NREL's S807 Airfoil (s807-nr) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: NREL's S807 Airfoil (s807-nr) Reynolds number: 200,000 Max Cl/Cd: 59.37 at α=10.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-s807-nr-200000-n5.txt Download as CSV file: xf-s807-nr-200000-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 = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -0.7814 0.15115 0.14656 -0.0217 1.0000 0.0184
-19.500 -0.8189 0.13863 0.13377 -0.0286 1.0000 0.0183
-19.250 -0.8410 0.13024 0.12517 -0.0330 1.0000 0.0184
-19.000 -0.8588 0.12310 0.11785 -0.0365 1.0000 0.0185
-18.750 -0.8716 0.11718 0.11176 -0.0392 1.0000 0.0186
-18.500 -0.8829 0.11169 0.10608 -0.0416 1.0000 0.0188
-18.250 -0.8925 0.10667 0.10088 -0.0436 1.0000 0.0190
-18.000 -0.8993 0.10228 0.09633 -0.0452 1.0000 0.0191
-17.750 -0.9049 0.09814 0.09201 -0.0465 1.0000 0.0193
-17.500 -0.9071 0.09465 0.08839 -0.0474 1.0000 0.0194
-17.250 -0.9049 0.09207 0.08578 -0.0477 1.0000 0.0197
-17.000 -0.9021 0.08956 0.08323 -0.0480 1.0000 0.0199
-16.750 -0.8996 0.08701 0.08064 -0.0483 1.0000 0.0202
-16.500 -0.8970 0.08449 0.07806 -0.0486 1.0000 0.0204
-16.250 -0.8936 0.08212 0.07564 -0.0487 1.0000 0.0207
-16.000 -0.8907 0.07969 0.07314 -0.0489 1.0000 0.0211
-15.750 -0.8875 0.07731 0.07069 -0.0490 1.0000 0.0215
-15.500 -0.8838 0.07505 0.06835 -0.0491 1.0000 0.0220
-15.250 -0.8791 0.07296 0.06618 -0.0489 1.0000 0.0225
-15.000 -0.8739 0.07096 0.06409 -0.0487 1.0000 0.0229
-14.750 -0.8680 0.06909 0.06213 -0.0483 1.0000 0.0233
-14.500 -0.8626 0.06732 0.06037 -0.0478 1.0000 0.0238
-14.250 -0.8574 0.06548 0.05853 -0.0474 1.0000 0.0242
-14.000 -0.8521 0.06365 0.05668 -0.0470 1.0000 0.0246
-13.750 -0.8471 0.06183 0.05482 -0.0465 1.0000 0.0250
-13.500 -0.8418 0.06007 0.05303 -0.0460 1.0000 0.0255
-13.250 -0.8367 0.05831 0.05123 -0.0454 1.0000 0.0262
-13.000 -0.8316 0.05659 0.04946 -0.0448 1.0000 0.0269
-12.750 -0.8262 0.05491 0.04773 -0.0441 1.0000 0.0276
-12.500 -0.8230 0.05309 0.04591 -0.0434 1.0000 0.0283
-12.250 -0.8204 0.05125 0.04406 -0.0426 1.0000 0.0288
-12.000 -0.8169 0.04952 0.04231 -0.0418 1.0000 0.0297
-11.750 -0.8137 0.04784 0.04059 -0.0409 1.0000 0.0307
-11.500 -0.8110 0.04616 0.03888 -0.0399 1.0000 0.0317
-11.250 -0.8084 0.04458 0.03725 -0.0387 1.0000 0.0326
-11.000 -0.8087 0.04285 0.03552 -0.0374 1.0000 0.0335
-10.750 -0.8092 0.04117 0.03384 -0.0360 1.0000 0.0347
-10.500 -0.8094 0.03958 0.03224 -0.0344 1.0000 0.0361
-10.250 -0.8100 0.03803 0.03066 -0.0327 1.0000 0.0376
-10.000 -0.8123 0.03644 0.02906 -0.0308 1.0000 0.0397
-9.750 -0.8161 0.03486 0.02748 -0.0286 1.0000 0.0416
-9.500 -0.8210 0.03332 0.02594 -0.0262 1.0000 0.0444
-9.250 -0.8294 0.03175 0.02437 -0.0233 1.0000 0.0472
-9.000 -0.8429 0.03019 0.02282 -0.0196 1.0000 0.0499
-8.750 -0.8570 0.02862 0.02123 -0.0158 1.0000 0.0529
-8.500 -0.8607 0.02667 0.01930 -0.0145 1.0000 0.0580
-8.250 -0.8554 0.02464 0.01728 -0.0148 1.0000 0.0666
-8.000 -0.8430 0.02272 0.01539 -0.0161 1.0000 0.0812
-7.750 -0.8070 0.02084 0.01366 -0.0216 0.9955 0.1132
-7.500 -0.7574 0.01827 0.01148 -0.0306 0.9865 0.1869
-7.250 -0.7116 0.01572 0.00964 -0.0386 0.9806 0.3128
-7.000 -0.6764 0.01540 0.00958 -0.0406 0.9751 0.3738
-6.750 -0.6360 0.01541 0.00958 -0.0432 0.9707 0.4039
-6.500 -0.5997 0.01554 0.00967 -0.0448 0.9654 0.4226
-6.250 -0.5645 0.01557 0.00961 -0.0462 0.9594 0.4349
-6.000 -0.5229 0.01580 0.00975 -0.0488 0.9550 0.4488
-5.750 -0.4955 0.01629 0.01031 -0.0478 0.9460 0.4585
-5.500 -0.4569 0.01624 0.01015 -0.0499 0.9400 0.4657
-5.250 -0.4306 0.01615 0.01005 -0.0493 0.9289 0.4681
-5.000 -0.4033 0.01596 0.00983 -0.0490 0.9163 0.4705
-4.750 -0.3757 0.01570 0.00949 -0.0489 0.9009 0.4731
-4.500 -0.3446 0.01535 0.00904 -0.0495 0.8842 0.4759
-4.250 -0.3056 0.01489 0.00844 -0.0517 0.8648 0.4787
-4.000 -0.2498 0.01444 0.00781 -0.0569 0.8341 0.4811
-3.750 -0.1578 0.01423 0.00726 -0.0691 0.7647 0.4829
-3.500 -0.1173 0.01437 0.00701 -0.0714 0.6907 0.4843
-3.250 -0.0905 0.01454 0.00686 -0.0711 0.6339 0.4859
-3.000 -0.0656 0.01469 0.00675 -0.0705 0.5885 0.4878
-2.500 -0.0142 0.01485 0.00645 -0.0698 0.5220 0.4921
-2.250 0.0124 0.01487 0.00626 -0.0697 0.4982 0.4942
-2.000 0.0399 0.01486 0.00606 -0.0699 0.4787 0.4963
-1.750 0.0668 0.01489 0.00598 -0.0697 0.4621 0.4977
-1.500 0.0938 0.01495 0.00595 -0.0695 0.4476 0.4991
-1.250 0.1210 0.01500 0.00595 -0.0694 0.4345 0.5007
-1.000 0.1484 0.01507 0.00594 -0.0693 0.4232 0.5025
-0.750 0.1758 0.01514 0.00592 -0.0692 0.4127 0.5044
-0.500 0.2039 0.01517 0.00589 -0.0693 0.4034 0.5064
-0.250 0.2317 0.01523 0.00585 -0.0694 0.3955 0.5084
0.000 0.2602 0.01526 0.00581 -0.0696 0.3885 0.5105
0.250 0.2888 0.01530 0.00577 -0.0698 0.3817 0.5126
0.500 0.3167 0.01538 0.00577 -0.0699 0.3760 0.5143
0.750 0.3447 0.01543 0.00584 -0.0699 0.3700 0.5159
1.000 0.3723 0.01553 0.00593 -0.0699 0.3643 0.5177
1.250 0.3998 0.01566 0.00601 -0.0698 0.3593 0.5197
1.500 0.4282 0.01573 0.00610 -0.0699 0.3543 0.5219
1.750 0.4565 0.01582 0.00618 -0.0700 0.3497 0.5240
2.000 0.4846 0.01593 0.00625 -0.0701 0.3457 0.5262
2.250 0.5129 0.01608 0.00632 -0.0703 0.3422 0.5285
2.500 0.5418 0.01617 0.00642 -0.0705 0.3385 0.5308
2.750 0.5696 0.01627 0.00657 -0.0705 0.3346 0.5324
3.000 0.5973 0.01640 0.00673 -0.0705 0.3309 0.5343
3.250 0.6248 0.01657 0.00689 -0.0704 0.3274 0.5365
3.500 0.6526 0.01676 0.00707 -0.0705 0.3243 0.5390
3.750 0.6809 0.01690 0.00727 -0.0706 0.3212 0.5416
4.000 0.7091 0.01705 0.00746 -0.0707 0.3181 0.5443
4.250 0.7373 0.01722 0.00763 -0.0708 0.3152 0.5469
4.500 0.7650 0.01740 0.00784 -0.0708 0.3126 0.5490
4.750 0.7924 0.01761 0.00807 -0.0707 0.3100 0.5510
5.000 0.8199 0.01783 0.00834 -0.0707 0.3072 0.5533
5.250 0.8474 0.01800 0.00862 -0.0707 0.3042 0.5558
5.500 0.8749 0.01821 0.00890 -0.0706 0.3015 0.5588
5.750 0.9024 0.01843 0.00917 -0.0706 0.2990 0.5620
6.000 0.9299 0.01866 0.00942 -0.0706 0.2963 0.5652
6.250 0.9567 0.01891 0.00971 -0.0705 0.2937 0.5676
6.500 0.9837 0.01919 0.01005 -0.0704 0.2913 0.5702
6.750 1.0102 0.01941 0.01042 -0.0702 0.2884 0.5730
7.000 1.0364 0.01962 0.01074 -0.0700 0.2850 0.5761
7.250 1.0623 0.01983 0.01101 -0.0697 0.2814 0.5794
7.500 1.0882 0.02006 0.01126 -0.0694 0.2778 0.5828
7.750 1.1135 0.02032 0.01161 -0.0690 0.2744 0.5857
8.000 1.1382 0.02053 0.01200 -0.0685 0.2705 0.5891
8.250 1.1628 0.02074 0.01233 -0.0680 0.2663 0.5929
8.500 1.1870 0.02096 0.01258 -0.0675 0.2622 0.5969
8.750 1.2109 0.02121 0.01290 -0.0669 0.2579 0.6006
9.000 1.2339 0.02141 0.01330 -0.0661 0.2528 0.6038
9.250 1.2564 0.02162 0.01361 -0.0653 0.2478 0.6076
9.500 1.2783 0.02188 0.01391 -0.0644 0.2431 0.6119
9.750 1.3007 0.02212 0.01433 -0.0635 0.2368 0.6167
10.000 1.3209 0.02235 0.01466 -0.0623 0.2306 0.6209
10.250 1.3416 0.02263 0.01509 -0.0613 0.2238 0.6256
10.500 1.3607 0.02292 0.01547 -0.0600 0.2161 0.6308
10.750 1.3795 0.02326 0.01593 -0.0586 0.2079 0.6357
11.000 1.3939 0.02362 0.01636 -0.0566 0.1991 0.6404
11.250 1.4095 0.02407 0.01693 -0.0549 0.1882 0.6460
11.500 1.4227 0.02465 0.01755 -0.0528 0.1760 0.6521
11.750 1.4326 0.02538 0.01833 -0.0505 0.1628 0.6579
12.000 1.4400 0.02633 0.01928 -0.0480 0.1498 0.6647
12.250 1.4449 0.02746 0.02044 -0.0454 0.1378 0.6713
12.500 1.4476 0.02878 0.02180 -0.0428 0.1274 0.6784
12.750 1.4481 0.03032 0.02339 -0.0403 0.1181 0.6859
13.000 1.4490 0.03191 0.02508 -0.0381 0.1101 0.6934
13.250 1.4454 0.03393 0.02718 -0.0359 0.1036 0.7021
13.500 1.4426 0.03605 0.02943 -0.0343 0.0973 0.7111
14.000 1.4275 0.04183 0.03547 -0.0324 0.0878 0.7328
14.250 1.4161 0.04565 0.03945 -0.0326 0.0839 0.7451
14.500 1.4004 0.05041 0.04436 -0.0336 0.0809 0.7583
14.750 1.3883 0.05511 0.04926 -0.0351 0.0779 0.7745
15.000 1.3722 0.06054 0.05489 -0.0369 0.0753 0.7931
15.250 1.3526 0.06651 0.06104 -0.0391 0.0730 0.8162
15.500 1.3308 0.07244 0.06718 -0.0408 0.0713 0.8563
15.750 1.3089 0.07790 0.07282 -0.0421 0.0697 1.0000
16.000 1.2962 0.08352 0.07855 -0.0446 0.0673 1.0000
16.250 1.2830 0.08932 0.08443 -0.0472 0.0649 1.0000
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