SD7034 (sd7034-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: SD7034 (sd7034-il) Reynolds number: 1,000,000 Max Cl/Cd: 128.44 at α=5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-sd7034-il-1000000.txt Download as CSV file: xf-sd7034-il-1000000.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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-10.500 -0.2592 0.10071 0.09922 -0.0294 0.9672 0.0140
-10.250 -0.6266 0.03512 0.03310 -0.0795 0.9649 0.0089
-10.000 -0.6350 0.02864 0.02604 -0.0822 0.9339 0.0090
-9.750 -0.6267 0.02553 0.02255 -0.0822 0.9189 0.0090
-9.500 -0.6109 0.02345 0.02017 -0.0819 0.9081 0.0091
-9.000 -0.5784 0.01846 0.01445 -0.0814 0.8887 0.0097
-8.750 -0.5547 0.01768 0.01356 -0.0811 0.8810 0.0099
-8.500 -0.5292 0.01715 0.01295 -0.0809 0.8731 0.0102
-8.250 -0.5044 0.01645 0.01211 -0.0806 0.8659 0.0106
-8.000 -0.4788 0.01569 0.01121 -0.0805 0.8582 0.0110
-7.750 -0.4535 0.01497 0.01032 -0.0802 0.8512 0.0113
-7.500 -0.4271 0.01431 0.00953 -0.0800 0.8438 0.0117
-7.250 -0.4004 0.01388 0.00895 -0.0798 0.8368 0.0119
-7.000 -0.3756 0.01261 0.00753 -0.0796 0.8297 0.0126
-6.750 -0.3486 0.01219 0.00705 -0.0795 0.8225 0.0131
-6.500 -0.3211 0.01182 0.00661 -0.0794 0.8156 0.0137
-6.250 -0.2937 0.01145 0.00614 -0.0793 0.8083 0.0144
-6.000 -0.2658 0.01119 0.00579 -0.0791 0.8015 0.0150
-5.750 -0.2390 0.01049 0.00502 -0.0790 0.7940 0.0161
-5.500 -0.2113 0.01026 0.00473 -0.0789 0.7871 0.0171
-5.250 -0.1831 0.01005 0.00447 -0.0789 0.7796 0.0183
-5.000 -0.1556 0.00961 0.00395 -0.0788 0.7726 0.0197
-4.750 -0.1274 0.00935 0.00367 -0.0787 0.7651 0.0212
-4.500 -0.0993 0.00916 0.00341 -0.0786 0.7580 0.0226
-4.250 -0.0712 0.00881 0.00302 -0.0786 0.7506 0.0245
-4.000 -0.0430 0.00864 0.00281 -0.0786 0.7432 0.0267
-3.750 -0.0146 0.00844 0.00256 -0.0786 0.7358 0.0289
-3.500 0.0136 0.00823 0.00233 -0.0785 0.7281 0.0323
-3.250 0.0421 0.00804 0.00213 -0.0785 0.7205 0.0368
-3.000 0.0705 0.00789 0.00195 -0.0785 0.7125 0.0435
-2.750 0.0990 0.00773 0.00182 -0.0785 0.7046 0.0538
-2.500 0.1273 0.00763 0.00171 -0.0785 0.6963 0.0629
-2.250 0.1559 0.00751 0.00160 -0.0785 0.6880 0.0731
-2.000 0.1842 0.00741 0.00150 -0.0785 0.6795 0.0853
-1.750 0.2128 0.00729 0.00141 -0.0785 0.6707 0.1010
-1.500 0.2412 0.00718 0.00133 -0.0786 0.6620 0.1245
-1.250 0.2695 0.00703 0.00127 -0.0786 0.6528 0.1598
-1.000 0.2977 0.00685 0.00122 -0.0787 0.6440 0.2139
-0.750 0.3257 0.00662 0.00118 -0.0788 0.6347 0.2937
-0.500 0.3538 0.00639 0.00117 -0.0789 0.6253 0.3750
-0.250 0.3817 0.00622 0.00117 -0.0789 0.6159 0.4534
0.000 0.4095 0.00605 0.00118 -0.0789 0.6059 0.5364
0.250 0.4371 0.00587 0.00121 -0.0789 0.5961 0.6231
0.500 0.4642 0.00573 0.00125 -0.0786 0.5858 0.7053
0.750 0.4900 0.00552 0.00130 -0.0780 0.5752 0.8040
1.000 0.5115 0.00525 0.00134 -0.0762 0.5651 0.9379
1.250 0.5504 0.00529 0.00133 -0.0785 0.5536 1.0000
1.500 0.5784 0.00539 0.00136 -0.0784 0.5421 1.0000
1.750 0.6065 0.00548 0.00139 -0.0784 0.5307 1.0000
2.000 0.6346 0.00559 0.00144 -0.0784 0.5193 1.0000
2.250 0.6625 0.00571 0.00149 -0.0783 0.5075 1.0000
2.500 0.6903 0.00585 0.00155 -0.0783 0.4952 1.0000
2.750 0.7182 0.00597 0.00162 -0.0783 0.4826 1.0000
3.000 0.7460 0.00610 0.00170 -0.0782 0.4699 1.0000
3.250 0.7737 0.00624 0.00178 -0.0782 0.4570 1.0000
3.500 0.8013 0.00640 0.00187 -0.0781 0.4437 1.0000
3.750 0.8288 0.00656 0.00198 -0.0781 0.4305 1.0000
4.000 0.8562 0.00673 0.00209 -0.0780 0.4167 1.0000
4.250 0.8834 0.00692 0.00222 -0.0779 0.4028 1.0000
4.500 0.9105 0.00711 0.00235 -0.0778 0.3885 1.0000
5.000 0.9646 0.00751 0.00264 -0.0776 0.3600 1.0000
5.250 0.9914 0.00772 0.00280 -0.0775 0.3457 1.0000
5.500 1.0180 0.00795 0.00298 -0.0774 0.3311 1.0000
5.750 1.0444 0.00820 0.00316 -0.0772 0.3163 1.0000
6.000 1.0706 0.00846 0.00336 -0.0770 0.3010 1.0000
6.250 1.0966 0.00873 0.00358 -0.0768 0.2857 1.0000
6.500 1.1224 0.00901 0.00380 -0.0766 0.2710 1.0000
6.750 1.1481 0.00930 0.00403 -0.0763 0.2564 1.0000
7.000 1.1736 0.00960 0.00428 -0.0760 0.2426 1.0000
7.250 1.1989 0.00990 0.00453 -0.0757 0.2292 1.0000
7.500 1.2240 0.01021 0.00480 -0.0754 0.2163 1.0000
7.750 1.2487 0.01055 0.00510 -0.0751 0.2028 1.0000
8.000 1.2730 0.01091 0.00540 -0.0747 0.1896 1.0000
8.250 1.2969 0.01129 0.00573 -0.0742 0.1760 1.0000
8.500 1.3204 0.01170 0.00608 -0.0737 0.1624 1.0000
8.750 1.3433 0.01214 0.00647 -0.0731 0.1482 1.0000
9.000 1.3656 0.01261 0.00687 -0.0724 0.1342 1.0000
9.250 1.3872 0.01312 0.00731 -0.0717 0.1202 1.0000
9.500 1.4079 0.01367 0.00779 -0.0708 0.1062 1.0000
9.750 1.4279 0.01424 0.00830 -0.0698 0.0933 1.0000
10.000 1.4475 0.01482 0.00883 -0.0688 0.0822 1.0000
10.250 1.4662 0.01541 0.00938 -0.0677 0.0722 1.0000
10.500 1.4837 0.01605 0.00998 -0.0663 0.0632 1.0000
10.750 1.4996 0.01674 0.01063 -0.0648 0.0549 1.0000
11.000 1.5156 0.01733 0.01122 -0.0633 0.0499 1.0000
11.250 1.5270 0.01798 0.01187 -0.0609 0.0450 1.0000
11.500 1.5384 0.01862 0.01254 -0.0587 0.0415 1.0000
11.750 1.5470 0.01946 0.01337 -0.0563 0.0373 1.0000
12.000 1.5590 0.02017 0.01413 -0.0544 0.0349 1.0000
12.250 1.5676 0.02113 0.01510 -0.0524 0.0321 1.0000
12.500 1.5772 0.02209 0.01610 -0.0506 0.0296 1.0000
12.750 1.5871 0.02307 0.01713 -0.0490 0.0277 1.0000
13.000 1.5935 0.02436 0.01844 -0.0472 0.0253 1.0000
13.250 1.6019 0.02557 0.01970 -0.0457 0.0238 1.0000
13.500 1.6105 0.02681 0.02100 -0.0444 0.0223 1.0000
13.750 1.6155 0.02840 0.02262 -0.0430 0.0206 1.0000
14.000 1.6194 0.03017 0.02445 -0.0417 0.0194 1.0000
14.250 1.6270 0.03168 0.02603 -0.0408 0.0185 1.0000
14.500 1.6321 0.03346 0.02787 -0.0399 0.0175 1.0000
14.750 1.6339 0.03564 0.03010 -0.0390 0.0164 1.0000
15.000 1.6317 0.03831 0.03285 -0.0383 0.0155 1.0000
15.250 1.6361 0.04040 0.03503 -0.0378 0.0151 1.0000
15.500 1.6396 0.04265 0.03736 -0.0375 0.0144 1.0000
15.750 1.6397 0.04533 0.04013 -0.0373 0.0138 1.0000
16.000 1.6380 0.04837 0.04324 -0.0374 0.0132 1.0000
16.250 1.6332 0.05192 0.04688 -0.0376 0.0127 1.0000
16.500 1.6232 0.05631 0.05138 -0.0383 0.0122 1.0000
16.750 1.6228 0.05959 0.05476 -0.0389 0.0119 1.0000
17.000 1.6205 0.06322 0.05849 -0.0398 0.0116 1.0000
17.250 1.6153 0.06737 0.06275 -0.0409 0.0113 1.0000
17.500 1.6107 0.07156 0.06704 -0.0421 0.0110 1.0000
17.750 1.6023 0.07645 0.07203 -0.0438 0.0107 1.0000
18.000 1.5934 0.08153 0.07722 -0.0456 0.0105 1.0000
18.250 1.5827 0.08706 0.08286 -0.0478 0.0102 1.0000
18.500 1.5700 0.09311 0.08901 -0.0503 0.0100 1.0000
18.750 1.5539 0.09982 0.09584 -0.0533 0.0098 1.0000
19.000 1.5352 0.10724 0.10340 -0.0568 0.0096 1.0000
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Polar data table (+)
Polar graphs
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