 1.2708 0.01406 0.00737 -0.0700 0.1621 1.0000
8.500 1.2926 0.01454 0.00782 -0.0693 0.1491 1.0000
8.750 1.3137 0.01506 0.00829 -0.0685 0.1360 1.0000
9.000 1.3340 0.01561 0.00880 -0.0676 0.1233 1.0000
9.250 1.3535 0.01620 0.00935 -0.0666 0.1108 1.0000
9.500 1.3720 0.01683 0.00994 -0.0654 0.0991 1.0000
9.750 1.3897 0.01746 0.01054 -0.0642 0.0883 1.0000
10.000 1.4064 0.01811 0.01117 -0.0628 0.0785 1.0000
10.250 1.4209 0.01879 0.01184 -0.0611 0.0700 1.0000
10.500 1.4325 0.01952 0.01256 -0.0589 0.0628 1.0000
10.750 1.4433 0.02030 0.01334 -0.0567 0.0562 1.0000
11.000 1.4545 0.02109 0.01416 -0.0548 0.0514 1.0000
11.250 1.4645 0.02201 0.01509 -0.0529 0.0468 1.0000
11.500 1.4751 0.02293 0.01605 -0.0511 0.0434 1.0000
11.750 1.4851 0.02394 0.01710 -0.0495 0.0401 1.0000
12.000 1.4932 0.02514 0.01833 -0.0478 0.0369 1.0000
12.250 1.5032 0.02624 0.01951 -0.0465 0.0347 1.0000
12.500 1.5107 0.02758 0.02090 -0.0451 0.0320 1.0000
12.750 1.5173 0.02906 0.02242 -0.0437 0.0300 1.0000
13.000 1.5254 0.03047 0.02392 -0.0426 0.0284 1.0000
13.250 1.5317 0.03210 0.02562 -0.0416 0.0266 1.0000
13.500 1.5358 0.03399 0.02756 -0.0406 0.0250 1.0000
13.750 1.5405 0.03590 0.02956 -0.0398 0.0236 1.0000
14.000 1.5453 0.03787 0.03163 -0.0391 0.0225 1.0000
14.250 1.5483 0.04009 0.03392 -0.0386 0.0214 1.0000
14.500 1.5489 0.04264 0.03654 -0.0382 0.0202 1.0000
14.750 1.5490 0.04534 0.03933 -0.0379 0.0193 1.0000
15.000 1.5501 0.04802 0.04212 -0.0379 0.0186 1.0000
15.250 1.5502 0.05092 0.04513 -0.0380 0.0178 1.0000
15.500 1.5483 0.05417 0.04847 -0.0383 0.0169 1.0000
15.750 1.5453 0.05771 0.05211 -0.0389 0.0163 1.0000
16.000 1.5400 0.06170 0.05619 -0.0397 0.0157 1.0000
16.250 1.5359 0.06563 0.06024 -0.0407 0.0152 1.0000
16.500 1.5324 0.06961 0.06435 -0.0418 0.0147 1.0000
16.750 1.5270 0.07399 0.06885 -0.0431 0.0142 1.0000
17.000 1.5204 0.07864 0.07361 -0.0447 0.0138 1.0000
17.250 1.5131 0.08354 0.07862 -0.0465 0.0132 1.0000
17.500 1.5039 0.08889 0.08409 -0.0486 0.0129 1.0000
17.750 1.4937 0.09455 0.08985 -0.0509 0.0126 1.0000
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