NREL's S807 Airfoil (s807-nr) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: NREL's S807 Airfoil (s807-nr) Reynolds number: 1,000,000 Max Cl/Cd: 106.69 at α=9.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-s807-nr-1000000.txt Download as CSV file: xf-s807-nr-1000000.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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.0226 0.10823 0.10454 -0.0382 1.0000 0.0120
-19.500 -1.0255 0.10468 0.10092 -0.0393 1.0000 0.0121
-19.250 -1.0273 0.10134 0.09750 -0.0402 1.0000 0.0122
-19.000 -1.0291 0.09805 0.09414 -0.0411 1.0000 0.0124
-18.750 -1.0300 0.09497 0.09100 -0.0418 1.0000 0.0124
-18.500 -1.0301 0.09191 0.08787 -0.0425 1.0000 0.0126
-18.250 -1.0300 0.08900 0.08490 -0.0431 1.0000 0.0127
-18.000 -1.0292 0.08614 0.08197 -0.0437 1.0000 0.0128
-17.750 -1.0276 0.08340 0.07917 -0.0442 1.0000 0.0129
-17.500 -1.0263 0.08082 0.07653 -0.0445 1.0000 0.0130
-17.250 -1.0300 0.07805 0.07371 -0.0443 1.0000 0.0133
-17.000 -1.0304 0.07539 0.07103 -0.0444 1.0000 0.0136
-16.750 -1.0298 0.07282 0.06843 -0.0446 1.0000 0.0138
-16.500 -1.0277 0.07051 0.06608 -0.0445 1.0000 0.0139
-16.250 -1.0254 0.06820 0.06373 -0.0445 1.0000 0.0140
-16.000 -1.0233 0.06591 0.06140 -0.0445 1.0000 0.0142
-15.750 -1.0193 0.06387 0.05932 -0.0443 1.0000 0.0144
-15.500 -1.0160 0.06176 0.05718 -0.0441 1.0000 0.0147
-15.250 -1.0126 0.05972 0.05510 -0.0438 1.0000 0.0149
-15.000 -1.0084 0.05780 0.05314 -0.0434 1.0000 0.0151
-14.750 -1.0053 0.05578 0.05107 -0.0431 1.0000 0.0152
-14.500 -1.0011 0.05394 0.04919 -0.0426 1.0000 0.0154
-14.250 -0.9958 0.05221 0.04742 -0.0421 1.0000 0.0157
-14.000 -0.9919 0.05037 0.04554 -0.0415 1.0000 0.0158
-13.750 -0.9851 0.04886 0.04399 -0.0409 1.0000 0.0159
-13.500 -0.9848 0.04684 0.04193 -0.0401 1.0000 0.0162
-13.250 -0.9898 0.04442 0.03947 -0.0391 1.0000 0.0166
-13.000 -0.9899 0.04249 0.03751 -0.0382 1.0000 0.0168
-12.750 -0.9896 0.04064 0.03563 -0.0371 1.0000 0.0170
-12.500 -0.9871 0.03906 0.03403 -0.0360 1.0000 0.0174
-12.250 -0.9878 0.03734 0.03227 -0.0346 1.0000 0.0175
-12.000 -0.9866 0.03585 0.03075 -0.0332 1.0000 0.0178
-11.750 -0.9880 0.03422 0.02909 -0.0315 1.0000 0.0181
-11.500 -0.9894 0.03268 0.02751 -0.0297 1.0000 0.0183
-11.250 -0.9916 0.03115 0.02595 -0.0277 1.0000 0.0185
-11.000 -0.9951 0.02965 0.02441 -0.0254 1.0000 0.0187
-10.750 -1.0012 0.02816 0.02288 -0.0227 1.0000 0.0190
-10.500 -1.0127 0.02663 0.02131 -0.0192 1.0000 0.0191
-10.250 -1.0371 0.02498 0.01961 -0.0139 1.0000 0.0191
-10.000 -1.0060 0.02352 0.01810 -0.0179 0.9971 0.0195
-9.500 -0.9133 0.01976 0.01428 -0.0328 0.9865 0.0219
-9.250 -0.8608 0.01848 0.01295 -0.0402 0.9834 0.0231
-9.000 -0.8116 0.01709 0.01153 -0.0472 0.9818 0.0252
-8.750 -0.7904 0.01613 0.01055 -0.0475 0.9765 0.0270
-8.500 -0.7576 0.01528 0.00972 -0.0499 0.9740 0.0312
-8.250 -0.7221 0.01426 0.00880 -0.0531 0.9722 0.0464
-8.000 -0.6851 0.01317 0.00788 -0.0567 0.9707 0.0739
-7.750 -0.6466 0.01212 0.00702 -0.0604 0.9696 0.1113
-7.500 -0.6145 0.01096 0.00613 -0.0628 0.9673 0.1639
-7.250 -0.5899 0.00972 0.00522 -0.0637 0.9629 0.2320
-7.000 -0.5542 0.00826 0.00425 -0.0670 0.9606 0.3380
-6.750 -0.5140 0.00781 0.00395 -0.0698 0.9586 0.3791
-6.500 -0.4727 0.00760 0.00376 -0.0725 0.9570 0.3965
-6.250 -0.4302 0.00743 0.00360 -0.0755 0.9558 0.4082
-6.000 -0.4069 0.00732 0.00345 -0.0744 0.9498 0.4147
-5.750 -0.3725 0.00713 0.00327 -0.0756 0.9450 0.4208
-5.500 -0.3309 0.00696 0.00308 -0.0782 0.9412 0.4277
-5.250 -0.3143 0.00687 0.00294 -0.0755 0.9274 0.4316
-5.000 -0.2796 0.00673 0.00283 -0.0767 0.9088 0.4410
-4.750 -0.2127 0.00686 0.00256 -0.0843 0.8162 0.4501
-4.500 -0.1931 0.00727 0.00258 -0.0824 0.7206 0.4534
-4.250 -0.1705 0.00756 0.00258 -0.0813 0.6514 0.4554
-4.000 -0.1456 0.00777 0.00257 -0.0806 0.5970 0.4571
-3.750 -0.1195 0.00795 0.00254 -0.0802 0.5520 0.4587
-3.500 -0.0923 0.00810 0.00252 -0.0801 0.5156 0.4604
-3.250 -0.0645 0.00821 0.00249 -0.0800 0.4861 0.4618
-3.000 -0.0364 0.00832 0.00246 -0.0800 0.4630 0.4630
-2.750 -0.0079 0.00841 0.00244 -0.0801 0.4437 0.4639
-2.500 0.0205 0.00841 0.00237 -0.0802 0.4271 0.4661
-2.000 0.0778 0.00849 0.00234 -0.0804 0.4009 0.4697
-1.750 0.1066 0.00855 0.00235 -0.0806 0.3902 0.4712
-1.500 0.1353 0.00862 0.00235 -0.0807 0.3799 0.4727
-1.250 0.1643 0.00867 0.00236 -0.0808 0.3717 0.4743
-1.000 0.1931 0.00874 0.00237 -0.0810 0.3635 0.4758
-0.750 0.2221 0.00879 0.00239 -0.0811 0.3569 0.4773
-0.500 0.2512 0.00885 0.00240 -0.0813 0.3508 0.4786
-0.250 0.2799 0.00894 0.00243 -0.0814 0.3444 0.4798
0.000 0.3089 0.00895 0.00244 -0.0815 0.3397 0.4818
0.250 0.3379 0.00897 0.00245 -0.0817 0.3351 0.4840
0.500 0.3666 0.00903 0.00250 -0.0818 0.3302 0.4858
0.750 0.3951 0.00912 0.00256 -0.0819 0.3250 0.4875
1.000 0.4243 0.00916 0.00260 -0.0820 0.3218 0.4892
1.250 0.4532 0.00922 0.00265 -0.0822 0.3179 0.4909
1.500 0.4818 0.00930 0.00271 -0.0822 0.3140 0.4926
1.750 0.5100 0.00942 0.00279 -0.0822 0.3095 0.4942
2.000 0.5389 0.00949 0.00286 -0.0824 0.3071 0.4956
2.250 0.5679 0.00956 0.00292 -0.0825 0.3046 0.4968
2.500 0.5966 0.00957 0.00297 -0.0826 0.3018 0.4995
2.750 0.6251 0.00964 0.00305 -0.0827 0.2988 0.5018
3.000 0.6533 0.00975 0.00315 -0.0827 0.2956 0.5039
3.250 0.6811 0.00991 0.00329 -0.0826 0.2919 0.5059
3.500 0.7099 0.00996 0.00337 -0.0827 0.2902 0.5079
3.750 0.7386 0.01003 0.00346 -0.0828 0.2882 0.5098
4.000 0.7670 0.01012 0.00356 -0.0828 0.2860 0.5115
4.250 0.7952 0.01022 0.00367 -0.0828 0.2837 0.5130
4.500 0.8233 0.01032 0.00377 -0.0828 0.2812 0.5152
4.750 0.8509 0.01045 0.00391 -0.0827 0.2781 0.5178
5.000 0.8784 0.01061 0.00409 -0.0826 0.2754 0.5201
5.250 0.9068 0.01068 0.00421 -0.0827 0.2739 0.5224
5.500 0.9351 0.01074 0.00431 -0.0827 0.2714 0.5248
5.750 0.9633 0.01083 0.00441 -0.0827 0.2684 0.5271
6.000 0.9909 0.01095 0.00454 -0.0826 0.2654 0.5291
6.250 1.0178 0.01114 0.00471 -0.0824 0.2620 0.5307
6.500 1.0451 0.01126 0.00488 -0.0823 0.2591 0.5339
6.750 1.0734 0.01131 0.00498 -0.0823 0.2567 0.5366
7.000 1.1013 0.01138 0.00511 -0.0823 0.2538 0.5392
7.250 1.1286 0.01150 0.00525 -0.0821 0.2506 0.5417
7.500 1.1552 0.01168 0.00542 -0.0819 0.2468 0.5442
7.750 1.1818 0.01185 0.00561 -0.0816 0.2432 0.5465
8.000 1.2097 0.01191 0.00573 -0.0816 0.2399 0.5492
8.250 1.2369 0.01201 0.00587 -0.0815 0.2354 0.5528
8.500 1.2629 0.01219 0.00606 -0.0812 0.2308 0.5560
8.750 1.2895 0.01235 0.00626 -0.0809 0.2272 0.5590
9.000 1.3163 0.01247 0.00643 -0.0807 0.2227 0.5620
9.250 1.3420 0.01267 0.00662 -0.0803 0.2168 0.5646
9.500 1.3678 0.01285 0.00684 -0.0800 0.2112 0.5681
9.750 1.3933 0.01306 0.00706 -0.0796 0.2031 0.5718
10.000 1.4179 0.01332 0.00733 -0.0791 0.1937 0.5755
10.250 1.4410 0.01368 0.00765 -0.0784 0.1804 0.5792
10.500 1.4616 0.01424 0.00810 -0.0773 0.1612 0.5825
10.750 1.4798 0.01494 0.00870 -0.0759 0.1406 0.5870
11.000 1.4973 0.01564 0.00933 -0.0744 0.1234 0.5912
11.250 1.5139 0.01635 0.00997 -0.0727 0.1090 0.5955
11.500 1.5287 0.01702 0.01059 -0.0707 0.0971 0.5994
11.750 1.5423 0.01766 0.01122 -0.0685 0.0870 0.6042
12.000 1.5552 0.01836 0.01190 -0.0662 0.0778 0.6093
12.250 1.5666 0.01911 0.01263 -0.0638 0.0696 0.6145
12.500 1.5791 0.01981 0.01333 -0.0616 0.0637 0.6201
12.750 1.5910 0.02052 0.01408 -0.0594 0.0584 0.6267
13.000 1.6011 0.02135 0.01491 -0.0570 0.0538 0.6332
13.250 1.6121 0.02211 0.01574 -0.0548 0.0501 0.6404
13.500 1.6205 0.02303 0.01670 -0.0524 0.0465 0.6482
13.750 1.6290 0.02398 0.01770 -0.0502 0.0436 0.6563
14.000 1.6367 0.02499 0.01877 -0.0480 0.0411 0.6657
14.250 1.6406 0.02627 0.02011 -0.0456 0.0386 0.6753
14.500 1.6464 0.02749 0.02142 -0.0436 0.0369 0.6868
14.750 1.6503 0.02892 0.02295 -0.0418 0.0352 0.7000
15.000 1.6502 0.03073 0.02486 -0.0399 0.0336 0.7147
15.250 1.6472 0.03295 0.02719 -0.0384 0.0320 0.7311
15.500 1.6480 0.03507 0.02945 -0.0375 0.0311 0.7515
15.750 1.6450 0.03776 0.03231 -0.0370 0.0301 0.7766
16.000 1.6384 0.04111 0.03585 -0.0370 0.0292 0.8131
16.250 1.6219 0.04485 0.03997 -0.0364 0.0285 1.0000
16.500 1.6071 0.05005 0.04529 -0.0380 0.0277 1.0000
16.750 1.5877 0.05624 0.05161 -0.0403 0.0271 1.0000
17.000 1.5690 0.06249 0.05801 -0.0428 0.0267 1.0000
17.250 1.5482 0.06913 0.06479 -0.0454 0.0265 1.0000
17.500 1.5256 0.07609 0.07189 -0.0483 0.0263 1.0000
17.750 1.5041 0.08301 0.07893 -0.0513 0.0259 1.0000
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