; 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 52 9.00% NumberSets=1 [Set1] Origin=PEFView Description1=XFLR Analysis, M=0.285 Description2=Copyright 2007 Martin Hepperle NumberPolars=5 [Set1-Polar1] ReynoldsNumber=500000 MachNumber=0 NumberPoints=44 Values=Alpha Cl Cd Cm TU TL Value01=-2.000 -0.207 0.00624 -0.0088 0.963 0.741 Value02=-1.750 -0.178 0.00616 -0.0085 0.957 0.771 Value03=-1.500 -0.150 0.00611 -0.0076 0.950 0.799 Value04=-1.250 -0.125 0.00609 -0.0062 0.942 0.822 Value05=-1.000 -0.100 0.00609 -0.0049 0.934 0.840 Value06=-0.750 -0.075 0.00611 -0.0034 0.926 0.857 Value07=-0.500 -0.051 0.00613 -0.0019 0.917 0.872 Value08=-0.250 -0.026 0.00614 -0.0003 0.907 0.884 Value09=0.000 -0.002 0.00614 0.0013 0.896 0.896 Value10=0.250 0.023 0.00614 0.0028 0.884 0.906 Value11=0.500 0.047 0.00613 0.0044 0.871 0.915 Value12=0.750 0.071 0.00611 0.0059 0.855 0.924 Value13=1.000 0.096 0.00610 0.0074 0.838 0.932 Value14=1.250 0.121 0.00611 0.0088 0.817 0.940 Value15=1.500 0.147 0.00614 0.0101 0.790 0.947 Value16=1.750 0.173 0.00620 0.0112 0.762 0.954 Value17=2.000 0.200 0.00630 0.0119 0.729 0.960 Value18=2.250 0.230 0.00643 0.0121 0.691 0.966 Value19=2.500 0.261 0.00662 0.0119 0.642 0.970 Value20=2.750 0.292 0.00695 0.0114 0.566 0.975 Value21=3.000 0.325 0.00749 0.0105 0.455 0.978 Value22=3.250 0.360 0.00817 0.0088 0.337 0.981 Value23=3.500 0.395 0.00886 0.0070 0.231 0.984 Value24=3.750 0.430 0.00950 0.0053 0.148 0.986 Value25=4.000 0.465 0.01013 0.0036 0.084 0.989 Value26=4.250 0.500 0.01085 0.0020 0.044 0.992 Value27=4.500 0.536 0.01142 0.0006 0.034 0.994 Value28=4.750 0.572 0.01203 -0.0009 0.029 0.996 Value29=5.000 0.608 0.01270 -0.0024 0.026 0.999 Value30=5.250 0.638 0.01341 -0.0029 0.024 1.000 Value31=5.500 0.658 0.01418 -0.0011 0.023 1.000 Value32=5.750 0.678 0.01486 0.0008 0.021 1.000 Value33=6.000 0.696 0.01579 0.0028 0.020 1.000 Value34=6.250 0.715 0.01666 0.0049 0.019 1.000 Value35=6.500 0.733 0.01772 0.0072 0.018 1.000 Value36=6.750 0.750 0.01888 0.0096 0.018 1.000 Value37=7.000 0.767 0.02015 0.0118 0.017 1.000 Value38=7.250 0.785 0.02187 0.0137 0.017 1.000 Value39=7.500 0.802 0.02447 0.0154 0.017 1.000 Value40=7.750 0.817 0.02720 0.0172 0.017 1.000 Value41=8.000 0.828 0.03044 0.0192 0.016 1.000 Value42=8.250 0.833 0.03450 0.0210 0.016 1.000 Value43=8.500 0.835 0.03853 0.0225 0.016 1.000 Value44=8.750 0.835 0.04237 0.0237 0.017 1.000 [Set1-Polar2] ReynoldsNumber=750000 MachNumber=0 NumberPoints=50 Values=Alpha Cl Cd Cm TU TL Value01=-2.000 -0.214 0.00543 -0.0058 0.937 0.666 Value02=-1.750 -0.188 0.00527 -0.0048 0.929 0.702 Value03=-1.500 -0.162 0.00512 -0.0038 0.922 0.735 Value04=-1.250 -0.136 0.00500 -0.0029 0.915 0.764 Value05=-1.000 -0.110 0.00490 -0.0020 0.908 0.792 Value06=-0.750 -0.083 0.00483 -0.0011 0.899 0.815 Value07=-0.500 -0.056 0.00479 -0.0003 0.889 0.836 Value08=-0.250 -0.029 0.00477 0.0005 0.878 0.852 Value09=0.000 -0.002 0.00476 0.0012 0.866 0.865 Value10=0.250 0.026 0.00477 0.0019 0.850 0.878 Value11=0.500 0.053 0.00480 0.0027 0.832 0.889 Value12=0.750 0.080 0.00485 0.0035 0.811 0.897 Value13=1.000 0.106 0.00493 0.0044 0.784 0.906 Value14=1.250 0.133 0.00505 0.0053 0.753 0.913 Value15=1.500 0.159 0.00518 0.0062 0.722 0.921 Value16=1.750 0.185 0.00534 0.0072 0.688 0.927 Value17=2.000 0.210 0.00550 0.0081 0.651 0.933 Value18=2.250 0.236 0.00572 0.0092 0.603 0.940 Value19=2.500 0.260 0.00604 0.0103 0.531 0.946 Value20=2.750 0.283 0.00649 0.0115 0.437 0.951 Value21=3.000 0.307 0.00694 0.0125 0.352 0.957 Value22=3.250 0.331 0.00741 0.0134 0.270 0.963 Value23=3.500 0.356 0.00788 0.0140 0.197 0.968 Value24=3.750 0.384 0.00831 0.0143 0.141 0.973 Value25=4.000 0.413 0.00873 0.0141 0.095 0.977 Value26=4.250 0.444 0.00926 0.0135 0.051 0.981 Value27=4.500 0.477 0.00976 0.0126 0.033 0.984 Value28=4.750 0.511 0.01023 0.0115 0.027 0.986 Value29=5.000 0.546 0.01072 0.0104 0.023 0.989 Value30=5.250 0.582 0.01120 0.0089 0.021 0.990 Value31=5.500 0.616 0.01188 0.0078 0.019 0.992 Value32=5.750 0.650 0.01242 0.0067 0.018 0.994 Value33=6.000 0.683 0.01333 0.0058 0.016 0.996 Value34=6.250 0.717 0.01414 0.0049 0.015 0.998 Value35=6.500 0.751 0.01507 0.0039 0.015 1.000 Value36=6.750 0.768 0.01600 0.0060 0.014 1.000 Value37=7.000 0.782 0.01744 0.0089 0.014 1.000 Value38=7.250 0.798 0.01860 0.0115 0.013 1.000 Value39=7.500 0.815 0.02016 0.0137 0.013 1.000 Value40=7.750 0.834 0.02203 0.0153 0.012 1.000 Value41=8.000 0.851 0.02451 0.0169 0.012 1.000 Value42=8.250 0.863 0.02773 0.0185 0.012 1.000 Value43=8.500 0.867 0.03212 0.0204 0.012 1.000 Value44=8.750 0.857 0.03838 0.0225 0.012 1.000 Value45=9.000 0.839 0.04494 0.0237 0.012 1.000 Value46=9.250 0.819 0.04994 0.0244 0.013 1.000 Value47=9.500 0.799 0.05518 0.0227 0.013 1.000 Value48=9.750 0.779 0.06202 0.0170 0.013 1.000 Value49=10.000 0.762 0.07356 0.0059 0.013 1.000 Value50=10.250 0.752 0.08203 -0.0005 0.013 1.000 [Set1-Polar3] ReynoldsNumber=1000000 MachNumber=0 NumberPoints=52 Values=Alpha Cl Cd Cm TU TL Value01=-2.000 -0.220 0.00503 -0.0030 0.919 0.608 Value02=-1.750 -0.193 0.00483 -0.0024 0.912 0.650 Value03=-1.500 -0.165 0.00467 -0.0019 0.905 0.686 Value04=-1.250 -0.138 0.00452 -0.0014 0.898 0.719 Value05=-1.000 -0.110 0.00439 -0.0008 0.889 0.748 Value06=-0.750 -0.083 0.00428 -0.0003 0.879 0.778 Value07=-0.500 -0.055 0.00420 0.0002 0.867 0.802 Value08=-0.250 -0.027 0.00415 0.0007 0.854 0.825 Value09=0.000 0.001 0.00414 0.0013 0.836 0.843 Value10=0.250 0.029 0.00417 0.0018 0.816 0.856 Value11=0.500 0.057 0.00423 0.0023 0.793 0.870 Value12=0.750 0.084 0.00434 0.0028 0.764 0.880 Value13=1.000 0.112 0.00447 0.0034 0.732 0.889 Value14=1.250 0.139 0.00461 0.0039 0.700 0.897 Value15=1.500 0.167 0.00477 0.0044 0.665 0.905 Value16=1.750 0.194 0.00494 0.0049 0.629 0.912 Value17=2.000 0.221 0.00517 0.0055 0.578 0.918 Value18=2.500 0.272 0.00599 0.0070 0.408 0.929 Value19=2.750 0.297 0.00640 0.0077 0.332 0.935 Value20=3.000 0.323 0.00686 0.0083 0.254 0.940 Value21=3.250 0.348 0.00728 0.0089 0.189 0.945 Value22=3.500 0.374 0.00765 0.0096 0.141 0.950 Value23=3.750 0.399 0.00800 0.0104 0.101 0.955 Value24=4.000 0.424 0.00836 0.0112 0.066 0.959 Value25=4.250 0.450 0.00875 0.0121 0.037 0.964 Value26=4.500 0.475 0.00910 0.0129 0.028 0.969 Value27=4.750 0.502 0.00942 0.0136 0.023 0.974 Value28=5.000 0.530 0.00972 0.0140 0.021 0.978 Value29=5.250 0.560 0.01013 0.0140 0.019 0.982 Value30=5.500 0.591 0.01056 0.0135 0.017 0.986 Value31=5.750 0.624 0.01108 0.0129 0.016 0.988 Value32=6.000 0.657 0.01160 0.0121 0.015 0.990 Value33=6.250 0.689 0.01253 0.0113 0.014 0.993 Value34=6.500 0.723 0.01320 0.0104 0.013 0.994 Value35=6.750 0.756 0.01405 0.0095 0.012 0.996 Value36=7.000 0.789 0.01500 0.0087 0.012 0.998 Value37=7.250 0.817 0.01620 0.0087 0.011 1.000 Value38=7.500 0.830 0.01751 0.0117 0.011 1.000 Value39=7.750 0.849 0.01881 0.0136 0.010 1.000 Value40=8.000 0.868 0.02079 0.0152 0.010 1.000 Value41=8.250 0.884 0.02340 0.0167 0.010 1.000 Value42=8.500 0.895 0.02683 0.0184 0.010 1.000 Value43=8.750 0.898 0.03125 0.0203 0.010 1.000 Value44=9.000 0.890 0.03683 0.0222 0.010 1.000 Value45=9.250 0.870 0.04307 0.0236 0.010 1.000 Value46=9.500 0.845 0.04863 0.0243 0.010 1.000 Value47=9.750 0.820 0.05493 0.0214 0.010 1.000 Value48=10.000 0.796 0.06391 0.0133 0.010 1.000 Value49=10.250 0.771 0.07968 0.0001 0.010 1.000 Value50=10.500 0.757 0.08823 -0.0054 0.011 1.000 Value51=10.750 0.746 0.09542 -0.0096 0.011 1.000 Value52=11.000 0.740 0.10065 -0.0126 0.011 1.000 [Set1-Polar4] ReynoldsNumber=1500000 MachNumber=0 NumberPoints=57 Values=Alpha Cl Cd Cm TU TL Value01=-2.000 -0.227 0.00475 -0.0011 0.898 0.504 Value02=-1.750 -0.199 0.00449 -0.0008 0.891 0.559 Value03=-1.500 -0.171 0.00429 -0.0006 0.883 0.603 Value04=-1.250 -0.143 0.00414 -0.0003 0.873 0.641 Value05=-1.000 -0.115 0.00399 -0.0001 0.861 0.676 Value06=-0.750 -0.086 0.00388 0.0002 0.848 0.705 Value07=-0.500 -0.058 0.00379 0.0005 0.831 0.736 Value08=-0.250 -0.030 0.00374 0.0009 0.807 0.766 Value09=0.000 -0.002 0.00373 0.0012 0.784 0.791 Value10=0.250 0.026 0.00375 0.0016 0.759 0.815 Value11=0.500 0.054 0.00383 0.0019 0.726 0.832 Value12=0.750 0.083 0.00393 0.0022 0.694 0.848 Value13=1.000 0.111 0.00405 0.0024 0.663 0.862 Value14=1.250 0.139 0.00420 0.0027 0.625 0.872 Value15=1.500 0.168 0.00436 0.0029 0.589 0.881 Value16=1.750 0.196 0.00460 0.0031 0.535 0.889 Value17=2.000 0.223 0.00497 0.0034 0.453 0.896 Value18=2.250 0.250 0.00540 0.0038 0.367 0.903 Value19=2.500 0.277 0.00574 0.0041 0.304 0.908 Value20=2.750 0.304 0.00616 0.0043 0.230 0.913 Value21=3.000 0.332 0.00652 0.0046 0.175 0.918 Value22=3.250 0.359 0.00684 0.0049 0.133 0.923 Value23=3.500 0.387 0.00716 0.0052 0.096 0.927 Value24=3.750 0.415 0.00747 0.0054 0.067 0.931 Value25=4.000 0.442 0.00781 0.0059 0.040 0.935 Value26=4.250 0.470 0.00811 0.0063 0.027 0.939 Value27=4.500 0.498 0.00838 0.0066 0.022 0.943 Value28=4.750 0.526 0.00864 0.0071 0.019 0.946 Value29=5.000 0.553 0.00897 0.0077 0.017 0.950 Value30=5.250 0.580 0.00920 0.0082 0.015 0.954 Value31=5.500 0.607 0.00952 0.0089 0.014 0.958 Value32=5.750 0.633 0.00991 0.0097 0.013 0.962 Value33=6.000 0.660 0.01024 0.0105 0.012 0.966 Value34=6.250 0.686 0.01060 0.0114 0.012 0.971 Value35=6.500 0.710 0.01131 0.0125 0.011 0.976 Value36=6.750 0.738 0.01174 0.0131 0.011 0.980 Value37=7.000 0.766 0.01233 0.0135 0.010 0.985 Value38=7.250 0.797 0.01298 0.0133 0.009 0.989 Value39=7.500 0.828 0.01367 0.0128 0.009 0.993 Value40=7.750 0.857 0.01533 0.0125 0.008 0.997 Value41=8.000 0.886 0.01645 0.0124 0.008 1.000 Value42=8.250 0.907 0.01781 0.0137 0.008 1.000 Value43=8.500 0.928 0.01966 0.0150 0.008 1.000 Value44=8.750 0.945 0.02210 0.0163 0.008 1.000 Value45=9.000 0.956 0.02531 0.0180 0.007 1.000 Value46=9.250 0.959 0.02940 0.0198 0.007 1.000 Value47=9.500 0.952 0.03443 0.0217 0.007 1.000 Value48=9.750 0.932 0.04003 0.0236 0.007 1.000 Value49=10.000 0.903 0.04554 0.0243 0.007 1.000 Value50=10.250 0.873 0.05261 0.0207 0.007 1.000 Value51=10.500 0.841 0.06434 0.0096 0.007 1.000 Value52=10.750 0.787 0.08680 -0.0057 0.008 1.000 Value53=11.000 0.765 0.09667 -0.0114 0.008 1.000 Value54=11.250 0.749 0.10509 -0.0159 0.008 1.000 Value55=11.500 0.738 0.11250 -0.0195 0.008 1.000 Value56=11.750 0.730 0.11910 -0.0226 0.008 1.000 Value57=12.000 0.726 0.12487 -0.0253 0.008 1.000 [Set1-Polar5] ReynoldsNumber=2000000 MachNumber=0 NumberPoints=55 Values=Alpha Cl Cd Cm TU TL Value01=-2.000 -0.226 0.00471 -0.0003 0.882 0.415 Value02=-1.750 -0.198 0.00435 -0.0001 0.873 0.496 Value03=-1.500 -0.170 0.00415 0.0001 0.862 0.542 Value04=-1.250 -0.141 0.00398 0.0002 0.848 0.586 Value05=-1.000 -0.113 0.00385 0.0004 0.833 0.624 Value06=-0.750 -0.085 0.00376 0.0006 0.812 0.659 Value07=-0.500 -0.056 0.00373 0.0008 0.785 0.687 Value08=-0.250 -0.028 0.00369 0.0010 0.761 0.718 Value09=0.000 0.001 0.00367 0.0012 0.735 0.747 Value10=0.250 0.029 0.00370 0.0014 0.702 0.775 Value11=0.500 0.057 0.00375 0.0017 0.670 0.800 Value12=0.750 0.086 0.00382 0.0018 0.639 0.818 Value13=1.000 0.115 0.00393 0.0020 0.601 0.836 Value14=1.250 0.143 0.00406 0.0021 0.565 0.852 Value15=1.750 0.199 0.00460 0.0025 0.436 0.873 Value16=2.000 0.227 0.00500 0.0027 0.352 0.881 Value17=2.250 0.255 0.00531 0.0028 0.293 0.888 Value18=2.500 0.283 0.00566 0.0029 0.229 0.895 Value19=2.750 0.310 0.00599 0.0031 0.175 0.900 Value20=3.000 0.339 0.00627 0.0032 0.136 0.905 Value21=3.250 0.367 0.00657 0.0034 0.100 0.910 Value22=3.500 0.396 0.00684 0.0036 0.073 0.914 Value23=3.750 0.424 0.00713 0.0037 0.048 0.918 Value24=4.000 0.452 0.00742 0.0040 0.029 0.922 Value25=4.250 0.481 0.00767 0.0042 0.022 0.926 Value26=4.500 0.510 0.00789 0.0045 0.019 0.929 Value27=4.750 0.538 0.00814 0.0047 0.016 0.933 Value28=5.000 0.567 0.00837 0.0050 0.015 0.936 Value29=5.250 0.595 0.00867 0.0054 0.013 0.939 Value30=5.500 0.624 0.00892 0.0057 0.013 0.943 Value31=5.750 0.652 0.00920 0.0062 0.012 0.946 Value32=6.000 0.679 0.00966 0.0067 0.011 0.950 Value33=6.250 0.707 0.00996 0.0073 0.010 0.953 Value34=6.500 0.734 0.01032 0.0080 0.010 0.957 Value35=6.750 0.762 0.01070 0.0086 0.009 0.960 Value36=7.000 0.787 0.01138 0.0096 0.009 0.964 Value37=7.250 0.812 0.01192 0.0106 0.008 0.968 Value38=7.500 0.837 0.01247 0.0117 0.008 0.974 Value39=7.750 0.862 0.01314 0.0129 0.008 0.980 Value40=8.000 0.888 0.01394 0.0136 0.007 0.986 Value41=8.250 0.918 0.01489 0.0137 0.007 0.991 Value42=8.500 0.948 0.01601 0.0134 0.007 0.997 Value43=8.750 0.973 0.01730 0.0139 0.007 1.000 Value44=9.000 0.992 0.01930 0.0151 0.007 1.000 Value45=9.250 1.004 0.02240 0.0167 0.006 1.000 Value46=9.500 1.017 0.02516 0.0182 0.006 1.000 Value47=9.750 1.018 0.02917 0.0201 0.006 1.000 Value48=10.000 1.004 0.03451 0.0223 0.006 1.000 Value49=10.250 0.980 0.03959 0.0244 0.006 1.000 Value50=10.500 0.955 0.04474 0.0242 0.006 1.000 Value51=10.750 0.933 0.05093 0.0204 0.006 1.000 Value52=11.000 0.918 0.05904 0.0123 0.006 1.000 Value53=11.250 0.891 0.07452 0.0009 0.006 1.000 Value54=11.500 0.858 0.08666 -0.0068 0.006 1.000 Value55=11.750 0.815 0.10004 -0.0145 0.006 1.000