S1046 17% (Danny Howell) (s1046-il) Xfoil prediction polar at RE=100,000 Ncrit=9
| Details | Polar file |
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Airfoil: S1046 17% (Danny Howell) (s1046-il) Reynolds number: 100,000 Max Cl/Cd: 37.18 at α=7° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-s1046-il-100000.txt Download as CSV file: xf-s1046-il-100000.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 = 0.100 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.000 -0.5200 0.18632 0.18169 0.0217 1.0000 0.1271
-17.750 -0.6758 0.19870 0.19327 0.0267 1.0000 0.1268
-17.500 -0.9601 0.10939 0.10371 -0.0194 1.0000 0.0657
-17.250 -0.8681 0.12390 0.11860 -0.0091 1.0000 0.0762
-17.000 -0.9373 0.10620 0.10067 -0.0194 1.0000 0.0734
-16.750 -0.9838 0.09436 0.08854 -0.0262 1.0000 0.0723
-16.500 -1.0101 0.08666 0.08059 -0.0302 1.0000 0.0729
-16.250 -1.0327 0.08004 0.07372 -0.0335 1.0000 0.0742
-16.000 -1.0547 0.07398 0.06740 -0.0362 1.0000 0.0757
-15.750 -1.0461 0.07187 0.06541 -0.0361 1.0000 0.0806
-15.500 -1.0540 0.06795 0.06140 -0.0374 1.0000 0.0843
-15.250 -0.7010 0.13214 0.12669 -0.0010 1.0000 0.1225
-15.000 -1.0671 0.06074 0.05405 -0.0389 1.0000 0.0933
-14.750 -1.0775 0.05704 0.05020 -0.0397 1.0000 0.0980
-14.500 -1.0822 0.05394 0.04708 -0.0399 1.0000 0.1040
-14.250 -1.0874 0.05114 0.04424 -0.0401 1.0000 0.1103
-14.000 -1.0925 0.04829 0.04134 -0.0399 1.0000 0.1168
-13.750 -1.0977 0.04584 0.03885 -0.0395 1.0000 0.1239
-13.500 -1.1002 0.04356 0.03657 -0.0389 1.0000 0.1313
-13.250 -1.1074 0.04129 0.03419 -0.0379 1.0000 0.1387
-13.000 -1.1057 0.03963 0.03260 -0.0368 1.0000 0.1469
-12.750 -1.1160 0.03758 0.03034 -0.0349 1.0000 0.1543
-12.500 -1.1104 0.03646 0.02935 -0.0334 1.0000 0.1636
-12.250 -1.1145 0.03500 0.02781 -0.0309 1.0000 0.1720
-12.000 -1.1158 0.03403 0.02681 -0.0280 1.0000 0.1810
-11.750 -1.1126 0.03324 0.02610 -0.0253 1.0000 0.1904
-11.500 -1.1145 0.03225 0.02496 -0.0220 1.0000 0.2001
-11.250 -1.1063 0.03166 0.02439 -0.0197 1.0000 0.2110
-11.000 -1.0930 0.03110 0.02391 -0.0179 1.0000 0.2219
-10.750 -1.0828 0.03038 0.02314 -0.0157 1.0000 0.2328
-10.500 -1.0774 0.02957 0.02209 -0.0129 1.0000 0.2436
-10.250 -1.0558 0.02918 0.02187 -0.0120 1.0000 0.2548
-10.000 -1.0386 0.02865 0.02136 -0.0105 1.0000 0.2655
-9.750 -1.0266 0.02795 0.02054 -0.0084 1.0000 0.2765
-9.500 -1.0100 0.02751 0.02008 -0.0068 1.0000 0.2876
-9.250 -0.9894 0.02714 0.01978 -0.0056 1.0000 0.2981
-9.000 -0.9745 0.02657 0.01915 -0.0037 1.0000 0.3089
-8.750 -0.9606 0.02609 0.01858 -0.0016 1.0000 0.3198
-8.500 -0.9393 0.02580 0.01842 -0.0004 1.0000 0.3296
-8.250 -0.9261 0.02525 0.01779 0.0018 1.0000 0.3397
-8.000 -0.9116 0.02489 0.01743 0.0038 1.0000 0.3497
-7.750 -0.8965 0.02455 0.01714 0.0059 1.0000 0.3586
-7.500 -0.8926 0.02406 0.01648 0.0093 1.0000 0.3683
-7.250 -0.8774 0.02390 0.01649 0.0113 1.0000 0.3761
-7.000 -0.8730 0.02346 0.01590 0.0144 1.0000 0.3855
-6.750 -0.8595 0.02335 0.01589 0.0165 1.0000 0.3936
-6.500 -0.8504 0.02302 0.01548 0.0188 1.0000 0.4029
-6.250 -0.8303 0.02287 0.01532 0.0194 0.9979 0.4130
-6.000 -0.7832 0.02279 0.01525 0.0152 0.9878 0.4259
-5.750 -0.7372 0.02263 0.01506 0.0112 0.9777 0.4388
-5.500 -0.6900 0.02244 0.01482 0.0071 0.9681 0.4523
-5.250 -0.6492 0.02220 0.01448 0.0042 0.9566 0.4656
-5.000 -0.6051 0.02207 0.01438 0.0010 0.9464 0.4780
-4.750 -0.5539 0.02192 0.01426 -0.0034 0.9386 0.4906
-4.500 -0.5133 0.02172 0.01406 -0.0058 0.9274 0.5027
-4.250 -0.4700 0.02148 0.01377 -0.0087 0.9180 0.5159
-4.000 -0.4303 0.02124 0.01348 -0.0108 0.9074 0.5294
-3.750 -0.3939 0.02121 0.01353 -0.0119 0.8952 0.5394
-3.500 -0.3596 0.02107 0.01338 -0.0128 0.8836 0.5510
-3.250 -0.3258 0.02087 0.01312 -0.0135 0.8731 0.5635
-3.000 -0.2990 0.02084 0.01310 -0.0128 0.8592 0.5745
-2.750 -0.2722 0.02083 0.01312 -0.0121 0.8459 0.5846
-2.500 -0.2474 0.02074 0.01298 -0.0112 0.8329 0.5964
-2.250 -0.2212 0.02069 0.01290 -0.0103 0.8211 0.6082
-2.000 -0.1943 0.02070 0.01293 -0.0093 0.8089 0.6180
-1.750 -0.1715 0.02066 0.01287 -0.0081 0.7953 0.6297
-1.500 -0.1486 0.02062 0.01278 -0.0068 0.7824 0.6424
-1.250 -0.1217 0.02067 0.01288 -0.0058 0.7708 0.6518
-1.000 -0.0968 0.02060 0.01278 -0.0046 0.7593 0.6635
-0.750 -0.0745 0.02058 0.01272 -0.0034 0.7460 0.6764
-0.500 -0.0490 0.02065 0.01285 -0.0023 0.7336 0.6865
-0.250 -0.0238 0.02062 0.01279 -0.0012 0.7226 0.6980
0.000 0.0000 0.02056 0.01271 0.0000 0.7108 0.7108
0.250 0.0238 0.02062 0.01279 0.0012 0.6981 0.7227
0.500 0.0490 0.02065 0.01285 0.0023 0.6865 0.7336
0.750 0.0745 0.02058 0.01273 0.0034 0.6764 0.7460
1.000 0.0968 0.02060 0.01278 0.0046 0.6635 0.7593
1.250 0.1217 0.02067 0.01288 0.0058 0.6518 0.7708
1.500 0.1486 0.02062 0.01278 0.0068 0.6424 0.7824
1.750 0.1715 0.02066 0.01287 0.0081 0.6297 0.7953
2.000 0.1943 0.02069 0.01293 0.0093 0.6180 0.8088
2.250 0.2212 0.02069 0.01290 0.0103 0.6082 0.8211
2.500 0.2474 0.02074 0.01298 0.0112 0.5964 0.8329
2.750 0.2721 0.02083 0.01312 0.0121 0.5846 0.8459
3.000 0.2990 0.02084 0.01310 0.0128 0.5745 0.8592
3.250 0.3258 0.02086 0.01312 0.0135 0.5635 0.8731
3.500 0.3596 0.02107 0.01338 0.0128 0.5510 0.8837
3.750 0.3939 0.02121 0.01353 0.0119 0.5395 0.8953
4.000 0.4303 0.02124 0.01346 0.0108 0.5293 0.9074
4.250 0.4700 0.02148 0.01377 0.0087 0.5159 0.9180
4.500 0.5133 0.02172 0.01406 0.0058 0.5028 0.9274
4.750 0.5539 0.02192 0.01426 0.0034 0.4906 0.9386
5.000 0.6051 0.02207 0.01438 -0.0010 0.4780 0.9464
5.250 0.6493 0.02219 0.01447 -0.0042 0.4656 0.9567
5.500 0.6900 0.02245 0.01482 -0.0071 0.4524 0.9681
5.750 0.7373 0.02263 0.01506 -0.0113 0.4389 0.9778
6.000 0.7832 0.02279 0.01525 -0.0152 0.4260 0.9878
6.250 0.8304 0.02287 0.01532 -0.0194 0.4129 0.9979
6.500 0.8503 0.02301 0.01547 -0.0188 0.4029 1.0000
6.750 0.8593 0.02335 0.01589 -0.0164 0.3936 1.0000
7.000 0.8727 0.02347 0.01592 -0.0144 0.3855 1.0000
7.250 0.8772 0.02390 0.01649 -0.0113 0.3762 1.0000
7.500 0.8924 0.02405 0.01648 -0.0092 0.3683 1.0000
7.750 0.8964 0.02455 0.01714 -0.0059 0.3586 1.0000
8.000 0.9115 0.02489 0.01742 -0.0038 0.3498 1.0000
8.250 0.9261 0.02524 0.01779 -0.0018 0.3397 1.0000
8.500 0.9393 0.02580 0.01841 0.0004 0.3296 1.0000
8.750 0.9606 0.02609 0.01858 0.0016 0.3198 1.0000
9.000 0.9744 0.02657 0.01915 0.0037 0.3089 1.0000
9.250 0.9894 0.02714 0.01978 0.0056 0.2981 1.0000
9.500 1.0101 0.02751 0.02007 0.0067 0.2876 1.0000
9.750 1.0267 0.02795 0.02053 0.0084 0.2765 1.0000
10.000 1.0387 0.02865 0.02136 0.0105 0.2655 1.0000
10.250 1.0558 0.02918 0.02187 0.0120 0.2548 1.0000
10.500 1.0776 0.02958 0.02210 0.0129 0.2436 1.0000
10.750 1.0830 0.03037 0.02313 0.0157 0.2327 1.0000
11.000 1.0932 0.03110 0.02391 0.0178 0.2219 1.0000
11.250 1.1064 0.03166 0.02439 0.0196 0.2109 1.0000
11.500 1.1147 0.03224 0.02495 0.0219 0.2000 1.0000
11.750 1.1130 0.03325 0.02610 0.0252 0.1903 1.0000
12.000 1.1160 0.03404 0.02683 0.0280 0.1809 1.0000
12.250 1.1152 0.03499 0.02779 0.0308 0.1719 1.0000
12.500 1.1107 0.03646 0.02935 0.0333 0.1635 1.0000
12.750 1.1163 0.03758 0.03034 0.0348 0.1542 1.0000
13.000 1.1064 0.03962 0.03259 0.0367 0.1468 1.0000
13.250 1.1078 0.04129 0.03420 0.0378 0.1386 1.0000
13.500 1.1012 0.04353 0.03654 0.0388 0.1311 1.0000
13.750 1.0986 0.04583 0.03884 0.0394 0.1238 1.0000
14.000 1.0940 0.04824 0.04127 0.0398 0.1166 1.0000
14.250 1.0878 0.05116 0.04426 0.0399 0.1101 1.0000
14.500 1.0838 0.05387 0.04699 0.0398 0.1037 1.0000
14.750 1.0787 0.05703 0.05020 0.0396 0.0980 1.0000
15.000 1.0684 0.06070 0.05400 0.0388 0.0930 1.0000
15.250 1.0727 0.06306 0.05623 0.0388 0.0871 1.0000
15.500 1.0552 0.06795 0.06139 0.0372 0.0842 1.0000
15.750 1.0482 0.07171 0.06523 0.0360 0.0803 1.0000
16.000 1.0551 0.07408 0.06750 0.0360 0.0756 1.0000
16.250 1.0337 0.08009 0.07378 0.0332 0.0741 1.0000
16.500 1.0113 0.08670 0.08063 0.0300 0.0728 1.0000
16.750 0.9846 0.09446 0.08863 0.0259 0.0720 1.0000
17.000 0.9384 0.10625 0.10072 0.0191 0.0731 1.0000
17.250 0.8508 0.12806 0.12282 0.0063 0.0771 1.0000
17.500 0.9523 0.11109 0.10549 0.0178 0.0663 1.0000
17.750 0.7000 0.18334 0.17791 -0.0211 0.0881 1.0000
18.000 0.7045 0.18897 0.18356 -0.0231 0.0883 1.0000
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