NREL's S807 Airfoil (s807-nr) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: NREL's S807 Airfoil (s807-nr) Reynolds number: 500,000 Max Cl/Cd: 84.94 at α=10.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-s807-nr-500000.txt Download as CSV file: xf-s807-nr-500000.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 = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -0.9592 0.11501 0.11095 -0.0410 1.0000 0.0163
-19.500 -0.9655 0.11079 0.10664 -0.0425 1.0000 0.0165
-19.250 -0.9723 0.10654 0.10229 -0.0440 1.0000 0.0166
-19.000 -0.9759 0.10290 0.09859 -0.0451 1.0000 0.0167
-18.750 -0.9785 0.09940 0.09502 -0.0463 1.0000 0.0169
-18.500 -0.9810 0.09594 0.09150 -0.0474 1.0000 0.0172
-18.250 -0.9850 0.09232 0.08779 -0.0484 1.0000 0.0174
-18.000 -0.9863 0.08919 0.08458 -0.0492 1.0000 0.0176
-17.750 -0.9877 0.08606 0.08137 -0.0498 1.0000 0.0178
-17.500 -0.9878 0.08320 0.07842 -0.0503 1.0000 0.0179
-17.250 -0.9878 0.08037 0.07550 -0.0506 1.0000 0.0182
-17.000 -0.9868 0.07773 0.07277 -0.0509 1.0000 0.0184
-16.750 -0.9855 0.07517 0.07011 -0.0510 1.0000 0.0187
-16.500 -0.9826 0.07287 0.06772 -0.0509 1.0000 0.0188
-16.250 -0.9794 0.07061 0.06538 -0.0509 1.0000 0.0190
-16.000 -0.9767 0.06829 0.06296 -0.0510 1.0000 0.0193
-15.750 -0.9732 0.06610 0.06068 -0.0509 1.0000 0.0194
-15.500 -0.9633 0.06525 0.05983 -0.0493 1.0000 0.0199
-15.250 -0.9559 0.06385 0.05843 -0.0484 1.0000 0.0202
-15.000 -0.9500 0.06213 0.05670 -0.0480 1.0000 0.0206
-14.750 -0.9437 0.06049 0.05503 -0.0474 1.0000 0.0209
-14.500 -0.9376 0.05882 0.05333 -0.0470 1.0000 0.0214
-14.250 -0.9315 0.05718 0.05166 -0.0464 1.0000 0.0218
-14.000 -0.9250 0.05560 0.05004 -0.0457 1.0000 0.0221
-13.750 -0.9187 0.05405 0.04845 -0.0450 1.0000 0.0225
-13.500 -0.9119 0.05258 0.04693 -0.0442 1.0000 0.0229
-13.250 -0.9052 0.05109 0.04539 -0.0434 1.0000 0.0232
-13.000 -0.9003 0.04958 0.04385 -0.0424 1.0000 0.0235
-12.750 -0.8988 0.04786 0.04213 -0.0412 1.0000 0.0241
-12.500 -0.8960 0.04619 0.04046 -0.0401 1.0000 0.0244
-12.250 -0.8930 0.04457 0.03882 -0.0391 1.0000 0.0247
-12.000 -0.8901 0.04296 0.03719 -0.0380 1.0000 0.0253
-11.750 -0.8876 0.04139 0.03560 -0.0368 1.0000 0.0259
-11.500 -0.8861 0.03985 0.03404 -0.0354 1.0000 0.0264
-11.250 -0.8844 0.03837 0.03251 -0.0339 1.0000 0.0270
-11.000 -0.8831 0.03693 0.03104 -0.0323 1.0000 0.0274
-10.750 -0.8837 0.03540 0.02948 -0.0306 1.0000 0.0279
-10.500 -0.8928 0.03345 0.02750 -0.0282 1.0000 0.0284
-10.250 -0.8999 0.03172 0.02576 -0.0258 1.0000 0.0288
-10.000 -0.9095 0.03002 0.02403 -0.0229 1.0000 0.0295
-9.750 -0.9210 0.02845 0.02244 -0.0194 1.0000 0.0298
-9.500 -0.9422 0.02689 0.02085 -0.0144 1.0000 0.0300
-9.250 -0.9478 0.02513 0.01905 -0.0124 1.0000 0.0308
-9.000 -0.9425 0.02334 0.01720 -0.0122 1.0000 0.0318
-8.750 -0.9286 0.02158 0.01537 -0.0134 1.0000 0.0331
-8.500 -0.8901 0.01978 0.01356 -0.0193 0.9969 0.0371
-8.250 -0.8454 0.01848 0.01228 -0.0252 0.9933 0.0463
-8.000 -0.8110 0.01664 0.01065 -0.0297 0.9892 0.0771
-7.750 -0.7726 0.01487 0.00921 -0.0347 0.9858 0.1345
-7.500 -0.7323 0.01268 0.00756 -0.0406 0.9836 0.2363
-7.250 -0.6891 0.01105 0.00655 -0.0461 0.9821 0.3669
-7.000 -0.6541 0.01086 0.00641 -0.0477 0.9779 0.3953
-6.750 -0.6156 0.01080 0.00633 -0.0498 0.9740 0.4110
-6.500 -0.5732 0.01078 0.00627 -0.0526 0.9711 0.4218
-6.250 -0.5278 0.01083 0.00624 -0.0561 0.9690 0.4331
-6.000 -0.4981 0.01076 0.00619 -0.0562 0.9628 0.4399
-5.750 -0.4571 0.01076 0.00608 -0.0587 0.9587 0.4472
-5.500 -0.4130 0.01076 0.00612 -0.0616 0.9560 0.4539
-5.250 -0.3821 0.01099 0.00630 -0.0618 0.9487 0.4644
-5.000 -0.3441 0.01114 0.00657 -0.0632 0.9436 0.4713
-4.750 -0.3092 0.01101 0.00641 -0.0644 0.9371 0.4746
-4.500 -0.2754 0.01077 0.00611 -0.0653 0.9277 0.4773
-4.250 -0.2488 0.01052 0.00579 -0.0648 0.9123 0.4793
-4.000 -0.2185 0.01017 0.00538 -0.0650 0.8908 0.4811
-3.750 -0.1298 0.00966 0.00474 -0.0770 0.8506 0.4831
-3.500 -0.0839 0.00995 0.00452 -0.0803 0.7417 0.4849
-3.250 -0.0627 0.01028 0.00449 -0.0788 0.6640 0.4864
-3.000 -0.0400 0.01052 0.00444 -0.0777 0.6050 0.4879
-2.750 -0.0153 0.01070 0.00439 -0.0770 0.5580 0.4895
-2.500 0.0106 0.01085 0.00433 -0.0766 0.5206 0.4912
-2.250 0.0374 0.01098 0.00428 -0.0765 0.4914 0.4931
-2.000 0.0649 0.01109 0.00423 -0.0764 0.4682 0.4950
-1.750 0.0927 0.01119 0.00419 -0.0764 0.4494 0.4964
-1.500 0.1206 0.01117 0.00408 -0.0765 0.4340 0.4980
-1.250 0.1484 0.01118 0.00404 -0.0765 0.4212 0.4996
-1.000 0.1762 0.01125 0.00404 -0.0764 0.4101 0.5011
-0.750 0.2045 0.01130 0.00405 -0.0764 0.4002 0.5026
-0.500 0.2326 0.01138 0.00408 -0.0765 0.3915 0.5043
-0.250 0.2610 0.01144 0.00410 -0.0765 0.3833 0.5062
0.000 0.2890 0.01156 0.00413 -0.0766 0.3762 0.5082
0.250 0.3180 0.01159 0.00415 -0.0767 0.3701 0.5102
0.500 0.3465 0.01168 0.00417 -0.0768 0.3642 0.5120
0.750 0.3748 0.01182 0.00423 -0.0769 0.3587 0.5134
1.000 0.4035 0.01177 0.00421 -0.0771 0.3542 0.5154
1.250 0.4318 0.01181 0.00425 -0.0771 0.3495 0.5171
1.500 0.4597 0.01193 0.00433 -0.0771 0.3448 0.5189
1.750 0.4879 0.01203 0.00444 -0.0771 0.3406 0.5207
2.000 0.5166 0.01209 0.00451 -0.0772 0.3367 0.5227
2.250 0.5450 0.01218 0.00460 -0.0773 0.3329 0.5249
2.500 0.5732 0.01231 0.00470 -0.0773 0.3294 0.5272
2.750 0.6012 0.01255 0.00486 -0.0774 0.3254 0.5293
3.000 0.6300 0.01260 0.00495 -0.0775 0.3230 0.5311
3.250 0.6583 0.01262 0.00502 -0.0776 0.3202 0.5334
3.500 0.6865 0.01271 0.00514 -0.0776 0.3173 0.5354
3.750 0.7145 0.01283 0.00528 -0.0776 0.3142 0.5375
4.000 0.7423 0.01301 0.00544 -0.0776 0.3111 0.5397
4.250 0.7704 0.01325 0.00567 -0.0776 0.3081 0.5421
4.500 0.7987 0.01334 0.00582 -0.0777 0.3060 0.5445
4.750 0.8269 0.01348 0.00597 -0.0777 0.3037 0.5468
5.000 0.8549 0.01358 0.00612 -0.0777 0.3011 0.5493
5.250 0.8826 0.01368 0.00627 -0.0777 0.2985 0.5519
5.500 0.9101 0.01385 0.00646 -0.0776 0.2959 0.5544
5.750 0.9379 0.01416 0.00675 -0.0776 0.2929 0.5569
6.000 0.9655 0.01431 0.00696 -0.0776 0.2905 0.5596
6.250 0.9928 0.01438 0.00710 -0.0774 0.2875 0.5623
6.500 1.0200 0.01449 0.00724 -0.0773 0.2842 0.5647
6.750 1.0469 0.01459 0.00739 -0.0771 0.2812 0.5675
7.000 1.0737 0.01479 0.00760 -0.0769 0.2780 0.5704
7.250 1.1005 0.01504 0.00791 -0.0768 0.2747 0.5735
7.500 1.1268 0.01509 0.00806 -0.0765 0.2716 0.5768
7.750 1.1531 0.01519 0.00821 -0.0762 0.2680 0.5801
8.000 1.1791 0.01532 0.00836 -0.0758 0.2645 0.5830
8.250 1.2046 0.01558 0.00863 -0.0755 0.2603 0.5863
8.500 1.2303 0.01565 0.00882 -0.0751 0.2570 0.5896
8.750 1.2558 0.01570 0.00897 -0.0746 0.2526 0.5931
9.000 1.2805 0.01583 0.00912 -0.0741 0.2479 0.5968
9.250 1.3048 0.01609 0.00938 -0.0735 0.2433 0.6004
9.500 1.3303 0.01612 0.00958 -0.0731 0.2388 0.6045
9.750 1.3546 0.01626 0.00979 -0.0725 0.2337 0.6088
10.000 1.3774 0.01651 0.01005 -0.0717 0.2282 0.6133
10.250 1.4025 0.01663 0.01027 -0.0712 0.2218 0.6176
10.500 1.4245 0.01686 0.01053 -0.0703 0.2146 0.6220
10.750 1.4482 0.01705 0.01083 -0.0696 0.2062 0.6269
11.000 1.4687 0.01736 0.01115 -0.0685 0.1958 0.6322
11.250 1.4869 0.01775 0.01153 -0.0670 0.1824 0.6373
11.500 1.5024 0.01829 0.01206 -0.0651 0.1657 0.6430
11.750 1.5144 0.01909 0.01278 -0.0628 0.1477 0.6493
12.000 1.5235 0.02005 0.01368 -0.0602 0.1315 0.6552
12.250 1.5320 0.02103 0.01465 -0.0576 0.1180 0.6618
12.500 1.5395 0.02208 0.01567 -0.0550 0.1058 0.6689
12.750 1.5465 0.02312 0.01675 -0.0524 0.0955 0.6762
13.000 1.5524 0.02426 0.01790 -0.0498 0.0866 0.6848
13.250 1.5562 0.02552 0.01922 -0.0472 0.0791 0.6936
13.500 1.5589 0.02690 0.02064 -0.0447 0.0728 0.7040
13.750 1.5615 0.02834 0.02218 -0.0424 0.0678 0.7159
14.000 1.5610 0.03007 0.02400 -0.0402 0.0635 0.7293
14.250 1.5580 0.03211 0.02616 -0.0382 0.0600 0.7450
14.500 1.5565 0.03422 0.02843 -0.0368 0.0570 0.7650
14.750 1.5493 0.03706 0.03143 -0.0358 0.0545 0.7904
15.000 1.5357 0.04078 0.03536 -0.0353 0.0523 0.8304
15.250 1.5214 0.04392 0.03882 -0.0341 0.0511 1.0000
15.500 1.5116 0.04839 0.04342 -0.0354 0.0495 1.0000
15.750 1.4962 0.05393 0.04908 -0.0374 0.0482 1.0000
16.000 1.4770 0.06021 0.05549 -0.0399 0.0471 1.0000
16.250 1.4550 0.06699 0.06239 -0.0427 0.0463 1.0000
16.500 1.4309 0.07411 0.06963 -0.0456 0.0454 1.0000
16.750 1.4063 0.08142 0.07705 -0.0487 0.0446 1.0000
17.000 1.3941 0.08702 0.08277 -0.0511 0.0436 1.0000
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