NREL's S807 Airfoil (s807-nr) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: NREL's S807 Airfoil (s807-nr) Reynolds number: 1,000,000 Max Cl/Cd: 101.66 at α=8.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-s807-nr-1000000-n5.txt Download as CSV file: xf-s807-nr-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NREL's S807 Airfoil
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
------ -------- --------- --------- -------- -------- --------
-19.750 -1.0601 0.10385 0.09991 -0.0386 1.0000 0.0095
-19.500 -1.0636 0.10028 0.09628 -0.0396 1.0000 0.0096
-19.250 -1.0683 0.09665 0.09258 -0.0406 1.0000 0.0096
-19.000 -1.0702 0.09340 0.08927 -0.0414 1.0000 0.0097
-18.750 -1.0704 0.09045 0.08626 -0.0420 1.0000 0.0098
-18.500 -1.0705 0.08756 0.08331 -0.0426 1.0000 0.0099
-18.250 -1.0705 0.08472 0.08042 -0.0431 1.0000 0.0100
-18.000 -1.0708 0.08188 0.07751 -0.0435 1.0000 0.0101
-17.750 -1.0694 0.07929 0.07487 -0.0438 1.0000 0.0102
-17.500 -1.0693 0.07656 0.07208 -0.0441 1.0000 0.0102
-17.250 -1.0692 0.07390 0.06937 -0.0444 1.0000 0.0104
-17.000 -1.0699 0.07115 0.06657 -0.0446 1.0000 0.0105
-16.750 -1.0701 0.06856 0.06393 -0.0447 1.0000 0.0106
-16.500 -1.0696 0.06604 0.06136 -0.0447 1.0000 0.0107
-16.250 -1.0673 0.06381 0.05910 -0.0446 1.0000 0.0109
-16.000 -1.0647 0.06165 0.05691 -0.0445 1.0000 0.0111
-15.750 -1.0622 0.05948 0.05469 -0.0443 1.0000 0.0112
-15.500 -1.0577 0.05760 0.05279 -0.0440 1.0000 0.0113
-15.250 -1.0551 0.05553 0.05067 -0.0436 1.0000 0.0115
-15.000 -1.0506 0.05369 0.04880 -0.0432 1.0000 0.0116
-14.750 -1.0467 0.05184 0.04691 -0.0427 1.0000 0.0117
-14.500 -1.0425 0.05002 0.04506 -0.0422 1.0000 0.0120
-14.250 -1.0357 0.04835 0.04336 -0.0419 0.9999 0.0122
-14.000 -1.0268 0.04654 0.04150 -0.0423 0.9996 0.0123
-13.750 -1.0171 0.04478 0.03970 -0.0427 0.9993 0.0125
-13.500 -1.0063 0.04320 0.03809 -0.0429 0.9989 0.0127
-13.250 -0.9964 0.04154 0.03639 -0.0432 0.9985 0.0129
-13.000 -0.9862 0.03991 0.03473 -0.0435 0.9980 0.0130
-12.750 -0.9787 0.03809 0.03287 -0.0437 0.9973 0.0133
-12.500 -0.9691 0.03632 0.03107 -0.0444 0.9965 0.0135
-12.250 -0.9595 0.03473 0.02945 -0.0446 0.9957 0.0137
-12.000 -0.9491 0.03318 0.02788 -0.0450 0.9949 0.0140
-11.750 -0.9374 0.03172 0.02639 -0.0454 0.9942 0.0143
-11.500 -0.9249 0.03023 0.02488 -0.0461 0.9935 0.0146
-11.250 -0.9135 0.02890 0.02352 -0.0462 0.9926 0.0149
-11.000 -0.9060 0.02754 0.02213 -0.0455 0.9910 0.0152
-10.750 -0.8961 0.02622 0.02077 -0.0452 0.9892 0.0155
-10.500 -0.8794 0.02491 0.01944 -0.0462 0.9871 0.0158
-10.250 -0.8556 0.02357 0.01807 -0.0485 0.9849 0.0161
-10.000 -0.8175 0.02200 0.01648 -0.0538 0.9825 0.0171
-9.750 -0.8080 0.02067 0.01512 -0.0534 0.9782 0.0174
-9.500 -0.7849 0.01927 0.01370 -0.0554 0.9736 0.0181
-9.250 -0.7489 0.01798 0.01239 -0.0595 0.9712 0.0191
-9.000 -0.7105 0.01670 0.01109 -0.0643 0.9697 0.0206
-8.750 -0.6938 0.01552 0.00988 -0.0649 0.9648 0.0220
-8.500 -0.6672 0.01467 0.00902 -0.0663 0.9604 0.0250
-8.250 -0.6335 0.01385 0.00823 -0.0689 0.9578 0.0313
-8.000 -0.5963 0.01300 0.00744 -0.0722 0.9556 0.0439
-7.750 -0.5872 0.01250 0.00696 -0.0692 0.9461 0.0510
-7.500 -0.5560 0.01186 0.00637 -0.0707 0.9410 0.0633
-7.000 -0.5054 0.01055 0.00523 -0.0713 0.9129 0.1037
-6.750 -0.4435 0.00952 0.00413 -0.0796 0.8200 0.1635
-6.500 -0.4272 0.00918 0.00364 -0.0781 0.7331 0.2095
-6.250 -0.4067 0.00852 0.00304 -0.0778 0.6730 0.2764
-6.000 -0.3825 0.00803 0.00262 -0.0779 0.6231 0.3373
-5.750 -0.3564 0.00794 0.00247 -0.0778 0.5784 0.3680
-5.500 -0.3293 0.00797 0.00239 -0.0778 0.5384 0.3842
-5.250 -0.3016 0.00801 0.00233 -0.0778 0.5063 0.3974
-5.000 -0.2734 0.00806 0.00230 -0.0780 0.4812 0.4136
-4.750 -0.2448 0.00811 0.00230 -0.0781 0.4607 0.4247
-4.500 -0.2160 0.00819 0.00228 -0.0782 0.4428 0.4300
-4.250 -0.1872 0.00825 0.00223 -0.0784 0.4271 0.4318
-4.000 -0.1584 0.00827 0.00218 -0.0785 0.4130 0.4337
-3.750 -0.1294 0.00830 0.00214 -0.0787 0.4004 0.4356
-3.500 -0.1005 0.00833 0.00211 -0.0789 0.3890 0.4371
-3.250 -0.0715 0.00837 0.00208 -0.0791 0.3781 0.4386
-3.000 -0.0423 0.00839 0.00206 -0.0793 0.3704 0.4402
-2.750 -0.0132 0.00843 0.00204 -0.0795 0.3623 0.4420
-2.500 0.0160 0.00847 0.00202 -0.0797 0.3560 0.4436
-2.250 0.0452 0.00850 0.00201 -0.0798 0.3495 0.4451
-2.000 0.0742 0.00855 0.00200 -0.0800 0.3431 0.4463
-1.750 0.1035 0.00858 0.00199 -0.0802 0.3383 0.4474
-1.500 0.1327 0.00861 0.00199 -0.0804 0.3325 0.4488
-1.250 0.1617 0.00866 0.00199 -0.0806 0.3266 0.4504
-1.000 0.1909 0.00868 0.00200 -0.0808 0.3223 0.4520
-0.750 0.2201 0.00871 0.00202 -0.0810 0.3181 0.4536
-0.500 0.2492 0.00876 0.00204 -0.0811 0.3138 0.4555
0.000 0.3074 0.00887 0.00210 -0.0815 0.3065 0.4590
0.250 0.3365 0.00891 0.00213 -0.0816 0.3034 0.4605
0.500 0.3655 0.00897 0.00216 -0.0818 0.3000 0.4619
0.750 0.3944 0.00903 0.00220 -0.0819 0.2965 0.4632
1.000 0.4232 0.00911 0.00225 -0.0820 0.2925 0.4645
1.250 0.4523 0.00915 0.00230 -0.0822 0.2901 0.4663
1.500 0.4813 0.00919 0.00235 -0.0823 0.2874 0.4681
1.750 0.5102 0.00925 0.00241 -0.0825 0.2847 0.4698
2.000 0.5390 0.00932 0.00248 -0.0826 0.2820 0.4716
2.250 0.5676 0.00940 0.00255 -0.0827 0.2792 0.4736
2.500 0.5962 0.00950 0.00263 -0.0827 0.2763 0.4756
2.750 0.6249 0.00956 0.00271 -0.0828 0.2746 0.4774
3.000 0.6536 0.00963 0.00279 -0.0829 0.2729 0.4789
3.250 0.6822 0.00971 0.00287 -0.0829 0.2709 0.4802
3.500 0.7108 0.00978 0.00296 -0.0830 0.2684 0.4822
3.750 0.7392 0.00987 0.00305 -0.0831 0.2658 0.4841
4.000 0.7675 0.00996 0.00316 -0.0831 0.2634 0.4861
4.250 0.7956 0.01007 0.00328 -0.0831 0.2610 0.4880
4.500 0.8238 0.01017 0.00340 -0.0831 0.2592 0.4900
4.750 0.8522 0.01026 0.00351 -0.0831 0.2578 0.4920
5.000 0.8804 0.01035 0.00363 -0.0831 0.2560 0.4940
5.250 0.9084 0.01045 0.00375 -0.0831 0.2538 0.4958
5.500 0.9363 0.01056 0.00386 -0.0830 0.2506 0.4977
5.750 0.9639 0.01069 0.00400 -0.0830 0.2463 0.5000
6.000 0.9915 0.01082 0.00415 -0.0829 0.2432 0.5022
6.250 1.0195 0.01091 0.00429 -0.0829 0.2410 0.5044
6.500 1.0472 0.01102 0.00443 -0.0828 0.2378 0.5066
6.750 1.0744 0.01116 0.00457 -0.0826 0.2335 0.5087
7.000 1.1012 0.01135 0.00475 -0.0824 0.2288 0.5107
7.250 1.1287 0.01146 0.00490 -0.0823 0.2260 0.5125
7.500 1.1558 0.01160 0.00506 -0.0821 0.2216 0.5145
7.750 1.1823 0.01178 0.00524 -0.0819 0.2158 0.5174
8.000 1.2090 0.01195 0.00544 -0.0817 0.2096 0.5202
8.250 1.2347 0.01219 0.00566 -0.0814 0.2005 0.5229
8.500 1.2606 0.01240 0.00588 -0.0810 0.1926 0.5254
8.750 1.2855 0.01270 0.00614 -0.0805 0.1827 0.5277
9.000 1.3093 0.01308 0.00646 -0.0799 0.1685 0.5298
9.250 1.3315 0.01357 0.00688 -0.0791 0.1510 0.5321
9.500 1.3530 0.01411 0.00735 -0.0781 0.1348 0.5349
9.750 1.3740 0.01466 0.00784 -0.0771 0.1208 0.5377
10.000 1.3947 0.01520 0.00834 -0.0760 0.1087 0.5408
10.250 1.4152 0.01572 0.00883 -0.0749 0.0984 0.5439
10.500 1.4347 0.01627 0.00935 -0.0736 0.0885 0.5467
10.750 1.4529 0.01688 0.00992 -0.0722 0.0783 0.5495
11.000 1.4698 0.01748 0.01050 -0.0705 0.0695 0.5528
11.250 1.4847 0.01805 0.01106 -0.0685 0.0624 0.5560
11.500 1.4994 0.01861 0.01163 -0.0665 0.0564 0.5593
11.750 1.5130 0.01925 0.01226 -0.0643 0.0511 0.5625
12.000 1.5263 0.01989 0.01291 -0.0621 0.0464 0.5653
12.250 1.5391 0.02057 0.01360 -0.0600 0.0421 0.5692
12.500 1.5506 0.02130 0.01436 -0.0578 0.0385 0.5735
12.750 1.5629 0.02200 0.01510 -0.0557 0.0359 0.5781
13.000 1.5740 0.02277 0.01591 -0.0536 0.0336 0.5819
13.250 1.5837 0.02363 0.01681 -0.0514 0.0316 0.5863
13.500 1.5939 0.02448 0.01773 -0.0494 0.0301 0.5910
13.750 1.6018 0.02549 0.01879 -0.0472 0.0284 0.5956
14.000 1.6075 0.02667 0.02002 -0.0450 0.0269 0.5999
14.250 1.6143 0.02783 0.02127 -0.0432 0.0259 0.6051
14.500 1.6190 0.02922 0.02274 -0.0414 0.0248 0.6111
14.750 1.6208 0.03090 0.02449 -0.0396 0.0238 0.6166
15.000 1.6203 0.03292 0.02660 -0.0382 0.0228 0.6230
15.250 1.6197 0.03515 0.02893 -0.0372 0.0220 0.6297
15.500 1.6175 0.03776 0.03165 -0.0367 0.0214 0.6360
15.750 1.6125 0.04097 0.03498 -0.0367 0.0207 0.6429
16.000 1.6044 0.04488 0.03901 -0.0374 0.0201 0.6494
16.250 1.5919 0.04973 0.04399 -0.0388 0.0194 0.6554
16.500 1.5768 0.05527 0.04968 -0.0408 0.0190 0.6618
16.750 1.5586 0.06143 0.05598 -0.0432 0.0186 0.6674
17.000 1.5394 0.06783 0.06254 -0.0458 0.0184 0.6731
17.250 1.5183 0.07457 0.06943 -0.0485 0.0182 0.6787
17.500 1.4963 0.08155 0.07655 -0.0515 0.0180 0.6842
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