S4083 (8%) (s4083-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
|---|---|
|
Airfoil: S4083 (8%) (s4083-il) Reynolds number: 500,000 Max Cl/Cd: 102.79 at α=6.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-s4083-il-500000.txt Download as CSV file: xf-s4083-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: S4083 (8%)
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-9.000 -0.3031 0.09305 0.09093 -0.0218 1.0000 0.0145
-8.750 -0.3018 0.08949 0.08738 -0.0224 1.0000 0.0145
-8.500 -0.3057 0.08409 0.08203 -0.0223 1.0000 0.0150
-8.250 -0.3024 0.08099 0.07894 -0.0218 1.0000 0.0152
-8.000 -0.2999 0.07792 0.07589 -0.0216 1.0000 0.0155
-7.750 -0.2990 0.07481 0.07279 -0.0216 1.0000 0.0157
-7.500 -0.2995 0.07166 0.06967 -0.0215 1.0000 0.0159
-7.250 -0.3014 0.06863 0.06667 -0.0213 1.0000 0.0161
-7.000 -0.3056 0.06574 0.06382 -0.0207 1.0000 0.0164
-6.750 -0.3136 0.06318 0.06130 -0.0194 1.0000 0.0166
-6.500 -0.3232 0.06066 0.05884 -0.0183 1.0000 0.0167
-6.250 -0.3273 0.05758 0.05579 -0.0188 1.0000 0.0170
-6.000 -0.3298 0.05429 0.05252 -0.0199 1.0000 0.0172
-5.750 -0.3055 0.04799 0.04619 -0.0291 0.9970 0.0179
-5.500 -0.2760 0.04089 0.03901 -0.0400 0.9939 0.0189
-5.250 -0.2380 0.03367 0.03161 -0.0513 0.9903 0.0204
-5.000 -0.2027 0.02751 0.02518 -0.0588 0.9871 0.0207
-4.750 -0.1784 0.01825 0.01551 -0.0662 0.9829 0.0218
-4.500 -0.1482 0.01568 0.01286 -0.0691 0.9779 0.0227
-4.250 -0.1133 0.01298 0.00996 -0.0725 0.9744 0.0244
-3.750 -0.0472 0.00757 0.00359 -0.0766 0.9625 0.0311
-3.500 -0.0397 0.01671 0.01205 -0.0750 0.9667 0.0194
-3.250 -0.0028 0.01375 0.00862 -0.0765 0.9622 0.0176
-3.000 0.0287 0.01280 0.00752 -0.0769 0.9520 0.0190
-2.750 0.0623 0.01122 0.00574 -0.0775 0.9414 0.0182
-2.500 0.1023 0.00999 0.00435 -0.0797 0.9288 0.0180
-2.250 0.1551 0.00904 0.00328 -0.0847 0.9108 0.0188
-2.000 0.2112 0.00832 0.00234 -0.0906 0.8725 0.0225
-1.750 0.2463 0.00792 0.00180 -0.0918 0.8158 0.0587
-1.500 0.2701 0.00767 0.00165 -0.0909 0.7625 0.1646
-1.250 0.2925 0.00749 0.00160 -0.0897 0.7169 0.2783
-1.000 0.3140 0.00718 0.00162 -0.0885 0.6796 0.4470
-0.750 0.3354 0.00692 0.00166 -0.0871 0.6481 0.6029
-0.500 0.3572 0.00678 0.00167 -0.0856 0.6211 0.7073
0.000 0.4300 0.00646 0.00162 -0.0889 0.5721 1.0000
0.250 0.4553 0.00662 0.00161 -0.0882 0.5534 1.0000
0.500 0.4807 0.00677 0.00162 -0.0876 0.5364 1.0000
0.750 0.5063 0.00692 0.00165 -0.0870 0.5211 1.0000
1.250 0.5580 0.00720 0.00172 -0.0859 0.4938 1.0000
1.500 0.5840 0.00734 0.00177 -0.0854 0.4811 1.0000
1.750 0.6101 0.00748 0.00183 -0.0849 0.4692 1.0000
2.000 0.6361 0.00762 0.00190 -0.0845 0.4580 1.0000
2.250 0.6621 0.00777 0.00198 -0.0840 0.4477 1.0000
2.500 0.6882 0.00792 0.00207 -0.0835 0.4375 1.0000
2.750 0.7145 0.00805 0.00216 -0.0831 0.4280 1.0000
3.000 0.7405 0.00821 0.00228 -0.0827 0.4189 1.0000
3.250 0.7666 0.00835 0.00239 -0.0822 0.4097 1.0000
3.500 0.7927 0.00849 0.00251 -0.0818 0.4004 1.0000
3.750 0.8185 0.00867 0.00264 -0.0813 0.3915 1.0000
4.000 0.8447 0.00881 0.00279 -0.0809 0.3820 1.0000
4.250 0.8706 0.00897 0.00294 -0.0805 0.3728 1.0000
4.500 0.8962 0.00916 0.00310 -0.0800 0.3640 1.0000
4.750 0.9223 0.00930 0.00326 -0.0796 0.3550 1.0000
5.000 0.9481 0.00948 0.00345 -0.0791 0.3453 1.0000
5.250 0.9734 0.00967 0.00363 -0.0786 0.3349 1.0000
5.500 0.9990 0.00985 0.00382 -0.0781 0.3242 1.0000
5.750 1.0247 0.01003 0.00402 -0.0777 0.3141 1.0000
6.000 1.0500 0.01023 0.00425 -0.0772 0.3028 1.0000
6.250 1.0751 0.01046 0.00448 -0.0766 0.2908 1.0000
6.500 1.0998 0.01070 0.00471 -0.0761 0.2740 1.0000
6.750 1.1235 0.01104 0.00497 -0.0754 0.2487 1.0000
7.000 1.1467 0.01145 0.00528 -0.0746 0.2218 1.0000
7.250 1.1696 0.01191 0.00566 -0.0738 0.1967 1.0000
7.500 1.1916 0.01246 0.00609 -0.0729 0.1694 1.0000
7.750 1.2130 0.01307 0.00659 -0.0719 0.1417 1.0000
8.000 1.2332 0.01379 0.00717 -0.0708 0.1112 1.0000
8.250 1.2516 0.01471 0.00789 -0.0694 0.0776 1.0000
8.500 1.2652 0.01611 0.00898 -0.0674 0.0323 1.0000
8.750 1.2782 0.01756 0.01032 -0.0650 0.0127 1.0000
9.000 1.2974 0.01831 0.01118 -0.0636 0.0111 1.0000
9.250 1.3155 0.01913 0.01210 -0.0620 0.0099 1.0000
9.500 1.3305 0.02020 0.01328 -0.0601 0.0090 1.0000
9.750 1.3400 0.02167 0.01492 -0.0573 0.0084 1.0000
10.000 1.3513 0.02286 0.01625 -0.0548 0.0082 1.0000
10.250 1.3616 0.02404 0.01755 -0.0523 0.0079 1.0000
10.500 1.3684 0.02529 0.01896 -0.0493 0.0078 1.0000
10.750 1.3704 0.02663 0.02042 -0.0455 0.0077 1.0000
11.000 1.3712 0.02808 0.02200 -0.0419 0.0076 1.0000
11.250 1.3710 0.02966 0.02371 -0.0385 0.0075 1.0000
11.500 1.3702 0.03140 0.02558 -0.0356 0.0074 1.0000
11.750 1.3693 0.03331 0.02762 -0.0331 0.0073 1.0000
12.000 1.3704 0.03516 0.02958 -0.0314 0.0070 1.0000
12.250 1.3674 0.03765 0.03220 -0.0299 0.0068 1.0000
12.500 1.3646 0.04038 0.03507 -0.0290 0.0067 1.0000
12.750 1.3616 0.04338 0.03821 -0.0285 0.0067 1.0000
13.000 1.3565 0.04689 0.04187 -0.0284 0.0067 1.0000
13.250 1.3524 0.05046 0.04559 -0.0288 0.0066 1.0000
13.500 1.3469 0.05439 0.04967 -0.0294 0.0066 1.0000
13.750 1.3408 0.05855 0.05399 -0.0303 0.0066 1.0000
14.000 1.3348 0.06281 0.05839 -0.0316 0.0065 1.0000
14.250 1.3267 0.06753 0.06326 -0.0331 0.0065 1.0000
14.500 1.3163 0.07275 0.06866 -0.0348 0.0065 1.0000
14.750 1.3056 0.07817 0.07425 -0.0369 0.0066 1.0000
15.000 1.2948 0.08380 0.08004 -0.0394 0.0065 1.0000
15.250 1.2817 0.09010 0.08651 -0.0424 0.0066 1.0000
15.500 1.2683 0.09669 0.09327 -0.0457 0.0066 1.0000
15.750 1.2528 0.10403 0.10079 -0.0495 0.0067 1.0000
16.000 1.2397 0.11114 0.10805 -0.0535 0.0066 1.0000
16.250 1.2212 0.11977 0.11687 -0.0584 0.0068 1.0000
16.500 1.2044 0.12841 0.12567 -0.0635 0.0068 1.0000
16.750 1.1878 0.13736 0.13477 -0.0689 0.0069 1.0000
17.000 1.1714 0.14663 0.14419 -0.0746 0.0070 1.0000
17.250 1.1534 0.15684 0.15453 -0.0810 0.0072 1.0000
17.500 1.1344 0.16794 0.16576 -0.0879 0.0073 1.0000
17.750 1.1136 0.18042 0.17835 -0.0954 0.0075 1.0000
18.000 1.0813 0.19857 0.19657 -0.1055 0.0080 1.0000
18.250 1.0747 0.20728 0.20528 -0.1099 0.0084 1.0000
|
Polar data table (+)
Polar graphs
<< Back to S4083 (8%) (s4083-il)