S1048 14% (Danny Howell) (s1048-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: S1048 14% (Danny Howell) (s1048-il) Reynolds number: 200,000 Max Cl/Cd: 54.63 at α=6.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-s1048-il-200000-n5.txt Download as CSV file: xf-s1048-il-200000-n5.csv |
XFOIL Version 6.96
Calculated polar for: S1048 14% (Danny Howell)
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.000 -0.8498 0.15247 0.14855 0.0214 1.0000 0.0101
-17.750 -0.8709 0.14211 0.13803 0.0155 1.0000 0.0100
-17.500 -0.8873 0.13344 0.12920 0.0106 1.0000 0.0099
-17.250 -0.9014 0.12564 0.12126 0.0062 1.0000 0.0100
-17.000 -0.9132 0.11866 0.11413 0.0023 1.0000 0.0100
-16.750 -0.9237 0.11210 0.10743 -0.0013 1.0000 0.0101
-16.500 -0.9333 0.10594 0.10113 -0.0046 1.0000 0.0103
-16.250 -0.9415 0.10025 0.09530 -0.0076 1.0000 0.0104
-16.000 -0.9494 0.09468 0.08958 -0.0105 1.0000 0.0106
-15.750 -0.9560 0.08956 0.08431 -0.0130 1.0000 0.0108
-15.500 -0.9621 0.08465 0.07924 -0.0155 1.0000 0.0110
-15.250 -0.9673 0.07999 0.07443 -0.0177 1.0000 0.0112
-15.000 -0.9720 0.07567 0.07000 -0.0195 1.0000 0.0114
-14.750 -0.9769 0.07151 0.06576 -0.0212 1.0000 0.0116
-14.500 -0.9823 0.06737 0.06152 -0.0229 1.0000 0.0118
-14.250 -0.9869 0.06345 0.05751 -0.0245 1.0000 0.0121
-14.000 -0.9907 0.05975 0.05372 -0.0258 1.0000 0.0123
-13.750 -0.9942 0.05617 0.05004 -0.0271 1.0000 0.0127
-13.500 -0.9969 0.05282 0.04659 -0.0280 1.0000 0.0129
-13.250 -0.9994 0.04955 0.04321 -0.0289 1.0000 0.0134
-13.000 -1.0008 0.04653 0.04008 -0.0296 1.0000 0.0136
-12.750 -1.0020 0.04361 0.03705 -0.0301 1.0000 0.0139
-12.500 -1.0033 0.04080 0.03410 -0.0304 1.0000 0.0146
-12.250 -1.0027 0.03829 0.03148 -0.0304 1.0000 0.0149
-12.000 -1.0040 0.03573 0.02881 -0.0303 1.0000 0.0154
-11.750 -1.0067 0.03325 0.02624 -0.0298 1.0000 0.0161
-11.500 -1.0056 0.03127 0.02418 -0.0290 1.0000 0.0167
-11.250 -1.0025 0.02960 0.02241 -0.0279 1.0000 0.0178
-11.000 -0.9981 0.02815 0.02086 -0.0264 1.0000 0.0193
-10.750 -0.9944 0.02680 0.01940 -0.0245 1.0000 0.0207
-10.500 -0.9917 0.02552 0.01808 -0.0220 1.0000 0.0224
-10.250 -0.9859 0.02451 0.01699 -0.0195 1.0000 0.0246
-10.000 -0.9774 0.02356 0.01596 -0.0171 1.0000 0.0271
-9.750 -0.9676 0.02253 0.01491 -0.0150 1.0000 0.0308
-9.500 -0.9548 0.02164 0.01398 -0.0132 1.0000 0.0364
-9.250 -0.9412 0.02077 0.01311 -0.0115 1.0000 0.0444
-9.000 -0.9276 0.01985 0.01224 -0.0098 1.0000 0.0560
-8.750 -0.9133 0.01897 0.01144 -0.0081 1.0000 0.0711
-8.500 -0.8976 0.01818 0.01070 -0.0065 1.0000 0.0889
-8.250 -0.8812 0.01745 0.01005 -0.0050 1.0000 0.1076
-8.000 -0.8641 0.01679 0.00946 -0.0035 1.0000 0.1270
-7.750 -0.8462 0.01621 0.00893 -0.0021 1.0000 0.1466
-7.500 -0.8287 0.01563 0.00844 -0.0006 1.0000 0.1680
-7.250 -0.8112 0.01509 0.00799 0.0010 1.0000 0.1925
-7.000 -0.7933 0.01461 0.00760 0.0025 1.0000 0.2175
-6.750 -0.7752 0.01419 0.00726 0.0040 1.0000 0.2391
-6.500 -0.7499 0.01385 0.00693 0.0041 0.9966 0.2580
-6.250 -0.7144 0.01348 0.00659 0.0021 0.9854 0.2786
-6.000 -0.6793 0.01316 0.00626 0.0003 0.9727 0.2993
-5.750 -0.6442 0.01287 0.00597 -0.0014 0.9587 0.3181
-5.500 -0.6088 0.01260 0.00570 -0.0031 0.9437 0.3352
-5.250 -0.5733 0.01237 0.00544 -0.0047 0.9279 0.3511
-5.000 -0.5390 0.01215 0.00518 -0.0061 0.9108 0.3664
-4.750 -0.5075 0.01197 0.00495 -0.0068 0.8918 0.3805
-4.500 -0.4782 0.01182 0.00475 -0.0069 0.8724 0.3940
-4.250 -0.4503 0.01169 0.00455 -0.0068 0.8537 0.4067
-3.750 -0.3974 0.01148 0.00422 -0.0060 0.8184 0.4313
-3.500 -0.3714 0.01139 0.00407 -0.0054 0.8018 0.4430
-3.250 -0.3453 0.01130 0.00393 -0.0049 0.7859 0.4548
-3.000 -0.3191 0.01123 0.00380 -0.0045 0.7708 0.4667
-2.750 -0.2928 0.01117 0.00368 -0.0040 0.7561 0.4789
-2.500 -0.2666 0.01111 0.00358 -0.0036 0.7419 0.4907
-2.250 -0.2402 0.01105 0.00349 -0.0032 0.7282 0.5023
-2.000 -0.2138 0.01100 0.00341 -0.0028 0.7148 0.5142
-1.750 -0.1872 0.01096 0.00332 -0.0024 0.7015 0.5261
-1.500 -0.1605 0.01092 0.00326 -0.0020 0.6883 0.5383
-1.250 -0.1338 0.01089 0.00321 -0.0017 0.6752 0.5504
-1.000 -0.1071 0.01086 0.00317 -0.0013 0.6624 0.5625
-0.750 -0.0804 0.01083 0.00314 -0.0010 0.6498 0.5746
-0.500 -0.0536 0.01082 0.00312 -0.0007 0.6372 0.5869
-0.250 -0.0268 0.01082 0.00310 -0.0003 0.6248 0.5995
0.000 0.0000 0.01082 0.00309 0.0000 0.6122 0.6122
0.250 0.0268 0.01082 0.00310 0.0003 0.5995 0.6248
0.500 0.0536 0.01082 0.00312 0.0007 0.5870 0.6372
0.750 0.0804 0.01083 0.00315 0.0010 0.5746 0.6498
1.000 0.1071 0.01086 0.00317 0.0013 0.5625 0.6624
1.250 0.1338 0.01089 0.00321 0.0017 0.5504 0.6752
1.500 0.1605 0.01092 0.00326 0.0020 0.5384 0.6883
1.750 0.1872 0.01096 0.00332 0.0024 0.5261 0.7015
2.000 0.2137 0.01100 0.00341 0.0028 0.5142 0.7148
2.250 0.2402 0.01105 0.00349 0.0032 0.5024 0.7282
2.500 0.2665 0.01111 0.00358 0.0036 0.4907 0.7420
2.750 0.2928 0.01117 0.00368 0.0040 0.4788 0.7562
3.000 0.3191 0.01123 0.00380 0.0045 0.4667 0.7708
3.250 0.3453 0.01130 0.00393 0.0049 0.4547 0.7859
3.500 0.3713 0.01139 0.00407 0.0054 0.4429 0.8018
3.750 0.3974 0.01148 0.00421 0.0060 0.4312 0.8184
4.250 0.4503 0.01169 0.00455 0.0068 0.4067 0.8537
4.500 0.4782 0.01182 0.00475 0.0069 0.3939 0.8724
4.750 0.5075 0.01197 0.00496 0.0068 0.3806 0.8918
5.000 0.5390 0.01216 0.00518 0.0061 0.3662 0.9108
5.250 0.5733 0.01237 0.00544 0.0047 0.3511 0.9279
5.500 0.6088 0.01260 0.00570 0.0031 0.3351 0.9437
5.750 0.6442 0.01287 0.00597 0.0014 0.3180 0.9587
6.000 0.6793 0.01316 0.00626 -0.0003 0.2995 0.9727
6.250 0.7143 0.01348 0.00658 -0.0021 0.2784 0.9853
6.500 0.7499 0.01385 0.00693 -0.0041 0.2581 0.9966
6.750 0.7752 0.01419 0.00726 -0.0040 0.2392 1.0000
7.000 0.7933 0.01461 0.00760 -0.0025 0.2174 1.0000
7.250 0.8113 0.01509 0.00799 -0.0010 0.1926 1.0000
7.500 0.8287 0.01563 0.00844 0.0006 0.1678 1.0000
7.750 0.8462 0.01621 0.00893 0.0021 0.1465 1.0000
8.000 0.8641 0.01679 0.00946 0.0035 0.1270 1.0000
8.250 0.8812 0.01745 0.01005 0.0050 0.1077 1.0000
8.500 0.8977 0.01817 0.01070 0.0065 0.0893 1.0000
8.750 0.9133 0.01897 0.01144 0.0081 0.0711 1.0000
9.000 0.9277 0.01985 0.01224 0.0098 0.0563 1.0000
9.250 0.9413 0.02076 0.01310 0.0115 0.0447 1.0000
9.500 0.9549 0.02164 0.01398 0.0132 0.0364 1.0000
9.750 0.9676 0.02253 0.01491 0.0151 0.0309 1.0000
10.000 0.9773 0.02357 0.01596 0.0172 0.0270 1.0000
10.250 0.9858 0.02451 0.01699 0.0195 0.0247 1.0000
10.500 0.9917 0.02552 0.01808 0.0220 0.0225 1.0000
10.750 0.9948 0.02678 0.01937 0.0244 0.0206 1.0000
11.000 0.9983 0.02815 0.02085 0.0264 0.0193 1.0000
11.250 1.0030 0.02957 0.02238 0.0278 0.0178 1.0000
11.500 1.0055 0.03128 0.02420 0.0290 0.0168 1.0000
11.750 1.0065 0.03328 0.02627 0.0298 0.0160 1.0000
12.000 1.0056 0.03562 0.02869 0.0302 0.0155 1.0000
12.250 1.0030 0.03829 0.03147 0.0304 0.0149 1.0000
12.500 1.0036 0.04080 0.03411 0.0303 0.0145 1.0000
12.750 1.0032 0.04352 0.03695 0.0300 0.0141 1.0000
13.000 1.0016 0.04649 0.04004 0.0295 0.0135 1.0000
13.250 1.0001 0.04953 0.04319 0.0288 0.0133 1.0000
13.500 0.9976 0.05279 0.04656 0.0280 0.0130 1.0000
13.750 0.9947 0.05620 0.05007 0.0269 0.0126 1.0000
14.000 0.9916 0.05972 0.05369 0.0258 0.0124 1.0000
14.250 0.9874 0.06347 0.05752 0.0243 0.0120 1.0000
14.500 0.9835 0.06731 0.06145 0.0228 0.0118 1.0000
14.750 0.9783 0.07143 0.06568 0.0211 0.0116 1.0000
15.000 0.9732 0.07564 0.06997 0.0193 0.0113 1.0000
15.250 0.9685 0.07998 0.07443 0.0175 0.0112 1.0000
15.500 0.9632 0.08469 0.07930 0.0152 0.0109 1.0000
15.750 0.9577 0.08944 0.08419 0.0130 0.0108 1.0000
16.000 0.9506 0.09470 0.08959 0.0103 0.0106 1.0000
16.250 0.9422 0.10039 0.09545 0.0072 0.0102 1.0000
16.500 0.9334 0.10623 0.10143 0.0042 0.0101 1.0000
16.750 0.9242 0.11230 0.10763 0.0010 0.0100 1.0000
17.000 0.9141 0.11874 0.11421 -0.0025 0.0100 1.0000
17.250 0.9024 0.12570 0.12131 -0.0064 0.0100 1.0000
17.500 0.8894 0.13323 0.12899 -0.0106 0.0100 1.0000
17.750 0.8725 0.14207 0.13798 -0.0157 0.0100 1.0000
18.000 0.8515 0.15239 0.14846 -0.0215 0.0101 1.0000
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