; This is a polar exchange file (PEF) ; Comments start with a ';' in column 1, blank lines are allowed ; The 'PolarBrowser' application, a reader and converter is available ; in the software section at: ; http://www.MH-AeroTools.de/airfoils/ [Airfoil] Description1=MH 50 7.98% NumberSets=1 [Set1] Origin=PEFView Description1=XFLR Analysis, M=0.285 Description2=Copyright 2007 Martin Hepperle NumberPolars=5 [Set1-Polar1] ReynoldsNumber=500000 MachNumber=0.285 NumberPoints=38 Values=Alpha Cl Cd Cm TU TL Value01=-2.000 -0.238 0.00593 -0.0026 0.983 0.746 Value02=-1.750 -0.201 0.00583 -0.0040 0.979 0.787 Value03=-1.500 -0.165 0.00580 -0.0053 0.975 0.819 Value04=-1.250 -0.132 0.00581 -0.0057 0.969 0.845 Value05=-1.000 -0.100 0.00584 -0.0058 0.962 0.863 Value06=-0.750 -0.072 0.00589 -0.0050 0.955 0.880 Value07=-0.500 -0.048 0.00593 -0.0035 0.945 0.894 Value08=-0.250 -0.024 0.00595 -0.0016 0.935 0.906 Value09=0.000 -0.002 0.00595 0.0005 0.925 0.917 Value10=0.250 0.021 0.00595 0.0025 0.913 0.927 Value11=0.500 0.043 0.00591 0.0045 0.900 0.937 Value12=0.750 0.067 0.00587 0.0063 0.885 0.946 Value13=1.000 0.092 0.00582 0.0077 0.867 0.954 Value14=1.250 0.119 0.00578 0.0087 0.845 0.961 Value15=1.500 0.150 0.00578 0.0089 0.817 0.968 Value16=1.750 0.182 0.00583 0.0086 0.784 0.973 Value17=2.000 0.216 0.00595 0.0079 0.740 0.977 Value18=2.250 0.251 0.00617 0.0068 0.681 0.980 Value19=2.500 0.285 0.00661 0.0056 0.574 0.984 Value20=2.750 0.320 0.00726 0.0041 0.436 0.987 Value21=3.000 0.354 0.00808 0.0024 0.286 0.990 Value22=3.250 0.389 0.00886 0.0006 0.163 0.992 Value23=3.500 0.424 0.00969 -0.0012 0.064 0.995 Value24=3.750 0.460 0.01039 -0.0029 0.036 0.997 Value25=4.000 0.497 0.01091 -0.0045 0.029 1.000 Value26=4.250 0.522 0.01148 -0.0039 0.026 1.000 Value27=4.500 0.544 0.01220 -0.0025 0.024 1.000 Value28=4.750 0.566 0.01274 -0.0011 0.022 1.000 Value29=5.000 0.586 0.01361 0.0005 0.020 1.000 Value30=5.250 0.607 0.01439 0.0023 0.019 1.000 Value31=5.500 0.627 0.01536 0.0042 0.019 1.000 Value32=5.750 0.648 0.01648 0.0061 0.018 1.000 Value33=6.000 0.668 0.01780 0.0080 0.017 1.000 Value34=6.250 0.687 0.01981 0.0097 0.017 1.000 Value35=6.500 0.708 0.02165 0.0115 0.016 1.000 Value36=6.750 0.726 0.02448 0.0132 0.016 1.000 Value37=7.000 0.742 0.02787 0.0148 0.017 1.000 Value38=7.250 0.757 0.03145 0.0159 0.017 1.000 [Set1-Polar2] ReynoldsNumber=750000 MachNumber=0.285 NumberPoints=38 Values=Alpha Cl Cd Cm TU TL Value01=-2.000 -0.205 0.00517 -0.0088 0.964 0.676 Value02=-1.750 -0.179 0.00501 -0.0078 0.957 0.718 Value03=-1.500 -0.154 0.00488 -0.0066 0.950 0.755 Value04=-1.250 -0.130 0.00478 -0.0053 0.943 0.788 Value05=-1.000 -0.105 0.00470 -0.0040 0.935 0.817 Value06=-0.750 -0.080 0.00466 -0.0027 0.926 0.839 Value07=-0.500 -0.054 0.00464 -0.0015 0.917 0.858 Value08=-0.250 -0.028 0.00463 -0.0005 0.907 0.874 Value09=0.000 -0.002 0.00462 0.0005 0.896 0.887 Value10=0.250 0.024 0.00461 0.0016 0.881 0.898 Value11=0.750 0.076 0.00464 0.0037 0.842 0.917 Value12=1.000 0.101 0.00469 0.0049 0.813 0.926 Value13=1.250 0.126 0.00479 0.0062 0.780 0.933 Value14=1.500 0.151 0.00491 0.0074 0.745 0.940 Value15=1.750 0.176 0.00507 0.0086 0.705 0.947 Value16=2.000 0.201 0.00526 0.0098 0.658 0.954 Value17=2.250 0.225 0.00554 0.0110 0.587 0.961 Value18=2.500 0.250 0.00601 0.0119 0.479 0.967 Value19=2.750 0.276 0.00653 0.0123 0.371 0.972 Value20=3.000 0.304 0.00713 0.0121 0.260 0.977 Value21=3.250 0.335 0.00771 0.0114 0.167 0.981 Value22=3.500 0.368 0.00827 0.0103 0.094 0.984 Value23=3.750 0.402 0.00889 0.0091 0.039 0.987 Value24=4.000 0.437 0.00937 0.0077 0.027 0.989 Value25=4.250 0.473 0.00983 0.0063 0.023 0.991 Value26=4.500 0.508 0.01039 0.0049 0.020 0.993 Value27=4.750 0.544 0.01086 0.0036 0.018 0.995 Value28=5.250 0.612 0.01238 0.0014 0.015 0.999 Value29=5.500 0.641 0.01320 0.0014 0.014 1.000 Value30=5.750 0.659 0.01451 0.0036 0.014 1.000 Value31=6.000 0.679 0.01529 0.0056 0.013 1.000 Value32=6.250 0.698 0.01641 0.0077 0.013 1.000 Value33=6.500 0.717 0.01791 0.0098 0.012 1.000 Value34=6.750 0.738 0.01978 0.0114 0.012 1.000 Value35=7.000 0.757 0.02222 0.0128 0.012 1.000 Value36=7.250 0.768 0.02723 0.0150 0.012 1.000 Value37=7.500 0.773 0.03340 0.0169 0.012 1.000 Value38=7.750 0.774 0.03922 0.0181 0.013 1.000 [Set1-Polar3] ReynoldsNumber=1000000 MachNumber=0.285 NumberPoints=42 Values=Alpha Cl Cd Cm TU TL Value01=-2.000 -0.210 0.00489 -0.0055 0.945 0.605 Value02=-1.750 -0.185 0.00464 -0.0045 0.938 0.664 Value03=-1.500 -0.159 0.00448 -0.0037 0.931 0.704 Value04=-1.250 -0.132 0.00432 -0.0029 0.924 0.741 Value05=-1.000 -0.106 0.00419 -0.0021 0.915 0.776 Value06=-0.750 -0.079 0.00408 -0.0013 0.906 0.806 Value07=-0.500 -0.052 0.00402 -0.0006 0.896 0.829 Value08=-0.250 -0.025 0.00398 0.0001 0.883 0.850 Value09=0.000 0.003 0.00397 0.0008 0.867 0.867 Value10=0.250 0.030 0.00399 0.0014 0.848 0.880 Value11=0.500 0.057 0.00404 0.0021 0.822 0.891 Value12=0.750 0.084 0.00414 0.0029 0.789 0.900 Value13=1.000 0.111 0.00427 0.0036 0.753 0.908 Value14=1.250 0.138 0.00442 0.0043 0.718 0.916 Value15=1.500 0.164 0.00459 0.0050 0.676 0.924 Value16=1.750 0.190 0.00480 0.0057 0.628 0.930 Value17=2.000 0.216 0.00512 0.0066 0.552 0.937 Value18=2.250 0.240 0.00560 0.0076 0.443 0.943 Value19=2.500 0.264 0.00607 0.0084 0.348 0.949 Value20=2.750 0.289 0.00656 0.0092 0.254 0.955 Value21=3.000 0.314 0.00701 0.0100 0.178 0.960 Value22=3.250 0.339 0.00742 0.0107 0.117 0.965 Value23=3.500 0.365 0.00781 0.0114 0.069 0.971 Value24=3.750 0.392 0.00826 0.0118 0.033 0.976 Value25=4.000 0.422 0.00861 0.0118 0.024 0.980 Value26=4.250 0.453 0.00899 0.0114 0.020 0.984 Value27=4.500 0.486 0.00932 0.0106 0.018 0.987 Value28=4.750 0.520 0.00979 0.0098 0.016 0.989 Value29=5.000 0.554 0.01029 0.0087 0.014 0.992 Value30=5.250 0.588 0.01103 0.0077 0.013 0.994 Value31=5.500 0.622 0.01173 0.0067 0.013 0.995 Value32=5.750 0.655 0.01249 0.0058 0.012 0.997 Value33=6.000 0.687 0.01375 0.0050 0.011 0.999 Value34=6.250 0.712 0.01473 0.0060 0.011 1.000 Value35=6.500 0.730 0.01593 0.0083 0.010 1.000 Value36=6.750 0.749 0.01753 0.0103 0.010 1.000 Value37=7.000 0.769 0.01970 0.0118 0.010 1.000 Value38=7.250 0.791 0.02163 0.0129 0.009 1.000 Value39=7.500 0.812 0.02320 0.0136 0.009 1.000 Value40=7.750 0.820 0.02775 0.0152 0.009 1.000 Value41=8.000 0.823 0.03313 0.0167 0.009 1.000 Value42=8.250 0.820 0.03880 0.0177 0.009 1.000 [Set1-Polar4] ReynoldsNumber=1500000 MachNumber=0.285 NumberPoints=47 Values=Alpha Cl Cd Cm TU TL Value01=-1.750 -0.197 0.00446 -0.0020 0.917 0.539 Value02=-1.500 -0.170 0.00416 -0.0016 0.910 0.610 Value03=-1.250 -0.142 0.00398 -0.0013 0.900 0.652 Value04=-1.000 -0.114 0.00382 -0.0010 0.891 0.690 Value05=-0.750 -0.086 0.00368 -0.0006 0.880 0.727 Value06=-0.500 -0.058 0.00356 -0.0002 0.864 0.763 Value07=-0.250 -0.031 0.00350 0.0003 0.843 0.791 Value08=0.000 -0.003 0.00348 0.0007 0.819 0.817 Value09=0.250 0.025 0.00352 0.0013 0.788 0.840 Value10=0.500 0.053 0.00363 0.0017 0.752 0.857 Value11=0.750 0.081 0.00376 0.0021 0.714 0.871 Value12=1.000 0.109 0.00389 0.0023 0.679 0.882 Value13=1.250 0.137 0.00406 0.0026 0.638 0.891 Value14=1.500 0.165 0.00426 0.0029 0.588 0.898 Value15=1.750 0.192 0.00455 0.0033 0.519 0.906 Value16=2.000 0.218 0.00504 0.0037 0.408 0.913 Value17=2.250 0.245 0.00546 0.0040 0.321 0.919 Value18=2.500 0.272 0.00589 0.0043 0.238 0.925 Value19=2.750 0.299 0.00628 0.0047 0.170 0.930 Value20=3.000 0.326 0.00664 0.0050 0.117 0.935 Value21=3.250 0.354 0.00697 0.0054 0.077 0.939 Value22=3.500 0.381 0.00734 0.0057 0.039 0.944 Value23=3.750 0.408 0.00764 0.0062 0.024 0.948 Value24=4.000 0.435 0.00789 0.0068 0.019 0.952 Value25=4.250 0.463 0.00815 0.0073 0.016 0.957 Value26=4.500 0.490 0.00839 0.0079 0.015 0.961 Value27=4.750 0.517 0.00872 0.0086 0.013 0.966 Value28=5.000 0.543 0.00900 0.0094 0.012 0.970 Value29=5.250 0.569 0.00943 0.0102 0.011 0.976 Value30=5.500 0.597 0.00990 0.0108 0.011 0.981 Value31=5.750 0.626 0.01038 0.0109 0.010 0.985 Value32=6.000 0.658 0.01086 0.0105 0.010 0.989 Value33=6.250 0.689 0.01172 0.0100 0.009 0.992 Value34=6.500 0.721 0.01284 0.0096 0.009 0.995 Value35=6.750 0.753 0.01389 0.0090 0.008 0.998 Value36=7.000 0.781 0.01522 0.0093 0.008 1.000 Value37=7.250 0.804 0.01641 0.0105 0.008 1.000 Value38=7.500 0.828 0.01752 0.0112 0.007 1.000 Value39=7.750 0.851 0.01922 0.0121 0.007 1.000 Value40=8.000 0.862 0.02339 0.0137 0.007 1.000 Value41=8.250 0.866 0.02889 0.0155 0.007 1.000 Value42=8.500 0.850 0.03783 0.0172 0.006 1.000 Value43=8.750 0.833 0.04626 0.0174 0.006 1.000 Value44=9.000 0.815 0.05319 0.0163 0.006 1.000 Value45=9.250 0.796 0.05941 0.0134 0.007 1.000 Value46=9.500 0.781 0.06943 0.0022 0.007 1.000 Value47=10.000 0.724 0.09572 -0.0159 0.008 1.000 [Set1-Polar5] ReynoldsNumber=2000000 MachNumber=0.285 NumberPoints=53 Values=Alpha Cl Cd Cm TU TL Value01=-2.000 -0.221 0.00489 -0.0013 0.907 0.344 Value02=-1.750 -0.194 0.00440 -0.0010 0.899 0.452 Value03=-1.500 -0.167 0.00401 -0.0007 0.889 0.545 Value04=-1.250 -0.139 0.00380 -0.0005 0.879 0.598 Value05=-1.000 -0.110 0.00366 -0.0003 0.866 0.637 Value06=-0.750 -0.082 0.00355 0.0000 0.846 0.675 Value07=-0.500 -0.054 0.00347 0.0003 0.820 0.713 Value08=-0.250 -0.026 0.00343 0.0006 0.792 0.747 Value09=0.000 0.002 0.00345 0.0008 0.760 0.774 Value10=0.250 0.030 0.00349 0.0012 0.723 0.803 Value11=0.500 0.058 0.00356 0.0014 0.685 0.829 Value12=0.750 0.086 0.00366 0.0017 0.650 0.847 Value13=1.000 0.115 0.00379 0.0018 0.610 0.862 Value14=1.250 0.143 0.00398 0.0020 0.558 0.874 Value15=1.500 0.171 0.00423 0.0022 0.497 0.883 Value16=1.750 0.198 0.00469 0.0024 0.389 0.891 Value17=2.000 0.226 0.00506 0.0026 0.308 0.898 Value18=2.250 0.254 0.00545 0.0027 0.232 0.905 Value19=2.500 0.282 0.00580 0.0029 0.170 0.911 Value20=2.750 0.309 0.00612 0.0031 0.120 0.916 Value21=3.000 0.338 0.00640 0.0033 0.083 0.921 Value22=3.250 0.366 0.00672 0.0035 0.048 0.926 Value23=3.500 0.394 0.00702 0.0037 0.026 0.930 Value24=3.750 0.422 0.00725 0.0040 0.019 0.934 Value25=4.250 0.479 0.00772 0.0046 0.014 0.942 Value26=4.500 0.508 0.00793 0.0049 0.013 0.945 Value27=4.750 0.536 0.00824 0.0053 0.011 0.949 Value28=5.000 0.564 0.00852 0.0058 0.011 0.953 Value29=5.250 0.592 0.00882 0.0063 0.010 0.957 Value30=5.500 0.619 0.00915 0.0069 0.009 0.961 Value31=5.750 0.645 0.00974 0.0078 0.009 0.966 Value32=6.000 0.671 0.01013 0.0087 0.008 0.971 Value33=6.250 0.697 0.01064 0.0096 0.008 0.976 Value34=6.500 0.724 0.01122 0.0104 0.008 0.982 Value35=6.750 0.753 0.01188 0.0107 0.007 0.987 Value36=7.000 0.783 0.01268 0.0105 0.007 0.992 Value37=7.250 0.813 0.01427 0.0102 0.007 0.996 Value38=7.500 0.842 0.01543 0.0102 0.006 1.000 Value39=7.750 0.865 0.01725 0.0113 0.006 1.000 Value40=8.000 0.884 0.01990 0.0125 0.006 1.000 Value41=8.250 0.898 0.02341 0.0138 0.006 1.000 Value42=8.500 0.907 0.02767 0.0152 0.005 1.000 Value43=8.750 0.902 0.03401 0.0167 0.005 1.000 Value44=9.000 0.879 0.04308 0.0175 0.005 1.000 Value45=9.250 0.851 0.05188 0.0167 0.005 1.000 Value46=9.500 0.800 0.06493 0.0086 0.005 1.000 Value47=9.750 0.767 0.08195 -0.0082 0.006 1.000 Value48=10.000 0.752 0.09050 -0.0138 0.006 1.000 Value49=10.250 0.740 0.09798 -0.0180 0.006 1.000 Value50=10.500 0.732 0.10490 -0.0216 0.006 1.000 Value51=10.750 0.725 0.11150 -0.0248 0.006 1.000 Value52=11.000 0.720 0.11763 -0.0276 0.006 1.000 Value53=11.250 0.719 0.12275 -0.0299 0.006 1.000