SD7034 (sd7034-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: SD7034 (sd7034-il) Reynolds number: 1,000,000 Max Cl/Cd: 116.34 at α=5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-sd7034-il-1000000-n5.txt Download as CSV file: xf-sd7034-il-1000000-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 = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-12.250 -0.8654 0.03047 0.02779 -0.0812 0.9589 0.0052
-12.000 -0.8563 0.02781 0.02487 -0.0815 0.9352 0.0052
-11.750 -0.8437 0.02583 0.02266 -0.0812 0.9198 0.0053
-11.500 -0.8276 0.02420 0.02084 -0.0809 0.9079 0.0054
-11.250 -0.8097 0.02271 0.01913 -0.0806 0.8974 0.0055
-11.000 -0.7894 0.02145 0.01770 -0.0804 0.8877 0.0056
-10.750 -0.7681 0.02030 0.01637 -0.0801 0.8791 0.0057
-10.500 -0.7456 0.01929 0.01519 -0.0799 0.8706 0.0058
-10.250 -0.7221 0.01841 0.01416 -0.0797 0.8629 0.0060
-10.000 -0.6979 0.01762 0.01323 -0.0795 0.8549 0.0061
-9.750 -0.6732 0.01691 0.01238 -0.0793 0.8477 0.0062
-9.500 -0.6482 0.01618 0.01152 -0.0791 0.8401 0.0063
-9.250 -0.6235 0.01529 0.01048 -0.0790 0.8330 0.0067
-9.000 -0.5977 0.01467 0.00975 -0.0789 0.8256 0.0069
-8.750 -0.5716 0.01412 0.00910 -0.0787 0.8188 0.0071
-8.500 -0.5449 0.01362 0.00852 -0.0786 0.8115 0.0073
-8.250 -0.5183 0.01317 0.00796 -0.0785 0.8045 0.0076
-8.000 -0.4912 0.01273 0.00743 -0.0784 0.7976 0.0079
-7.750 -0.4642 0.01232 0.00692 -0.0783 0.7904 0.0082
-7.500 -0.4368 0.01194 0.00646 -0.0782 0.7836 0.0084
-7.250 -0.4095 0.01153 0.00596 -0.0781 0.7763 0.0089
-7.000 -0.3820 0.01118 0.00555 -0.0781 0.7695 0.0094
-6.750 -0.3543 0.01088 0.00521 -0.0780 0.7621 0.0100
-6.500 -0.3266 0.01062 0.00487 -0.0779 0.7550 0.0106
-6.250 -0.2986 0.01036 0.00454 -0.0779 0.7475 0.0112
-6.000 -0.2708 0.01010 0.00424 -0.0778 0.7402 0.0122
-5.750 -0.2427 0.00989 0.00400 -0.0778 0.7325 0.0133
-5.500 -0.2146 0.00972 0.00375 -0.0777 0.7250 0.0142
-5.250 -0.1864 0.00947 0.00347 -0.0777 0.7173 0.0153
-5.000 -0.1583 0.00929 0.00324 -0.0777 0.7098 0.0164
-4.750 -0.1299 0.00913 0.00303 -0.0777 0.7020 0.0174
-4.500 -0.1017 0.00895 0.00280 -0.0776 0.6943 0.0185
-4.250 -0.0734 0.00877 0.00260 -0.0777 0.6865 0.0201
-4.000 -0.0450 0.00865 0.00242 -0.0776 0.6787 0.0215
-3.750 -0.0166 0.00849 0.00223 -0.0777 0.6706 0.0232
-3.500 0.0118 0.00836 0.00207 -0.0776 0.6624 0.0256
-3.250 0.0402 0.00823 0.00192 -0.0777 0.6537 0.0287
-3.000 0.0687 0.00812 0.00178 -0.0777 0.6454 0.0327
-2.750 0.0971 0.00800 0.00166 -0.0777 0.6361 0.0391
-2.500 0.1255 0.00790 0.00156 -0.0777 0.6271 0.0470
-2.000 0.1825 0.00777 0.00139 -0.0777 0.6079 0.0607
-1.750 0.2109 0.00771 0.00132 -0.0778 0.5984 0.0686
-1.500 0.2393 0.00766 0.00126 -0.0778 0.5879 0.0782
-1.250 0.2678 0.00759 0.00120 -0.0778 0.5781 0.0919
-1.000 0.2961 0.00753 0.00116 -0.0778 0.5681 0.1111
-0.750 0.3244 0.00744 0.00113 -0.0779 0.5576 0.1415
-0.500 0.3527 0.00736 0.00110 -0.0780 0.5473 0.1752
-0.250 0.3809 0.00728 0.00109 -0.0780 0.5368 0.2132
0.000 0.4090 0.00720 0.00109 -0.0781 0.5256 0.2609
0.250 0.4372 0.00712 0.00110 -0.0781 0.5146 0.3057
0.500 0.4652 0.00707 0.00112 -0.0782 0.5030 0.3537
0.750 0.4931 0.00698 0.00116 -0.0782 0.4912 0.4174
1.000 0.5208 0.00692 0.00121 -0.0783 0.4788 0.4824
1.250 0.5484 0.00677 0.00127 -0.0783 0.4671 0.5765
1.500 0.5757 0.00667 0.00134 -0.0782 0.4556 0.6544
1.750 0.6026 0.00659 0.00143 -0.0780 0.4437 0.7306
2.000 0.6265 0.00639 0.00153 -0.0770 0.4322 0.8505
2.250 0.6584 0.00626 0.00158 -0.0776 0.4193 1.0000
2.500 0.6862 0.00640 0.00165 -0.0775 0.4072 1.0000
2.750 0.7139 0.00654 0.00173 -0.0775 0.3953 1.0000
3.000 0.7414 0.00670 0.00182 -0.0775 0.3827 1.0000
3.250 0.7689 0.00687 0.00192 -0.0774 0.3703 1.0000
3.500 0.7963 0.00705 0.00203 -0.0773 0.3567 1.0000
3.750 0.8236 0.00722 0.00215 -0.0772 0.3434 1.0000
4.000 0.8509 0.00741 0.00227 -0.0772 0.3305 1.0000
4.250 0.8780 0.00760 0.00240 -0.0771 0.3176 1.0000
4.500 0.9050 0.00780 0.00255 -0.0770 0.3049 1.0000
4.750 0.9319 0.00802 0.00271 -0.0769 0.2923 1.0000
5.000 0.9586 0.00824 0.00287 -0.0767 0.2800 1.0000
5.250 0.9852 0.00847 0.00305 -0.0766 0.2675 1.0000
5.500 1.0117 0.00870 0.00323 -0.0764 0.2551 1.0000
5.750 1.0381 0.00894 0.00342 -0.0763 0.2432 1.0000
6.000 1.0641 0.00921 0.00363 -0.0760 0.2299 1.0000
6.250 1.0897 0.00951 0.00386 -0.0758 0.2155 1.0000
6.500 1.1153 0.00980 0.00410 -0.0755 0.2028 1.0000
6.750 1.1405 0.01012 0.00436 -0.0752 0.1889 1.0000
7.000 1.1656 0.01044 0.00463 -0.0749 0.1766 1.0000
7.250 1.1903 0.01079 0.00492 -0.0746 0.1640 1.0000
7.500 1.2150 0.01112 0.00520 -0.0742 0.1528 1.0000
7.750 1.2392 0.01149 0.00552 -0.0738 0.1407 1.0000
8.000 1.2629 0.01188 0.00587 -0.0733 0.1282 1.0000
8.250 1.2862 0.01231 0.00623 -0.0727 0.1160 1.0000
8.500 1.3090 0.01275 0.00663 -0.0721 0.1041 1.0000
8.750 1.3313 0.01321 0.00704 -0.0714 0.0930 1.0000
9.000 1.3531 0.01369 0.00746 -0.0707 0.0830 1.0000
9.250 1.3740 0.01422 0.00794 -0.0699 0.0722 1.0000
9.500 1.3942 0.01477 0.00844 -0.0689 0.0627 1.0000
10.000 1.4339 0.01581 0.00945 -0.0669 0.0492 1.0000
10.250 1.4525 0.01636 0.00998 -0.0658 0.0444 1.0000
10.500 1.4705 0.01691 0.01053 -0.0645 0.0397 1.0000
10.750 1.4873 0.01746 0.01109 -0.0631 0.0364 1.0000
11.000 1.5014 0.01799 0.01164 -0.0611 0.0335 1.0000
11.250 1.5127 0.01864 0.01230 -0.0589 0.0307 1.0000
11.500 1.5255 0.01925 0.01295 -0.0569 0.0288 1.0000
11.750 1.5372 0.01996 0.01369 -0.0550 0.0268 1.0000
12.000 1.5476 0.02079 0.01454 -0.0531 0.0248 1.0000
12.250 1.5589 0.02162 0.01541 -0.0514 0.0229 1.0000
12.500 1.5696 0.02253 0.01636 -0.0498 0.0216 1.0000
12.750 1.5783 0.02361 0.01747 -0.0481 0.0198 1.0000
13.000 1.5883 0.02467 0.01858 -0.0467 0.0188 1.0000
13.250 1.5972 0.02586 0.01983 -0.0453 0.0175 1.0000
13.500 1.6044 0.02723 0.02123 -0.0440 0.0162 1.0000
13.750 1.6117 0.02864 0.02270 -0.0427 0.0152 1.0000
14.000 1.6192 0.03010 0.02423 -0.0417 0.0144 1.0000
14.250 1.6245 0.03180 0.02597 -0.0406 0.0133 1.0000
14.500 1.6286 0.03369 0.02791 -0.0397 0.0125 1.0000
14.750 1.6337 0.03555 0.02985 -0.0390 0.0119 1.0000
15.000 1.6380 0.03755 0.03193 -0.0384 0.0113 1.0000
15.250 1.6410 0.03976 0.03421 -0.0379 0.0108 1.0000
15.500 1.6425 0.04220 0.03673 -0.0375 0.0104 1.0000
15.750 1.6427 0.04486 0.03946 -0.0373 0.0099 1.0000
16.000 1.6425 0.04769 0.04237 -0.0373 0.0094 1.0000
16.250 1.6425 0.05061 0.04538 -0.0374 0.0092 1.0000
16.500 1.6419 0.05370 0.04857 -0.0378 0.0089 1.0000
16.750 1.6401 0.05706 0.05201 -0.0383 0.0086 1.0000
17.000 1.6365 0.06076 0.05581 -0.0391 0.0082 1.0000
17.250 1.6322 0.06470 0.05984 -0.0400 0.0081 1.0000
17.500 1.6261 0.06898 0.06422 -0.0412 0.0077 1.0000
17.750 1.6195 0.07351 0.06885 -0.0427 0.0076 1.0000
18.000 1.6101 0.07857 0.07402 -0.0444 0.0072 1.0000
18.250 1.6030 0.08340 0.07896 -0.0462 0.0071 1.0000
18.500 1.5944 0.08860 0.08427 -0.0483 0.0070 1.0000
18.750 1.5848 0.09408 0.08988 -0.0506 0.0069 1.0000
19.000 1.5745 0.09978 0.09569 -0.0530 0.0067 1.0000
19.250 1.5634 0.10572 0.10174 -0.0557 0.0066 1.0000
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