S8036 (16%) (s8036-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: S8036 (16%) (s8036-il) Reynolds number: 1,000,000 Max Cl/Cd: 82.14 at α=7.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-s8036-il-1000000-n5.txt Download as CSV file: xf-s8036-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: S8036 (16%)
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
------ -------- --------- --------- -------- -------- --------
-18.750 -0.8925 0.10832 0.10539 -0.0426 1.0000 0.0059
-18.500 -0.9260 0.09845 0.09537 -0.0477 1.0000 0.0059
-18.250 -0.9552 0.08948 0.08625 -0.0523 1.0000 0.0060
-18.000 -0.9777 0.08190 0.07853 -0.0562 1.0000 0.0059
-17.750 -1.0091 0.07317 0.06963 -0.0608 1.0000 0.0060
-17.500 -1.0211 0.06780 0.06414 -0.0634 1.0000 0.0060
-17.250 -1.0399 0.06174 0.05796 -0.0663 1.0000 0.0058
-17.000 -1.0454 0.05780 0.05391 -0.0679 1.0000 0.0060
-16.750 -1.0598 0.05295 0.04893 -0.0697 1.0000 0.0059
-16.500 -1.0656 0.04943 0.04531 -0.0707 1.0000 0.0059
-16.250 -1.0696 0.04634 0.04212 -0.0712 1.0000 0.0060
-16.000 -1.0766 0.04308 0.03876 -0.0716 1.0000 0.0059
-15.750 -1.0763 0.04071 0.03631 -0.0715 1.0000 0.0060
-15.500 -1.0776 0.03830 0.03380 -0.0713 1.0000 0.0061
-15.250 -1.0770 0.03616 0.03157 -0.0708 1.0000 0.0061
-15.000 -1.0720 0.03452 0.02986 -0.0701 1.0000 0.0061
-14.750 -1.0733 0.03243 0.02768 -0.0692 1.0000 0.0061
-14.500 -1.0697 0.03084 0.02602 -0.0680 1.0000 0.0061
-14.250 -1.0652 0.02942 0.02453 -0.0668 1.0000 0.0062
-14.000 -1.0646 0.02780 0.02283 -0.0650 1.0000 0.0061
-13.750 -1.0644 0.02627 0.02122 -0.0630 1.0000 0.0063
-13.500 -1.0591 0.02519 0.02007 -0.0610 1.0000 0.0063
-13.250 -1.0576 0.02396 0.01878 -0.0584 1.0000 0.0065
-13.000 -1.0503 0.02290 0.01766 -0.0565 0.9997 0.0066
-12.750 -1.0266 0.02192 0.01661 -0.0576 0.9981 0.0066
-12.500 -1.0023 0.02106 0.01572 -0.0585 0.9960 0.0069
-12.250 -0.9789 0.02021 0.01481 -0.0591 0.9934 0.0068
-12.000 -0.9593 0.01945 0.01401 -0.0587 0.9893 0.0070
-11.750 -0.9376 0.01879 0.01330 -0.0585 0.9833 0.0071
-11.500 -0.9336 0.01821 0.01267 -0.0546 0.9617 0.0072
-11.250 -0.8951 0.01742 0.01184 -0.0577 0.9485 0.0074
-11.000 -0.8422 0.01660 0.01095 -0.0638 0.9386 0.0076
-10.750 -0.7776 0.01575 0.01003 -0.0725 0.9277 0.0079
-10.500 -0.7179 0.01506 0.00920 -0.0801 0.8986 0.0082
-10.250 -0.6963 0.01472 0.00867 -0.0794 0.8599 0.0084
-10.000 -0.6833 0.01440 0.00823 -0.0768 0.8340 0.0088
-9.750 -0.6696 0.01411 0.00784 -0.0743 0.8152 0.0088
-9.500 -0.6553 0.01382 0.00747 -0.0719 0.7994 0.0091
-9.250 -0.6405 0.01355 0.00712 -0.0695 0.7862 0.0096
-9.000 -0.6251 0.01333 0.00683 -0.0672 0.7743 0.0099
-8.750 -0.6090 0.01311 0.00655 -0.0650 0.7639 0.0103
-8.500 -0.5920 0.01286 0.00624 -0.0630 0.7552 0.0108
-8.250 -0.5731 0.01261 0.00596 -0.0614 0.7463 0.0113
-8.000 -0.5537 0.01237 0.00568 -0.0599 0.7387 0.0122
-7.500 -0.5133 0.01192 0.00516 -0.0570 0.7241 0.0146
-7.250 -0.4917 0.01170 0.00492 -0.0559 0.7177 0.0160
-7.000 -0.4708 0.01148 0.00468 -0.0546 0.7110 0.0183
-6.750 -0.4493 0.01127 0.00445 -0.0534 0.7048 0.0207
-6.500 -0.4268 0.01108 0.00424 -0.0523 0.6991 0.0231
-6.250 -0.4048 0.01089 0.00403 -0.0512 0.6927 0.0263
-6.000 -0.3824 0.01069 0.00384 -0.0502 0.6875 0.0299
-5.750 -0.3596 0.01049 0.00365 -0.0492 0.6818 0.0348
-5.500 -0.3369 0.01031 0.00346 -0.0482 0.6765 0.0411
-5.250 -0.3142 0.01013 0.00329 -0.0472 0.6718 0.0487
-4.750 -0.2682 0.00971 0.00296 -0.0453 0.6621 0.0709
-4.500 -0.2460 0.00949 0.00280 -0.0443 0.6569 0.0887
-4.250 -0.2233 0.00927 0.00264 -0.0433 0.6526 0.1076
-4.000 -0.2007 0.00902 0.00249 -0.0423 0.6481 0.1338
-3.250 -0.1350 0.00824 0.00206 -0.0389 0.6341 0.2403
-3.000 -0.1144 0.00789 0.00191 -0.0375 0.6293 0.2958
-2.750 -0.0938 0.00757 0.00178 -0.0361 0.6244 0.3528
-2.500 -0.0718 0.00733 0.00168 -0.0350 0.6197 0.3988
-2.250 -0.0486 0.00712 0.00159 -0.0340 0.6146 0.4392
-2.000 -0.0254 0.00696 0.00153 -0.0331 0.6091 0.4770
-1.750 -0.0025 0.00681 0.00148 -0.0320 0.6039 0.5150
-1.500 0.0221 0.00670 0.00146 -0.0313 0.5992 0.5463
-1.250 0.0474 0.00665 0.00144 -0.0307 0.5939 0.5661
-1.000 0.0728 0.00663 0.00143 -0.0302 0.5885 0.5823
-0.750 0.0989 0.00660 0.00143 -0.0297 0.5839 0.5989
-0.500 0.1250 0.00658 0.00143 -0.0293 0.5785 0.6135
-0.250 0.1506 0.00658 0.00143 -0.0288 0.5729 0.6237
0.000 0.1774 0.00659 0.00143 -0.0285 0.5676 0.6318
0.250 0.2035 0.00659 0.00144 -0.0281 0.5612 0.6398
0.500 0.2296 0.00664 0.00145 -0.0277 0.5544 0.6464
0.750 0.2563 0.00664 0.00146 -0.0274 0.5480 0.6522
1.000 0.2823 0.00667 0.00148 -0.0270 0.5407 0.6585
1.250 0.3088 0.00671 0.00150 -0.0267 0.5340 0.6644
1.500 0.3345 0.00674 0.00152 -0.0262 0.5252 0.6704
1.750 0.3601 0.00678 0.00155 -0.0257 0.5159 0.6776
2.000 0.3852 0.00686 0.00159 -0.0252 0.5039 0.6838
2.250 0.4099 0.00692 0.00163 -0.0245 0.4909 0.6901
2.500 0.4349 0.00699 0.00168 -0.0239 0.4781 0.6966
2.750 0.4598 0.00708 0.00174 -0.0233 0.4670 0.7022
3.000 0.4837 0.00717 0.00181 -0.0225 0.4542 0.7089
3.500 0.5313 0.00738 0.00197 -0.0209 0.4257 0.7227
3.750 0.5547 0.00750 0.00206 -0.0200 0.4108 0.7305
4.000 0.5760 0.00769 0.00218 -0.0188 0.3883 0.7385
4.250 0.5966 0.00789 0.00231 -0.0174 0.3654 0.7474
4.500 0.6158 0.00815 0.00248 -0.0158 0.3390 0.7563
4.750 0.6352 0.00837 0.00264 -0.0141 0.3159 0.7666
5.000 0.6545 0.00858 0.00281 -0.0125 0.2964 0.7770
5.500 0.6920 0.00899 0.00316 -0.0090 0.2617 0.8019
5.750 0.7089 0.00918 0.00333 -0.0069 0.2459 0.8161
6.000 0.7237 0.00936 0.00351 -0.0044 0.2295 0.8338
6.250 0.7388 0.00955 0.00371 -0.0019 0.2151 0.8556
6.500 0.7555 0.00975 0.00396 0.0002 0.2000 0.8855
6.750 0.7900 0.01006 0.00430 -0.0017 0.1842 0.9186
7.000 0.8443 0.01053 0.00474 -0.0081 0.1675 0.9361
7.250 0.8996 0.01105 0.00518 -0.0147 0.1505 0.9453
7.500 0.9471 0.01153 0.00561 -0.0195 0.1387 0.9557
7.750 0.9745 0.01191 0.00595 -0.0199 0.1299 0.9743
8.000 0.9912 0.01221 0.00623 -0.0180 0.1236 0.9872
8.250 1.0148 0.01258 0.00657 -0.0176 0.1165 0.9928
8.500 1.0432 0.01293 0.00690 -0.0183 0.1103 0.9961
8.750 1.0722 0.01335 0.00728 -0.0193 0.1029 0.9986
9.000 1.0991 0.01372 0.00764 -0.0197 0.0969 1.0000
9.250 1.1086 0.01407 0.00797 -0.0166 0.0922 1.0000
9.500 1.1189 0.01443 0.00832 -0.0136 0.0881 1.0000
9.750 1.1312 0.01477 0.00868 -0.0111 0.0855 1.0000
10.000 1.1424 0.01518 0.00909 -0.0085 0.0820 1.0000
10.250 1.1530 0.01566 0.00956 -0.0059 0.0784 1.0000
10.500 1.1659 0.01610 0.01002 -0.0038 0.0764 1.0000
10.750 1.1786 0.01657 0.01052 -0.0017 0.0743 1.0000
11.000 1.1905 0.01712 0.01108 0.0003 0.0720 1.0000
11.250 1.2018 0.01775 0.01171 0.0024 0.0697 1.0000
11.500 1.2137 0.01839 0.01237 0.0042 0.0674 1.0000
11.750 1.2265 0.01901 0.01303 0.0058 0.0656 1.0000
12.000 1.2388 0.01971 0.01376 0.0074 0.0638 1.0000
12.250 1.2499 0.02052 0.01458 0.0090 0.0617 1.0000
12.500 1.2609 0.02137 0.01545 0.0105 0.0599 1.0000
12.750 1.2723 0.02223 0.01634 0.0118 0.0583 1.0000
13.000 1.2846 0.02308 0.01724 0.0130 0.0571 1.0000
13.250 1.2956 0.02405 0.01823 0.0142 0.0547 1.0000
13.500 1.3051 0.02513 0.01933 0.0154 0.0526 1.0000
13.750 1.3145 0.02627 0.02049 0.0166 0.0509 1.0000
14.000 1.3253 0.02733 0.02160 0.0176 0.0496 1.0000
14.250 1.3355 0.02848 0.02279 0.0185 0.0485 1.0000
14.500 1.3437 0.02978 0.02411 0.0195 0.0461 1.0000
14.750 1.3507 0.03121 0.02556 0.0205 0.0442 1.0000
15.000 1.3589 0.03257 0.02697 0.0213 0.0428 1.0000
15.250 1.3671 0.03398 0.02842 0.0220 0.0414 1.0000
15.500 1.3732 0.03557 0.03004 0.0228 0.0393 1.0000
15.750 1.3776 0.03736 0.03185 0.0235 0.0374 1.0000
16.000 1.3847 0.03897 0.03352 0.0240 0.0370 1.0000
16.250 1.3905 0.04071 0.03530 0.0245 0.0352 1.0000
16.500 1.3957 0.04255 0.03719 0.0250 0.0343 1.0000
16.750 1.3984 0.04466 0.03934 0.0254 0.0328 1.0000
17.000 1.4018 0.04677 0.04149 0.0257 0.0320 1.0000
17.250 1.4063 0.04881 0.04359 0.0259 0.0310 1.0000
17.500 1.4083 0.05114 0.04597 0.0260 0.0294 1.0000
17.750 1.4109 0.05344 0.04834 0.0260 0.0290 1.0000
18.000 1.4113 0.05602 0.05097 0.0260 0.0279 1.0000
18.250 1.4111 0.05871 0.05371 0.0259 0.0268 1.0000
18.500 1.4117 0.06139 0.05645 0.0256 0.0260 1.0000
18.750 1.4120 0.06414 0.05928 0.0253 0.0256 1.0000
19.000 1.4102 0.06715 0.06235 0.0249 0.0247 1.0000
19.250 1.4063 0.07048 0.06575 0.0243 0.0239 1.0000
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