S4062-095-87 (s4062-il) Xfoil prediction polar at RE=200,000 Ncrit=9
| Details | Polar file |
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Airfoil: S4062-095-87 (s4062-il) Reynolds number: 200,000 Max Cl/Cd: 90.45 at α=6° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-s4062-il-200000.txt Download as CSV file: xf-s4062-il-200000.csv |
XFOIL Version 6.96
Calculated polar for: S4062-095-87
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.200 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-9.500 -0.3310 0.10736 0.10406 -0.0453 1.0000 0.0397
-9.250 -0.3485 0.10695 0.10375 -0.0411 1.0000 0.0397
-9.000 -0.3621 0.10590 0.10276 -0.0390 0.9995 0.0398
-8.750 -0.3453 0.10035 0.09720 -0.0367 0.9984 0.0415
-8.500 -0.3248 0.09695 0.09378 -0.0391 0.9954 0.0437
-8.250 -0.3088 0.09300 0.08982 -0.0438 0.9910 0.0464
-8.000 -0.2938 0.08832 0.08516 -0.0529 0.9854 0.0493
-7.750 -0.2793 0.08249 0.07934 -0.0700 0.9743 0.0506
-7.500 -0.2639 0.07598 0.07284 -0.0740 0.9720 0.0516
-7.250 -0.2472 0.07347 0.07033 -0.0726 0.9678 0.0530
-7.000 -0.2250 0.06987 0.06670 -0.0769 0.9632 0.0551
-6.750 -0.1974 0.06460 0.06139 -0.0866 0.9592 0.0586
-6.500 -0.1785 0.05391 0.05030 -0.1074 0.9466 0.0637
-6.250 -0.1549 0.05098 0.04746 -0.1079 0.9443 0.0652
-6.000 -0.1420 0.04879 0.04525 -0.1077 0.9360 0.0669
-5.750 -0.1311 0.03375 0.02902 -0.1158 0.9263 0.0414
-5.500 -0.1128 0.02700 0.02121 -0.1157 0.9195 0.0313
-5.250 -0.0838 0.02497 0.01872 -0.1161 0.9161 0.0308
-5.000 -0.0637 0.02290 0.01628 -0.1152 0.9093 0.0309
-4.750 -0.0386 0.02076 0.01394 -0.1152 0.9049 0.0334
-4.500 -0.0094 0.01972 0.01272 -0.1153 0.9017 0.0361
-4.250 0.0137 0.01868 0.01149 -0.1143 0.8955 0.0378
-4.000 0.0403 0.01756 0.01021 -0.1138 0.8909 0.0405
-3.750 0.0680 0.01660 0.00924 -0.1136 0.8876 0.0483
-3.500 0.0918 0.01588 0.00853 -0.1129 0.8819 0.0651
-3.250 0.1178 0.01530 0.00805 -0.1126 0.8769 0.1007
-3.000 0.1458 0.01490 0.00774 -0.1125 0.8734 0.1398
-2.750 0.1712 0.01466 0.00757 -0.1122 0.8685 0.1779
-2.500 0.1967 0.01439 0.00742 -0.1119 0.8631 0.2204
-2.250 0.2240 0.01401 0.00722 -0.1118 0.8594 0.2736
-2.000 0.2504 0.01369 0.00711 -0.1115 0.8556 0.3428
-1.750 0.2739 0.01344 0.00717 -0.1109 0.8493 0.4311
-1.250 0.3207 0.01243 0.00707 -0.1082 0.8424 0.7108
-1.000 0.3553 0.01201 0.00710 -0.1087 0.8370 0.9576
-0.750 0.3895 0.01202 0.00695 -0.1100 0.8325 1.0000
-0.500 0.4172 0.01201 0.00680 -0.1097 0.8290 1.0000
-0.250 0.4424 0.01220 0.00688 -0.1093 0.8231 1.0000
0.000 0.4689 0.01228 0.00686 -0.1090 0.8177 1.0000
0.250 0.4971 0.01224 0.00672 -0.1087 0.8141 1.0000
0.500 0.5222 0.01242 0.00685 -0.1083 0.8075 1.0000
0.750 0.5494 0.01242 0.00677 -0.1079 0.8021 1.0000
1.000 0.5783 0.01230 0.00655 -0.1076 0.7983 1.0000
1.250 0.6028 0.01242 0.00666 -0.1070 0.7895 1.0000
1.500 0.6316 0.01224 0.00640 -0.1065 0.7846 1.0000
1.750 0.6567 0.01231 0.00645 -0.1059 0.7758 1.0000
2.000 0.6854 0.01212 0.00620 -0.1055 0.7702 1.0000
2.250 0.7108 0.01219 0.00627 -0.1050 0.7616 1.0000
2.500 0.7394 0.01205 0.00610 -0.1046 0.7558 1.0000
2.750 0.7650 0.01212 0.00618 -0.1041 0.7470 1.0000
3.000 0.7937 0.01198 0.00599 -0.1037 0.7408 1.0000
3.250 0.8192 0.01203 0.00609 -0.1032 0.7311 1.0000
3.500 0.8469 0.01196 0.00601 -0.1028 0.7234 1.0000
3.750 0.8736 0.01192 0.00598 -0.1023 0.7137 1.0000
4.000 0.8997 0.01192 0.00601 -0.1017 0.7032 1.0000
4.250 0.9266 0.01187 0.00599 -0.1012 0.6927 1.0000
4.500 0.9535 0.01180 0.00593 -0.1007 0.6813 1.0000
4.750 0.9796 0.01178 0.00592 -0.1000 0.6679 1.0000
5.000 1.0049 0.01179 0.00598 -0.0993 0.6525 1.0000
5.250 1.0296 0.01183 0.00607 -0.0985 0.6343 1.0000
5.500 1.0542 0.01188 0.00613 -0.0977 0.6135 1.0000
5.750 1.0781 0.01199 0.00624 -0.0967 0.5888 1.0000
6.000 1.1008 0.01217 0.00639 -0.0955 0.5573 1.0000
6.250 1.1216 0.01249 0.00658 -0.0941 0.5158 1.0000
6.500 1.1393 0.01304 0.00689 -0.0923 0.4645 1.0000
6.750 1.1546 0.01380 0.00737 -0.0902 0.4106 1.0000
7.000 1.1686 0.01468 0.00800 -0.0880 0.3641 1.0000
7.250 1.1833 0.01552 0.00867 -0.0861 0.3254 1.0000
7.500 1.1979 0.01636 0.00936 -0.0842 0.2934 1.0000
7.750 1.2124 0.01719 0.01008 -0.0823 0.2648 1.0000
8.000 1.2263 0.01802 0.01082 -0.0803 0.2383 1.0000
8.250 1.2392 0.01887 0.01159 -0.0783 0.2126 1.0000
8.500 1.2493 0.01974 0.01236 -0.0758 0.1883 1.0000
8.750 1.2591 0.02064 0.01316 -0.0734 0.1640 1.0000
9.000 1.2695 0.02157 0.01404 -0.0711 0.1422 1.0000
9.250 1.2786 0.02266 0.01504 -0.0689 0.1231 1.0000
9.500 1.2878 0.02380 0.01614 -0.0667 0.1050 1.0000
9.750 1.2963 0.02505 0.01736 -0.0646 0.0880 1.0000
10.000 1.3026 0.02650 0.01874 -0.0624 0.0731 1.0000
10.250 1.3061 0.02827 0.02044 -0.0600 0.0601 1.0000
10.500 1.3094 0.03014 0.02232 -0.0576 0.0500 1.0000
10.750 1.3129 0.03209 0.02435 -0.0554 0.0435 1.0000
11.000 1.3153 0.03418 0.02642 -0.0534 0.0392 1.0000
11.250 1.3214 0.03611 0.02847 -0.0516 0.0362 1.0000
11.500 1.3291 0.03790 0.03037 -0.0500 0.0336 1.0000
11.750 1.3359 0.03986 0.03238 -0.0486 0.0318 1.0000
12.000 1.3434 0.04244 0.03499 -0.0470 0.0299 1.0000
12.250 1.3551 0.04452 0.03724 -0.0457 0.0288 1.0000
12.500 1.3645 0.04652 0.03943 -0.0444 0.0276 1.0000
12.750 1.3725 0.04867 0.04176 -0.0433 0.0264 1.0000
13.000 1.3782 0.05091 0.04414 -0.0423 0.0252 1.0000
13.250 1.3841 0.05340 0.04678 -0.0413 0.0244 1.0000
13.500 1.3897 0.05615 0.04966 -0.0404 0.0238 1.0000
13.750 1.3947 0.05949 0.05317 -0.0395 0.0231 1.0000
14.000 1.3939 0.06391 0.05785 -0.0387 0.0227 1.0000
14.250 1.3837 0.06914 0.06338 -0.0381 0.0224 1.0000
14.500 1.3718 0.07328 0.06779 -0.0380 0.0223 1.0000
14.750 1.3583 0.07781 0.07261 -0.0384 0.0222 1.0000
15.000 1.3431 0.08284 0.07789 -0.0393 0.0220 1.0000
15.250 1.3264 0.08853 0.08384 -0.0409 0.0220 1.0000
15.500 1.3087 0.09465 0.09021 -0.0432 0.0218 1.0000
15.750 1.2896 0.10158 0.09736 -0.0463 0.0219 1.0000
16.000 1.2700 0.10904 0.10504 -0.0502 0.0219 1.0000
16.250 1.2492 0.11731 0.11349 -0.0548 0.0220 1.0000
16.500 1.2281 0.12625 0.12262 -0.0602 0.0222 1.0000
16.750 1.2062 0.13602 0.13253 -0.0662 0.0224 1.0000
17.000 1.1914 0.14477 0.14146 -0.0725 0.0227 1.0000
17.250 1.0785 0.19143 0.18831 -0.1019 0.0295 1.0000
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Polar data table (+)
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