S1046 17% (Danny Howell) (s1046-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: S1046 17% (Danny Howell) (s1046-il) Reynolds number: 500,000 Max Cl/Cd: 70.38 at α=9° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-s1046-il-500000-n5.txt Download as CSV file: xf-s1046-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: S1046 17% (Danny Howell)
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.500 -1.0784 0.10224 0.09759 -0.0114 1.0000 0.0124
-18.250 -1.0879 0.09702 0.09229 -0.0138 1.0000 0.0126
-18.000 -1.0974 0.09191 0.08709 -0.0162 1.0000 0.0130
-17.750 -1.1065 0.08697 0.08206 -0.0184 1.0000 0.0133
-17.500 -1.1143 0.08228 0.07728 -0.0204 1.0000 0.0136
-17.250 -1.1217 0.07777 0.07268 -0.0222 1.0000 0.0140
-17.000 -1.1283 0.07346 0.06828 -0.0240 1.0000 0.0144
-16.750 -1.1343 0.06929 0.06402 -0.0256 1.0000 0.0148
-16.500 -1.1393 0.06536 0.05999 -0.0270 1.0000 0.0152
-16.250 -1.1460 0.06131 0.05586 -0.0284 1.0000 0.0155
-16.000 -1.1523 0.05741 0.05188 -0.0297 1.0000 0.0161
-15.750 -1.1564 0.05389 0.04828 -0.0307 1.0000 0.0167
-15.500 -1.1602 0.05051 0.04482 -0.0316 1.0000 0.0174
-15.250 -1.1622 0.04743 0.04166 -0.0323 1.0000 0.0180
-15.000 -1.1654 0.04436 0.03852 -0.0329 1.0000 0.0192
-14.750 -1.1668 0.04156 0.03565 -0.0333 1.0000 0.0200
-14.500 -1.1679 0.03889 0.03292 -0.0335 1.0000 0.0216
-14.250 -1.1668 0.03651 0.03047 -0.0335 1.0000 0.0227
-14.000 -1.1668 0.03411 0.02802 -0.0334 1.0000 0.0247
-13.750 -1.1641 0.03204 0.02591 -0.0331 1.0000 0.0267
-13.500 -1.1618 0.03001 0.02384 -0.0327 1.0000 0.0291
-13.250 -1.1579 0.02821 0.02200 -0.0321 1.0000 0.0320
-13.000 -1.1538 0.02651 0.02028 -0.0313 1.0000 0.0352
-12.750 -1.1478 0.02504 0.01877 -0.0304 1.0000 0.0386
-12.500 -1.1424 0.02362 0.01734 -0.0293 1.0000 0.0423
-12.250 -1.1354 0.02240 0.01609 -0.0280 1.0000 0.0469
-12.000 -1.1294 0.02122 0.01491 -0.0264 1.0000 0.0514
-11.750 -1.1215 0.02025 0.01392 -0.0247 1.0000 0.0567
-11.500 -1.1150 0.01929 0.01298 -0.0226 1.0000 0.0632
-11.250 -1.1070 0.01849 0.01220 -0.0204 1.0000 0.0692
-11.000 -1.0981 0.01782 0.01153 -0.0180 1.0000 0.0762
-10.750 -1.0915 0.01714 0.01089 -0.0150 1.0000 0.0843
-10.500 -1.0823 0.01659 0.01036 -0.0122 1.0000 0.0917
-10.250 -1.0690 0.01607 0.00986 -0.0101 1.0000 0.1004
-10.000 -1.0557 0.01553 0.00936 -0.0080 1.0000 0.1096
-9.750 -1.0409 0.01506 0.00893 -0.0061 1.0000 0.1178
-9.500 -1.0117 0.01454 0.00843 -0.0070 0.9855 0.1286
-9.250 -0.9765 0.01394 0.00789 -0.0093 0.9571 0.1438
-9.000 -0.9402 0.01336 0.00736 -0.0116 0.9271 0.1612
-8.750 -0.9147 0.01299 0.00695 -0.0115 0.8946 0.1739
-8.500 -0.8930 0.01275 0.00663 -0.0104 0.8678 0.1842
-8.250 -0.8718 0.01248 0.00631 -0.0093 0.8457 0.1936
-8.000 -0.8493 0.01227 0.00603 -0.0083 0.8270 0.2017
-7.750 -0.8262 0.01205 0.00576 -0.0075 0.8108 0.2113
-7.500 -0.8029 0.01181 0.00549 -0.0068 0.7959 0.2214
-7.250 -0.7787 0.01161 0.00525 -0.0062 0.7825 0.2310
-7.000 -0.7542 0.01142 0.00502 -0.0056 0.7701 0.2407
-6.500 -0.7039 0.01108 0.00459 -0.0047 0.7470 0.2576
-6.250 -0.6786 0.01089 0.00439 -0.0042 0.7367 0.2660
-6.000 -0.6525 0.01077 0.00421 -0.0039 0.7262 0.2738
-5.750 -0.6267 0.01059 0.00402 -0.0035 0.7164 0.2822
-5.250 -0.5741 0.01032 0.00369 -0.0030 0.6972 0.2991
-5.000 -0.5474 0.01021 0.00354 -0.0027 0.6879 0.3069
-4.750 -0.5209 0.01007 0.00340 -0.0025 0.6787 0.3156
-4.500 -0.4939 0.00996 0.00326 -0.0023 0.6695 0.3235
-4.250 -0.4671 0.00986 0.00313 -0.0021 0.6604 0.3320
-4.000 -0.4400 0.00975 0.00301 -0.0019 0.6509 0.3404
-3.750 -0.4129 0.00966 0.00290 -0.0017 0.6417 0.3488
-3.500 -0.3856 0.00956 0.00279 -0.0016 0.6317 0.3572
-3.250 -0.3583 0.00949 0.00269 -0.0014 0.6221 0.3663
-3.000 -0.3311 0.00940 0.00260 -0.0013 0.6117 0.3748
-2.750 -0.3034 0.00934 0.00251 -0.0012 0.6015 0.3840
-2.500 -0.2763 0.00926 0.00243 -0.0010 0.5913 0.3932
-2.250 -0.2486 0.00921 0.00236 -0.0009 0.5804 0.4022
-2.000 -0.2212 0.00915 0.00230 -0.0008 0.5699 0.4116
-1.750 -0.1936 0.00912 0.00224 -0.0007 0.5594 0.4204
-1.500 -0.1660 0.00908 0.00219 -0.0006 0.5487 0.4304
-1.250 -0.1384 0.00904 0.00215 -0.0005 0.5385 0.4395
-1.000 -0.1107 0.00903 0.00212 -0.0004 0.5281 0.4490
-0.750 -0.0831 0.00900 0.00209 -0.0003 0.5179 0.4589
-0.500 -0.0554 0.00899 0.00208 -0.0002 0.5077 0.4680
-0.250 -0.0278 0.00899 0.00206 -0.0001 0.4976 0.4781
0.000 0.0000 0.00897 0.00206 0.0000 0.4879 0.4878
0.250 0.0278 0.00899 0.00206 0.0001 0.4781 0.4976
0.500 0.0554 0.00899 0.00208 0.0002 0.4680 0.5077
0.750 0.0831 0.00900 0.00209 0.0003 0.4589 0.5178
1.250 0.1384 0.00904 0.00215 0.0005 0.4395 0.5384
1.500 0.1660 0.00908 0.00219 0.0006 0.4305 0.5488
1.750 0.1937 0.00912 0.00224 0.0007 0.4206 0.5595
2.000 0.2212 0.00915 0.00230 0.0008 0.4117 0.5698
2.250 0.2487 0.00921 0.00236 0.0009 0.4023 0.5803
2.500 0.2763 0.00926 0.00243 0.0010 0.3931 0.5913
2.750 0.3034 0.00934 0.00251 0.0012 0.3840 0.6014
3.000 0.3311 0.00940 0.00260 0.0013 0.3748 0.6117
3.250 0.3583 0.00949 0.00269 0.0014 0.3663 0.6220
3.500 0.3856 0.00956 0.00279 0.0016 0.3573 0.6317
3.750 0.4129 0.00966 0.00290 0.0017 0.3490 0.6417
4.000 0.4400 0.00975 0.00301 0.0019 0.3404 0.6509
4.250 0.4672 0.00986 0.00313 0.0021 0.3320 0.6603
4.500 0.4939 0.00996 0.00326 0.0023 0.3235 0.6695
4.750 0.5209 0.01007 0.00340 0.0025 0.3157 0.6787
5.000 0.5474 0.01021 0.00354 0.0027 0.3069 0.6881
5.250 0.5741 0.01032 0.00369 0.0030 0.2989 0.6971
5.750 0.6267 0.01059 0.00402 0.0035 0.2820 0.7163
6.000 0.6525 0.01077 0.00421 0.0039 0.2738 0.7263
6.250 0.6786 0.01089 0.00439 0.0042 0.2659 0.7367
6.500 0.7039 0.01108 0.00459 0.0047 0.2577 0.7470
7.000 0.7543 0.01142 0.00502 0.0056 0.2408 0.7701
7.250 0.7787 0.01161 0.00525 0.0062 0.2311 0.7826
7.500 0.8030 0.01181 0.00549 0.0068 0.2213 0.7958
7.750 0.8262 0.01205 0.00576 0.0075 0.2115 0.8107
8.000 0.8494 0.01226 0.00603 0.0083 0.2019 0.8270
8.250 0.8719 0.01248 0.00631 0.0093 0.1936 0.8457
8.750 0.9145 0.01301 0.00696 0.0115 0.1730 0.8943
9.000 0.9403 0.01336 0.00735 0.0116 0.1613 0.9270
9.250 0.9766 0.01394 0.00789 0.0092 0.1437 0.9571
9.500 1.0118 0.01454 0.00843 0.0070 0.1286 0.9856
9.750 1.0410 0.01506 0.00892 0.0061 0.1180 1.0000
10.000 1.0557 0.01553 0.00936 0.0080 0.1090 1.0000
10.250 1.0691 0.01607 0.00986 0.0101 0.1002 1.0000
10.500 1.0828 0.01658 0.01035 0.0122 0.0921 1.0000
10.750 1.0919 0.01714 0.01089 0.0149 0.0844 1.0000
11.000 1.0985 0.01781 0.01152 0.0179 0.0762 1.0000
11.250 1.1076 0.01848 0.01219 0.0203 0.0693 1.0000
11.500 1.1155 0.01928 0.01297 0.0225 0.0631 1.0000
11.750 1.1221 0.02024 0.01391 0.0246 0.0567 1.0000
12.000 1.1306 0.02118 0.01487 0.0263 0.0519 1.0000
12.250 1.1362 0.02238 0.01607 0.0279 0.0470 1.0000
12.500 1.1433 0.02359 0.01731 0.0292 0.0424 1.0000
12.750 1.1487 0.02501 0.01875 0.0303 0.0388 1.0000
13.000 1.1546 0.02649 0.02025 0.0312 0.0351 1.0000
13.250 1.1588 0.02819 0.02198 0.0320 0.0319 1.0000
13.500 1.1632 0.02995 0.02378 0.0326 0.0293 1.0000
13.750 1.1653 0.03200 0.02586 0.0330 0.0267 1.0000
14.000 1.1678 0.03409 0.02800 0.0333 0.0245 1.0000
14.250 1.1685 0.03643 0.03039 0.0334 0.0229 1.0000
14.500 1.1694 0.03883 0.03286 0.0333 0.0215 1.0000
14.750 1.1696 0.04138 0.03548 0.0331 0.0204 1.0000
15.000 1.1655 0.04446 0.03861 0.0327 0.0188 1.0000
15.250 1.1640 0.04735 0.04158 0.0322 0.0182 1.0000
15.500 1.1623 0.05039 0.04470 0.0315 0.0175 1.0000
15.750 1.1585 0.05377 0.04816 0.0306 0.0167 1.0000
16.000 1.1536 0.05740 0.05186 0.0295 0.0160 1.0000
16.250 1.1479 0.06123 0.05577 0.0282 0.0155 1.0000
16.500 1.1418 0.06522 0.05984 0.0268 0.0150 1.0000
16.750 1.1365 0.06918 0.06390 0.0254 0.0147 1.0000
17.000 1.1309 0.07329 0.06810 0.0238 0.0142 1.0000
17.250 1.1237 0.07768 0.07259 0.0220 0.0139 1.0000
17.500 1.1162 0.08222 0.07722 0.0201 0.0135 1.0000
17.750 1.1081 0.08695 0.08204 0.0181 0.0132 1.0000
18.000 1.0986 0.09197 0.08715 0.0159 0.0128 1.0000
18.250 1.0896 0.09700 0.09226 0.0136 0.0126 1.0000
18.500 1.0809 0.10210 0.09745 0.0112 0.0124 1.0000
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