PW106 (pw106-pw) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: PW106 (pw106-pw) Reynolds number: 500,000 Max Cl/Cd: 74.45 at α=4.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-pw106-pw-500000.txt Download as CSV file: xf-pw106-pw-500000.csv |
XFOIL Version 6.96
Calculated polar for: PW106
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
------ -------- --------- --------- -------- -------- --------
-20.000 -0.8671 0.26904 0.26668 0.1081 1.0000 0.0070
-19.750 -0.8580 0.26587 0.26351 0.1058 1.0000 0.0070
-19.500 -0.8490 0.26269 0.26033 0.1037 1.0000 0.0070
-19.250 -0.8400 0.25948 0.25713 0.1015 1.0000 0.0070
-19.000 -0.8310 0.25626 0.25391 0.0994 1.0000 0.0070
-18.750 -0.8220 0.25302 0.25067 0.0972 1.0000 0.0070
-18.500 -0.8130 0.24975 0.24740 0.0951 1.0000 0.0070
-18.250 -0.8041 0.24646 0.24412 0.0930 1.0000 0.0070
-18.000 -0.7952 0.24315 0.24081 0.0909 1.0000 0.0071
-17.750 -0.7863 0.23980 0.23746 0.0889 1.0000 0.0071
-17.500 -0.7775 0.23644 0.23411 0.0868 1.0000 0.0071
-17.250 -0.7687 0.23307 0.23074 0.0848 1.0000 0.0071
-17.000 -0.7600 0.22967 0.22735 0.0828 1.0000 0.0071
-16.750 -0.7512 0.22623 0.22391 0.0808 1.0000 0.0071
-16.500 -0.7426 0.22274 0.22042 0.0788 1.0000 0.0071
-16.250 -0.7340 0.21923 0.21692 0.0768 1.0000 0.0071
-16.000 -0.7255 0.21571 0.21340 0.0749 1.0000 0.0071
-15.750 -0.7171 0.21215 0.20985 0.0730 1.0000 0.0071
-15.500 -0.7088 0.20855 0.20626 0.0711 1.0000 0.0071
-15.250 -0.7007 0.20494 0.20265 0.0692 1.0000 0.0071
-15.000 -0.6926 0.20128 0.19897 0.0674 1.0000 0.0071
-14.750 -0.6849 0.19761 0.19531 0.0656 1.0000 0.0071
-14.500 -0.6772 0.19393 0.19163 0.0638 1.0000 0.0071
-14.250 -0.6695 0.19019 0.18790 0.0620 1.0000 0.0071
-14.000 -0.6622 0.18640 0.18412 0.0603 1.0000 0.0071
-13.750 -0.6550 0.18261 0.18033 0.0585 1.0000 0.0071
-13.500 -0.6480 0.17876 0.17650 0.0569 1.0000 0.0071
-13.250 -0.6414 0.17489 0.17263 0.0552 1.0000 0.0071
-13.000 -0.6350 0.17093 0.16868 0.0535 1.0000 0.0071
-12.750 -0.6288 0.16694 0.16470 0.0519 1.0000 0.0071
-12.500 -0.6229 0.16288 0.16065 0.0503 1.0000 0.0071
-12.250 -0.6175 0.15873 0.15651 0.0488 1.0000 0.0071
-12.000 -0.6130 0.15433 0.15212 0.0473 1.0000 0.0070
-11.750 -0.6126 0.14877 0.14658 0.0458 1.0000 0.0065
-11.500 -0.6102 0.14411 0.14193 0.0442 1.0000 0.0062
-11.250 -0.6076 0.13959 0.13743 0.0426 1.0000 0.0060
-11.000 -0.6050 0.13507 0.13291 0.0408 1.0000 0.0059
-10.750 -0.6028 0.13050 0.12836 0.0391 1.0000 0.0058
-10.500 -0.6009 0.12588 0.12376 0.0372 1.0000 0.0057
-10.250 -0.5995 0.12115 0.11905 0.0353 1.0000 0.0057
-10.000 -0.5984 0.11639 0.11430 0.0332 1.0000 0.0057
-9.750 -0.5980 0.11143 0.10936 0.0310 1.0000 0.0057
-9.500 -0.5978 0.10646 0.10442 0.0287 1.0000 0.0058
-9.250 -0.5979 0.10145 0.09943 0.0262 1.0000 0.0059
-9.000 -0.5980 0.09649 0.09449 0.0235 1.0000 0.0061
-8.750 -0.5976 0.09164 0.08967 0.0206 1.0000 0.0063
-8.500 -0.5972 0.08681 0.08486 0.0174 1.0000 0.0064
-8.250 -0.5965 0.08195 0.08003 0.0134 1.0000 0.0066
-8.000 -0.5974 0.07610 0.07420 0.0068 1.0000 0.0066
-7.500 -0.5353 0.05077 0.04888 -0.0119 1.0000 0.0079
-7.250 -0.5440 0.04118 0.03909 -0.0162 1.0000 0.0083
-7.000 -0.5287 0.04035 0.03822 -0.0169 1.0000 0.0096
-6.750 -0.5073 0.04087 0.03876 -0.0170 1.0000 0.0114
-6.500 -0.4879 0.03883 0.03665 -0.0179 1.0000 0.0154
-6.250 -0.4788 0.03259 0.03016 -0.0192 1.0000 0.0149
-6.000 -0.4681 0.02630 0.02355 -0.0197 1.0000 0.0137
-5.750 -0.4526 0.02162 0.01853 -0.0197 1.0000 0.0135
-5.500 -0.4365 0.01696 0.01342 -0.0190 1.0000 0.0126
-5.250 -0.4131 0.01095 0.00659 -0.0190 0.9799 0.0107
-5.000 -0.3880 0.00806 0.00304 -0.0184 0.9601 0.0095
-4.750 -0.3657 0.00707 0.00178 -0.0171 0.9378 0.0093
-4.500 -0.3451 0.00638 0.00087 -0.0153 0.9159 0.0090
-4.250 -0.3232 0.00583 0.00012 -0.0138 0.8953 0.0089
-3.750 -0.2805 0.01340 0.00721 -0.0118 0.8791 0.0087
-3.500 -0.2561 0.01275 0.00640 -0.0108 0.8581 0.0087
-3.250 -0.2311 0.01214 0.00565 -0.0099 0.8373 0.0088
-3.000 -0.2054 0.01158 0.00496 -0.0092 0.8167 0.0090
-2.750 -0.1794 0.01109 0.00434 -0.0085 0.7966 0.0093
-2.500 -0.1529 0.01066 0.00380 -0.0080 0.7765 0.0097
-2.250 -0.1262 0.01031 0.00333 -0.0076 0.7574 0.0101
-2.000 -0.0989 0.01020 0.00321 -0.0074 0.7382 0.0135
-1.750 -0.0715 0.00995 0.00282 -0.0071 0.7200 0.0147
-1.500 -0.0440 0.00967 0.00240 -0.0068 0.7024 0.0144
-1.250 -0.0161 0.00948 0.00209 -0.0065 0.6849 0.0142
-1.000 0.0119 0.00937 0.00185 -0.0063 0.6680 0.0142
-0.750 0.0400 0.00931 0.00167 -0.0061 0.6517 0.0145
-0.500 0.0682 0.00926 0.00153 -0.0060 0.6352 0.0151
-0.250 0.0964 0.00923 0.00143 -0.0059 0.6190 0.0165
0.000 0.1235 0.00884 0.00134 -0.0058 0.6033 0.1207
0.250 0.1478 0.00783 0.00128 -0.0058 0.5885 0.4221
0.500 0.1600 0.00626 0.00141 -0.0020 0.5752 0.9097
0.750 0.2346 0.00641 0.00154 -0.0115 0.5538 1.0000
1.000 0.2616 0.00648 0.00153 -0.0113 0.5384 1.0000
1.250 0.2885 0.00657 0.00153 -0.0111 0.5231 1.0000
1.500 0.3154 0.00667 0.00154 -0.0109 0.5081 1.0000
1.750 0.3422 0.00676 0.00156 -0.0107 0.4932 1.0000
2.000 0.3690 0.00686 0.00158 -0.0105 0.4781 1.0000
2.250 0.3958 0.00697 0.00162 -0.0102 0.4630 1.0000
2.500 0.4225 0.00709 0.00168 -0.0100 0.4481 1.0000
2.750 0.4492 0.00722 0.00174 -0.0098 0.4331 1.0000
3.000 0.4759 0.00736 0.00181 -0.0096 0.4183 1.0000
3.250 0.5025 0.00751 0.00188 -0.0094 0.4033 1.0000
3.500 0.5291 0.00766 0.00197 -0.0091 0.3886 1.0000
3.750 0.5558 0.00781 0.00207 -0.0089 0.3739 1.0000
4.000 0.5825 0.00798 0.00222 -0.0088 0.3595 1.0000
4.250 0.6090 0.00818 0.00232 -0.0086 0.3381 1.0000
4.500 0.6337 0.00877 0.00242 -0.0085 0.2569 1.0000
4.750 0.6595 0.00917 0.00259 -0.0084 0.2187 1.0000
5.000 0.6855 0.00952 0.00279 -0.0083 0.1903 1.0000
5.250 0.7114 0.00990 0.00301 -0.0082 0.1630 1.0000
5.500 0.7374 0.01028 0.00326 -0.0080 0.1398 1.0000
5.750 0.7622 0.01090 0.00363 -0.0079 0.1001 1.0000
6.000 0.7867 0.01160 0.00409 -0.0078 0.0614 1.0000
6.250 0.8114 0.01223 0.00456 -0.0076 0.0334 1.0000
6.500 0.8371 0.01263 0.00493 -0.0075 0.0243 1.0000
6.750 0.8633 0.01291 0.00522 -0.0073 0.0223 1.0000
7.000 0.8877 0.01360 0.00597 -0.0071 0.0037 1.0000
7.250 0.9137 0.01391 0.00632 -0.0069 0.0030 1.0000
7.500 0.9395 0.01424 0.00670 -0.0068 0.0028 1.0000
7.750 0.9651 0.01463 0.00713 -0.0066 0.0027 1.0000
8.000 0.9904 0.01505 0.00762 -0.0064 0.0027 1.0000
8.250 1.0155 0.01551 0.00816 -0.0061 0.0027 1.0000
8.500 1.0403 0.01601 0.00876 -0.0059 0.0027 1.0000
8.750 1.0646 0.01657 0.00944 -0.0056 0.0027 1.0000
9.000 1.0884 0.01720 0.01019 -0.0052 0.0027 1.0000
9.250 1.1115 0.01792 0.01106 -0.0048 0.0027 1.0000
9.500 1.1336 0.01876 0.01204 -0.0044 0.0028 1.0000
9.750 1.1546 0.01972 0.01323 -0.0038 0.0028 1.0000
10.000 1.1742 0.02081 0.01447 -0.0032 0.0029 1.0000
10.250 1.1924 0.02199 0.01581 -0.0025 0.0030 1.0000
10.500 1.2091 0.02328 0.01726 -0.0018 0.0030 1.0000
10.750 1.2239 0.02468 0.01881 -0.0009 0.0031 1.0000
11.000 1.2365 0.02620 0.02049 0.0000 0.0031 1.0000
11.250 1.2463 0.02787 0.02231 0.0011 0.0032 1.0000
11.500 1.2509 0.02968 0.02428 0.0024 0.0033 1.0000
11.750 1.2526 0.03187 0.02663 0.0031 0.0033 1.0000
12.000 1.2531 0.03451 0.02943 0.0030 0.0034 1.0000
12.250 1.2524 0.03761 0.03269 0.0023 0.0034 1.0000
12.500 1.2503 0.04113 0.03638 0.0011 0.0035 1.0000
12.750 1.2465 0.04504 0.04046 -0.0005 0.0035 1.0000
13.000 1.2410 0.04934 0.04492 -0.0023 0.0036 1.0000
13.250 1.2338 0.05397 0.04971 -0.0044 0.0036 1.0000
13.500 1.2249 0.05893 0.05483 -0.0066 0.0037 1.0000
13.750 1.2144 0.06421 0.06026 -0.0090 0.0037 1.0000
14.000 1.2027 0.06976 0.06596 -0.0115 0.0038 1.0000
14.250 1.1899 0.07559 0.07193 -0.0142 0.0038 1.0000
14.500 1.1764 0.08166 0.07814 -0.0171 0.0038 1.0000
14.750 1.1623 0.08810 0.08471 -0.0202 0.0039 1.0000
15.000 1.1483 0.09477 0.09151 -0.0234 0.0039 1.0000
15.250 1.1338 0.10173 0.09860 -0.0269 0.0039 1.0000
15.500 1.1193 0.10888 0.10588 -0.0304 0.0039 1.0000
15.750 1.1044 0.11634 0.11345 -0.0342 0.0039 1.0000
16.000 1.0896 0.12395 0.12118 -0.0380 0.0039 1.0000
16.250 1.0753 0.13173 0.12906 -0.0420 0.0039 1.0000
16.500 1.0607 0.13984 0.13727 -0.0462 0.0040 1.0000
16.750 1.0463 0.14817 0.14571 -0.0506 0.0040 1.0000
17.000 1.0319 0.15695 0.15457 -0.0552 0.0040 1.0000
17.250 1.0180 0.16600 0.16371 -0.0601 0.0040 1.0000
17.500 1.0030 0.17588 0.17366 -0.0653 0.0040 1.0000
17.750 0.9821 0.18869 0.18654 -0.0719 0.0040 1.0000
18.000 0.9454 0.21153 0.20934 -0.0816 0.0046 1.0000
18.250 0.9435 0.22053 0.21830 -0.0856 0.0051 1.0000
18.500 0.9466 0.22688 0.22463 -0.0888 0.0056 1.0000
18.750 0.9515 0.23228 0.23001 -0.0915 0.0060 1.0000
19.000 0.9570 0.23720 0.23492 -0.0942 0.0066 1.0000
19.250 0.9628 0.24178 0.23950 -0.0967 0.0071 1.0000
19.500 0.9708 0.24402 0.24177 -0.0978 0.0087 1.0000
19.750 0.9796 0.24849 0.24623 -0.1003 0.0092 1.0000
20.000 0.9867 0.25288 0.25062 -0.1029 0.0093 1.0000
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