NREL's S835 Airfoil (s835-nr) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: NREL's S835 Airfoil (s835-nr) Reynolds number: 1,000,000 Max Cl/Cd: 70.62 at α=4° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-s835-nr-1000000-n5.txt Download as CSV file: xf-s835-nr-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NREL's S835 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 -1.0132 0.08641 0.08251 -0.0951 0.9884 0.0842
-19.500 -1.0209 0.08262 0.07869 -0.0965 0.9879 0.0861
-19.250 -1.0227 0.07960 0.07563 -0.0977 0.9874 0.0882
-19.000 -1.0256 0.07644 0.07241 -0.0990 0.9869 0.0903
-18.750 -1.0297 0.07317 0.06911 -0.1002 0.9863 0.0922
-18.500 -1.0350 0.06974 0.06564 -0.1015 0.9858 0.0941
-18.250 -1.0368 0.06677 0.06263 -0.1027 0.9853 0.0969
-18.000 -1.0360 0.06404 0.05985 -0.1039 0.9847 0.0984
-17.750 -1.0365 0.06106 0.05684 -0.1053 0.9841 0.1006
-17.500 -1.0390 0.05793 0.05366 -0.1067 0.9836 0.1032
-17.250 -1.0390 0.05513 0.05083 -0.1078 0.9830 0.1060
-17.000 -1.0334 0.05293 0.04858 -0.1089 0.9826 0.1080
-16.750 -1.0338 0.05010 0.04572 -0.1102 0.9821 0.1102
-16.500 -1.0306 0.04768 0.04327 -0.1113 0.9816 0.1129
-16.250 -1.0267 0.04528 0.04083 -0.1125 0.9811 0.1158
-15.750 -1.0142 0.04096 0.03644 -0.1149 0.9803 0.1209
-15.500 -1.0071 0.03878 0.03424 -0.1163 0.9798 0.1239
-15.250 -0.9955 0.03696 0.03239 -0.1178 0.9793 0.1271
-15.000 -0.9849 0.03513 0.03052 -0.1191 0.9789 0.1298
-14.750 -0.9870 0.03339 0.02877 -0.1179 0.9766 0.1323
-14.500 -0.9855 0.03171 0.02706 -0.1171 0.9740 0.1351
-14.250 -0.9747 0.03026 0.02558 -0.1176 0.9723 0.1383
-14.000 -0.9622 0.02875 0.02404 -0.1185 0.9709 0.1412
-13.750 -0.9502 0.02708 0.02236 -0.1198 0.9697 0.1450
-13.500 -0.9330 0.02579 0.02105 -0.1211 0.9687 0.1484
-13.250 -0.9134 0.02463 0.01986 -0.1226 0.9679 0.1514
-13.000 -0.8955 0.02325 0.01847 -0.1244 0.9671 0.1555
-12.750 -0.8742 0.02205 0.01726 -0.1263 0.9665 0.1597
-12.500 -0.8487 0.02112 0.01632 -0.1284 0.9659 0.1630
-12.250 -0.8254 0.02001 0.01519 -0.1305 0.9652 0.1674
-12.000 -0.8363 0.01915 0.01432 -0.1256 0.9590 0.1697
-11.750 -0.8175 0.01830 0.01346 -0.1261 0.9569 0.1737
-11.500 -0.7947 0.01756 0.01269 -0.1272 0.9553 0.1769
-11.250 -0.7729 0.01666 0.01180 -0.1284 0.9537 0.1814
-11.000 -0.7489 0.01590 0.01103 -0.1297 0.9522 0.1855
-10.750 -0.7238 0.01527 0.01038 -0.1309 0.9508 0.1893
-10.500 -0.7294 0.01473 0.00982 -0.1260 0.9436 0.1915
-10.250 -0.7132 0.01403 0.00912 -0.1256 0.9400 0.1954
-10.000 -0.6924 0.01341 0.00849 -0.1258 0.9374 0.1994
-9.750 -0.6802 0.01291 0.00797 -0.1241 0.9331 0.2024
-9.500 -0.6800 0.01246 0.00749 -0.1200 0.9251 0.2044
-9.250 -0.6635 0.01194 0.00694 -0.1192 0.9211 0.2076
-9.000 -0.6592 0.01154 0.00653 -0.1158 0.9126 0.2109
-8.750 -0.6360 0.01120 0.00618 -0.1157 0.9079 0.2146
-8.500 -0.6062 0.01091 0.00586 -0.1167 0.9048 0.2180
-8.250 -0.5864 0.01072 0.00565 -0.1157 0.8982 0.2203
-8.000 -0.5608 0.01043 0.00534 -0.1158 0.8924 0.2240
-7.750 -0.5305 0.01015 0.00505 -0.1169 0.8879 0.2283
-7.500 -0.5063 0.00996 0.00485 -0.1166 0.8810 0.2318
-7.250 -0.4779 0.00979 0.00464 -0.1171 0.8747 0.2346
-7.000 -0.4488 0.00962 0.00443 -0.1177 0.8690 0.2376
-6.750 -0.4237 0.00943 0.00424 -0.1176 0.8618 0.2418
-6.500 -0.3959 0.00927 0.00406 -0.1179 0.8551 0.2457
-6.250 -0.3687 0.00914 0.00391 -0.1181 0.8492 0.2492
-6.000 -0.3421 0.00904 0.00378 -0.1181 0.8423 0.2522
-5.750 -0.3148 0.00890 0.00362 -0.1183 0.8354 0.2562
-5.500 -0.2885 0.00877 0.00349 -0.1183 0.8291 0.2604
-5.250 -0.2618 0.00866 0.00337 -0.1182 0.8224 0.2649
-5.000 -0.2342 0.00859 0.00326 -0.1184 0.8160 0.2682
-4.750 -0.2075 0.00848 0.00315 -0.1183 0.8097 0.2723
-4.500 -0.1809 0.00837 0.00305 -0.1183 0.8027 0.2774
-4.250 -0.1538 0.00830 0.00295 -0.1183 0.7960 0.2820
-4.000 -0.1265 0.00823 0.00288 -0.1183 0.7902 0.2855
-3.750 -0.0997 0.00815 0.00279 -0.1183 0.7832 0.2902
-3.250 -0.0461 0.00801 0.00264 -0.1181 0.7694 0.3005
-3.000 -0.0194 0.00797 0.00258 -0.1179 0.7616 0.3042
-2.750 0.0069 0.00790 0.00251 -0.1177 0.7546 0.3101
-2.500 0.0341 0.00783 0.00245 -0.1177 0.7478 0.3159
-2.250 0.0606 0.00780 0.00241 -0.1175 0.7405 0.3204
-2.000 0.0871 0.00777 0.00237 -0.1172 0.7338 0.3249
-1.750 0.1142 0.00770 0.00232 -0.1172 0.7272 0.3311
-1.500 0.1405 0.00768 0.00229 -0.1169 0.7199 0.3369
-1.250 0.1667 0.00767 0.00227 -0.1165 0.7133 0.3413
-1.000 0.1937 0.00761 0.00224 -0.1164 0.7064 0.3471
-0.750 0.2193 0.00760 0.00222 -0.1160 0.6987 0.3525
-0.500 0.2450 0.00760 0.00221 -0.1155 0.6919 0.3576
-0.250 0.2702 0.00757 0.00219 -0.1150 0.6838 0.3632
0.000 0.2927 0.00757 0.00218 -0.1139 0.6745 0.3696
0.250 0.3175 0.00757 0.00218 -0.1132 0.6650 0.3752
0.750 0.3646 0.00760 0.00220 -0.1114 0.6449 0.3853
1.000 0.3869 0.00766 0.00223 -0.1102 0.6339 0.3909
1.250 0.4122 0.00769 0.00226 -0.1097 0.6234 0.3963
1.500 0.4353 0.00776 0.00231 -0.1087 0.6123 0.4021
1.750 0.4598 0.00781 0.00236 -0.1080 0.6004 0.4090
2.000 0.4830 0.00790 0.00243 -0.1070 0.5886 0.4144
2.250 0.5056 0.00803 0.00252 -0.1059 0.5747 0.4188
2.500 0.5296 0.00812 0.00261 -0.1051 0.5604 0.4250
2.750 0.5525 0.00825 0.00271 -0.1041 0.5458 0.4313
3.000 0.5746 0.00842 0.00283 -0.1030 0.5286 0.4369
3.250 0.5962 0.00860 0.00296 -0.1017 0.5099 0.4427
3.500 0.6171 0.00880 0.00312 -0.1004 0.4894 0.4495
3.750 0.6373 0.00904 0.00329 -0.0989 0.4660 0.4552
4.000 0.6575 0.00931 0.00347 -0.0975 0.4417 0.4604
4.250 0.6771 0.00960 0.00368 -0.0959 0.4156 0.4671
4.500 0.6962 0.00992 0.00390 -0.0943 0.3883 0.4736
4.750 0.7144 0.01028 0.00415 -0.0926 0.3595 0.4783
5.000 0.7320 0.01066 0.00442 -0.0908 0.3314 0.4844
5.250 0.7508 0.01102 0.00469 -0.0892 0.3054 0.4909
5.500 0.7686 0.01143 0.00499 -0.0875 0.2788 0.4964
5.750 0.7868 0.01184 0.00529 -0.0858 0.2547 0.5011
6.000 0.8049 0.01222 0.00561 -0.0842 0.2322 0.5076
6.250 0.8216 0.01268 0.00596 -0.0823 0.2082 0.5136
6.500 0.8383 0.01316 0.00633 -0.0805 0.1854 0.5188
6.750 0.8564 0.01358 0.00669 -0.0789 0.1667 0.5241
7.000 0.8746 0.01399 0.00705 -0.0774 0.1520 0.5302
7.250 0.8925 0.01442 0.00743 -0.0758 0.1387 0.5362
7.750 0.9283 0.01531 0.00823 -0.0727 0.1138 0.5472
8.000 0.9458 0.01577 0.00867 -0.0712 0.1033 0.5536
8.250 0.9620 0.01631 0.00915 -0.0694 0.0919 0.5596
8.500 0.9788 0.01684 0.00964 -0.0678 0.0817 0.5646
8.750 0.9956 0.01736 0.01014 -0.0663 0.0728 0.5705
9.000 1.0113 0.01794 0.01070 -0.0646 0.0638 0.5764
9.250 1.0274 0.01853 0.01125 -0.0630 0.0564 0.5825
9.500 1.0446 0.01907 0.01179 -0.0616 0.0517 0.5877
9.750 1.0608 0.01965 0.01238 -0.0601 0.0470 0.5941
10.000 1.0766 0.02029 0.01301 -0.0586 0.0416 0.6003
10.250 1.0927 0.02091 0.01363 -0.0571 0.0382 0.6056
10.500 1.1085 0.02157 0.01430 -0.0557 0.0352 0.6115
10.750 1.1247 0.02222 0.01497 -0.0543 0.0325 0.6176
11.000 1.1402 0.02291 0.01568 -0.0529 0.0303 0.6237
11.250 1.1550 0.02367 0.01645 -0.0515 0.0279 0.6289
11.500 1.1709 0.02437 0.01719 -0.0503 0.0263 0.6355
11.750 1.1849 0.02520 0.01804 -0.0488 0.0245 0.6415
12.000 1.2000 0.02599 0.01886 -0.0476 0.0232 0.6475
12.250 1.2139 0.02687 0.01976 -0.0462 0.0217 0.6531
12.500 1.2279 0.02775 0.02069 -0.0450 0.0207 0.6600
12.750 1.2421 0.02865 0.02162 -0.0438 0.0196 0.6661
13.000 1.2546 0.02969 0.02269 -0.0424 0.0187 0.6715
13.250 1.2680 0.03068 0.02372 -0.0413 0.0178 0.6779
13.500 1.2809 0.03172 0.02482 -0.0401 0.0170 0.6849
13.750 1.2928 0.03287 0.02600 -0.0390 0.0162 0.6910
14.000 1.3044 0.03407 0.02724 -0.0378 0.0155 0.6964
14.250 1.3163 0.03527 0.02850 -0.0368 0.0150 0.7033
14.500 1.3282 0.03650 0.02978 -0.0358 0.0144 0.7104
15.000 1.3488 0.03929 0.03266 -0.0339 0.0133 0.7228
15.250 1.3579 0.04084 0.03427 -0.0330 0.0128 0.7296
15.500 1.3681 0.04232 0.03580 -0.0322 0.0124 0.7361
15.750 1.3770 0.04396 0.03751 -0.0314 0.0119 0.7433
16.000 1.3858 0.04564 0.03925 -0.0307 0.0115 0.7503
16.250 1.3931 0.04751 0.04118 -0.0301 0.0111 0.7566
16.500 1.4004 0.04941 0.04313 -0.0295 0.0107 0.7635
16.750 1.4067 0.05145 0.04525 -0.0290 0.0104 0.7718
17.250 1.4201 0.05562 0.04957 -0.0283 0.0099 0.7859
17.500 1.4258 0.05788 0.05190 -0.0281 0.0096 0.7938
17.750 1.4304 0.06030 0.05439 -0.0280 0.0094 0.8012
18.000 1.4342 0.06285 0.05703 -0.0280 0.0092 0.8102
18.500 1.4395 0.06844 0.06278 -0.0283 0.0088 0.8264
18.750 1.4414 0.07142 0.06586 -0.0287 0.0087 0.8352
19.000 1.4419 0.07460 0.06914 -0.0291 0.0085 0.8451
19.250 1.4404 0.07814 0.07277 -0.0298 0.0083 0.8550
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