NREL's S807 Airfoil (s807-nr) Xfoil prediction polar at RE=100,000 Ncrit=9
| Details | Polar file |
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Airfoil: NREL's S807 Airfoil (s807-nr) Reynolds number: 100,000 Max Cl/Cd: 33.39 at α=12.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-s807-nr-100000.txt Download as CSV file: xf-s807-nr-100000.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 = 0.100 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-15.750 -0.6142 0.13768 0.13211 -0.0316 1.0000 0.0735
-15.500 -0.5991 0.13732 0.13176 -0.0301 1.0000 0.0743
-15.250 -0.8065 0.09474 0.08858 -0.0559 1.0000 0.0625
-15.000 -0.8290 0.08883 0.08252 -0.0578 1.0000 0.0622
-14.750 -0.8504 0.08345 0.07698 -0.0593 1.0000 0.0619
-14.500 -0.8710 0.07851 0.07186 -0.0604 1.0000 0.0616
-14.250 -0.8900 0.07398 0.06714 -0.0611 1.0000 0.0615
-14.000 -0.9059 0.06993 0.06289 -0.0614 1.0000 0.0614
-13.750 -0.9194 0.06621 0.05896 -0.0612 1.0000 0.0614
-13.500 -0.9299 0.06285 0.05536 -0.0608 1.0000 0.0615
-13.250 -0.9379 0.05978 0.05207 -0.0600 1.0000 0.0617
-13.000 -0.9424 0.05705 0.04910 -0.0590 1.0000 0.0620
-12.750 -0.9453 0.05458 0.04640 -0.0578 1.0000 0.0625
-12.500 -0.9204 0.05226 0.04407 -0.0567 1.0000 0.0645
-12.250 -0.9023 0.05070 0.04250 -0.0555 1.0000 0.0664
-12.000 -0.8883 0.04917 0.04090 -0.0542 1.0000 0.0687
-11.750 -0.8710 0.04772 0.03932 -0.0526 1.0000 0.0709
-11.500 -0.8550 0.04641 0.03781 -0.0510 1.0000 0.0729
-11.250 -0.8146 0.04631 0.03798 -0.0487 1.0000 0.0778
-11.000 -0.7986 0.04545 0.03709 -0.0469 1.0000 0.0824
-10.750 -0.7741 0.04533 0.03715 -0.0444 1.0000 0.0890
-10.500 -0.7586 0.04478 0.03660 -0.0420 1.0000 0.0967
-10.250 -0.7450 0.04447 0.03657 -0.0391 1.0000 0.1088
-10.000 -0.7427 0.04341 0.03578 -0.0363 1.0000 0.1253
-9.750 -0.7524 0.04151 0.03421 -0.0335 1.0000 0.1433
-9.500 -0.7716 0.03901 0.03202 -0.0304 1.0000 0.1643
-9.250 -0.7970 0.03634 0.02964 -0.0268 1.0000 0.1856
-9.000 -0.8271 0.03382 0.02735 -0.0223 1.0000 0.2022
-8.750 -0.8584 0.03077 0.02455 -0.0186 1.0000 0.2238
-8.500 -0.8495 0.03222 0.02725 -0.0145 1.0000 0.3618
-8.250 -0.8515 0.02940 0.02422 -0.0164 1.0000 0.3985
-8.000 -0.8180 0.03266 0.02737 -0.0135 1.0000 0.4198
-7.750 -0.7809 0.03682 0.03143 -0.0098 1.0000 0.4341
-7.500 -0.7396 0.04201 0.03654 -0.0052 1.0000 0.4477
-7.250 -0.6457 0.05155 0.04589 0.0005 1.0000 0.4496
-7.000 -0.5431 0.05750 0.05156 0.0001 1.0000 0.4585
-6.750 -0.5117 0.05845 0.05243 0.0018 1.0000 0.4696
-6.500 -0.5389 0.05702 0.05105 0.0069 1.0000 0.4821
-6.250 -0.4792 0.05862 0.05252 0.0065 1.0000 0.4923
-6.000 -0.4488 0.05889 0.05273 0.0078 1.0000 0.5033
-5.750 -0.5097 0.05664 0.05062 0.0153 1.0000 0.5146
-5.500 -0.3462 0.06276 0.05648 0.0106 1.0000 0.5616
-5.250 -0.3596 0.06092 0.05467 0.0135 1.0000 0.5621
-5.000 -0.3745 0.05910 0.05287 0.0168 1.0000 0.5620
-4.750 -0.4000 0.05735 0.05117 0.0214 1.0000 0.5624
-4.500 -0.3266 0.06052 0.05432 0.0223 1.0000 0.6181
-4.250 -0.2767 0.05867 0.05241 0.0200 1.0000 0.6245
-4.000 -0.2987 0.05835 0.05218 0.0255 1.0000 0.6364
-3.750 -0.2676 0.05711 0.05094 0.0252 1.0000 0.6435
-3.500 -0.2793 0.05664 0.05055 0.0291 0.9988 0.6545
-3.250 -0.2324 0.05577 0.04961 0.0219 0.9844 0.6690
-3.000 -0.1475 0.05292 0.04668 0.0120 0.9760 0.6737
-2.750 -0.1047 0.05160 0.04532 0.0061 0.9572 0.6866
-2.500 -0.0329 0.04880 0.04250 -0.0017 0.9365 0.6914
-2.250 -0.0085 0.04741 0.04112 -0.0029 0.8951 0.7038
-2.000 0.1003 0.04372 0.03721 -0.0179 0.8266 0.7086
-1.750 0.2106 0.04198 0.03446 -0.0365 0.6905 0.7201
-1.500 0.2584 0.04071 0.03269 -0.0405 0.6306 0.7236
-1.000 0.1664 0.03782 0.02962 -0.0313 0.6099 0.6510
-0.750 0.1927 0.03718 0.02874 -0.0315 0.5867 0.6529
-0.500 0.2136 0.03628 0.02768 -0.0319 0.5677 0.6461
-0.250 0.2210 0.03505 0.02633 -0.0321 0.5541 0.6400
0.000 0.2341 0.03411 0.02530 -0.0324 0.5409 0.6389
0.250 0.2499 0.03295 0.02399 -0.0343 0.5300 0.6369
0.500 0.2725 0.03240 0.02333 -0.0349 0.5190 0.6377
0.750 0.2955 0.03208 0.02299 -0.0349 0.5089 0.6397
1.000 0.3205 0.03171 0.02250 -0.0356 0.5005 0.6416
1.250 0.3438 0.03122 0.02200 -0.0366 0.4918 0.6427
1.500 0.3703 0.03079 0.02147 -0.0381 0.4840 0.6441
1.750 0.3965 0.03042 0.02109 -0.0395 0.4765 0.6462
2.000 0.4252 0.03002 0.02063 -0.0418 0.4693 0.6493
2.250 0.4576 0.02977 0.02023 -0.0444 0.4637 0.6519
2.500 0.4803 0.02971 0.02032 -0.0439 0.4576 0.6536
2.750 0.5059 0.02971 0.02035 -0.0440 0.4520 0.6556
3.000 0.5347 0.02979 0.02035 -0.0448 0.4471 0.6579
3.250 0.5600 0.02984 0.02054 -0.0452 0.4415 0.6609
3.500 0.5888 0.02988 0.02061 -0.0465 0.4361 0.6646
3.750 0.6238 0.02991 0.02057 -0.0496 0.4316 0.6683
4.000 0.6489 0.03021 0.02092 -0.0493 0.4279 0.6704
4.250 0.6711 0.03052 0.02144 -0.0488 0.4235 0.6728
4.500 0.6968 0.03080 0.02182 -0.0490 0.4188 0.6756
4.750 0.7260 0.03107 0.02210 -0.0500 0.4146 0.6793
5.000 0.7584 0.03155 0.02254 -0.0519 0.4110 0.6838
5.250 0.7797 0.03210 0.02336 -0.0516 0.4071 0.6870
5.500 0.8008 0.03265 0.02409 -0.0509 0.4029 0.6900
5.750 0.8273 0.03307 0.02458 -0.0511 0.3988 0.6934
6.000 0.8579 0.03358 0.02506 -0.0523 0.3953 0.6973
6.250 0.8823 0.03451 0.02620 -0.0531 0.3913 0.7016
6.500 0.8987 0.03536 0.02732 -0.0519 0.3867 0.7049
6.750 0.9208 0.03599 0.02808 -0.0513 0.3825 0.7089
7.000 0.9509 0.03646 0.02855 -0.0520 0.3787 0.7139
7.250 0.9731 0.03765 0.02990 -0.0525 0.3742 0.7188
7.500 0.9837 0.03887 0.03143 -0.0507 0.3689 0.7220
7.750 1.0076 0.03939 0.03204 -0.0504 0.3642 0.7263
8.000 1.0447 0.03956 0.03211 -0.0518 0.3600 0.7320
8.250 1.0453 0.04168 0.03466 -0.0497 0.3540 0.7366
8.500 1.0604 0.04253 0.03569 -0.0482 0.3484 0.7412
8.750 1.1008 0.04214 0.03521 -0.0495 0.3438 0.7480
9.000 1.0992 0.04452 0.03795 -0.0474 0.3374 0.7530
9.250 1.1115 0.04543 0.03905 -0.0457 0.3312 0.7578
9.500 1.1673 0.04388 0.03727 -0.0483 0.3259 0.7658
9.750 1.1428 0.04738 0.04129 -0.0439 0.3186 0.7703
10.000 1.1804 0.04624 0.04015 -0.0440 0.3121 0.7782
10.250 1.2010 0.04681 0.04081 -0.0435 0.3056 0.7864
10.500 1.1968 0.04837 0.04264 -0.0403 0.2983 0.7927
10.750 1.2689 0.04504 0.03902 -0.0437 0.2915 0.8046
11.000 1.2309 0.04873 0.04323 -0.0377 0.2842 0.8104
11.250 1.3106 0.04426 0.03843 -0.0412 0.2763 0.8252
11.500 1.2788 0.04748 0.04212 -0.0358 0.2692 0.8344
11.750 1.3436 0.04351 0.03791 -0.0376 0.2606 0.8523
12.000 1.3163 0.04582 0.04062 -0.0319 0.2541 0.8658
12.250 1.3585 0.04281 0.03749 -0.0313 0.2455 0.8913
12.500 1.3332 0.04403 0.03904 -0.0249 0.2402 0.9376
12.750 1.3864 0.04152 0.03629 -0.0277 0.2282 1.0000
13.000 1.3619 0.04439 0.03949 -0.0246 0.2204 1.0000
13.250 1.3823 0.04401 0.03903 -0.0245 0.2099 1.0000
13.500 1.4028 0.04347 0.03830 -0.0240 0.1989 1.0000
13.750 1.3766 0.04705 0.04216 -0.0218 0.1916 1.0000
14.000 1.3797 0.04834 0.04336 -0.0211 0.1821 1.0000
14.250 1.3742 0.05070 0.04569 -0.0207 0.1732 1.0000
14.500 1.3557 0.05502 0.05012 -0.0212 0.1661 1.0000
14.750 1.3615 0.05679 0.05168 -0.0211 0.1566 1.0000
15.000 1.3321 0.06329 0.05842 -0.0233 0.1516 1.0000
15.250 1.3401 0.06513 0.06004 -0.0234 0.1426 1.0000
15.500 1.3102 0.07247 0.06763 -0.0266 0.1385 1.0000
15.750 0.8846 0.16162 0.15743 -0.0747 0.1409 1.0000
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