; 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 54 8.00% 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=48 Values=Alpha Cl Cd Cm TU TL Value01=-2.000 -0.154 0.00632 -0.0188 0.966 0.757 Value02=-1.750 -0.125 0.00616 -0.0180 0.962 0.835 Value03=-1.500 -0.096 0.00616 -0.0175 0.957 0.871 Value04=-1.250 -0.068 0.00619 -0.0166 0.951 0.895 Value05=-1.000 -0.042 0.00623 -0.0154 0.945 0.914 Value06=-0.750 -0.016 0.00627 -0.0139 0.938 0.929 Value07=-0.500 0.009 0.00631 -0.0124 0.931 0.943 Value08=-0.250 0.036 0.00634 -0.0112 0.924 0.955 Value09=0.000 0.068 0.00635 -0.0113 0.917 0.963 Value10=0.250 0.102 0.00631 -0.0119 0.910 0.970 Value11=0.750 0.179 0.00618 -0.0154 0.890 0.980 Value12=1.000 0.216 0.00609 -0.0169 0.877 0.985 Value13=1.250 0.254 0.00599 -0.0186 0.859 0.989 Value14=1.500 0.292 0.00590 -0.0203 0.836 0.994 Value15=1.750 0.329 0.00584 -0.0219 0.801 0.997 Value16=2.000 0.365 0.00591 -0.0232 0.752 1.000 Value17=2.250 0.391 0.00611 -0.0224 0.696 1.000 Value18=2.500 0.418 0.00638 -0.0219 0.632 1.000 Value19=2.750 0.443 0.00678 -0.0214 0.549 1.000 Value20=3.000 0.469 0.00735 -0.0209 0.443 1.000 Value21=3.250 0.494 0.00791 -0.0205 0.349 1.000 Value22=3.500 0.518 0.00848 -0.0199 0.266 1.000 Value23=3.750 0.542 0.00905 -0.0191 0.190 1.000 Value24=4.000 0.565 0.00964 -0.0183 0.127 1.000 Value25=4.250 0.587 0.01026 -0.0172 0.073 1.000 Value26=4.500 0.609 0.01092 -0.0159 0.044 1.000 Value27=4.750 0.632 0.01147 -0.0145 0.034 1.000 Value28=5.000 0.654 0.01206 -0.0130 0.029 1.000 Value29=5.250 0.675 0.01272 -0.0113 0.026 1.000 Value30=5.500 0.695 0.01347 -0.0096 0.024 1.000 Value31=5.750 0.715 0.01417 -0.0077 0.022 1.000 Value32=6.000 0.735 0.01510 -0.0058 0.020 1.000 Value33=6.250 0.755 0.01612 -0.0039 0.019 1.000 Value34=6.500 0.776 0.01707 -0.0022 0.018 1.000 Value35=6.750 0.796 0.01867 -0.0005 0.017 1.000 Value36=7.000 0.818 0.02010 0.0013 0.015 1.000 Value37=7.250 0.839 0.02145 0.0026 0.014 1.000 Value38=7.500 0.855 0.02424 0.0048 0.014 1.000 Value39=7.750 0.867 0.02777 0.0074 0.013 1.000 Value40=8.000 0.880 0.03014 0.0092 0.012 1.000 Value41=8.250 0.889 0.03275 0.0110 0.011 1.000 Value42=8.500 0.885 0.03780 0.0138 0.011 1.000 Value43=8.750 0.876 0.04272 0.0160 0.011 1.000 Value44=9.000 0.863 0.04711 0.0178 0.011 1.000 Value45=9.250 0.847 0.05108 0.0190 0.011 1.000 Value46=9.500 0.831 0.05551 0.0180 0.011 1.000 Value47=9.750 0.817 0.06082 0.0144 0.011 1.000 Value48=10.000 0.805 0.06759 0.0079 0.011 1.000 [Set1-Polar2] ReynoldsNumber=750000 MachNumber=0 NumberPoints=54 Values=Alpha Cl Cd Cm TU TL Value01=-2.000 -0.143 0.00574 -0.0193 0.944 0.604 Value02=-1.750 -0.122 0.00529 -0.0173 0.938 0.715 Value03=-1.500 -0.100 0.00500 -0.0154 0.932 0.793 Value04=-1.000 -0.051 0.00481 -0.0126 0.920 0.870 Value05=-0.750 -0.025 0.00478 -0.0114 0.914 0.893 Value06=-0.500 0.000 0.00476 -0.0101 0.906 0.911 Value07=-0.250 0.026 0.00475 -0.0089 0.898 0.925 Value08=0.000 0.051 0.00476 -0.0076 0.890 0.938 Value09=0.250 0.076 0.00477 -0.0063 0.880 0.949 Value10=0.500 0.103 0.00478 -0.0055 0.869 0.958 Value11=0.750 0.131 0.00478 -0.0049 0.855 0.965 Value12=1.000 0.162 0.00479 -0.0051 0.836 0.971 Value13=1.250 0.196 0.00483 -0.0057 0.810 0.975 Value14=1.500 0.230 0.00492 -0.0067 0.776 0.979 Value15=1.750 0.266 0.00508 -0.0081 0.733 0.982 Value16=2.000 0.302 0.00530 -0.0096 0.683 0.985 Value17=2.250 0.338 0.00557 -0.0111 0.624 0.988 Value18=2.500 0.373 0.00589 -0.0126 0.557 0.990 Value19=2.750 0.407 0.00638 -0.0141 0.460 0.993 Value20=3.000 0.442 0.00693 -0.0156 0.358 0.995 Value21=3.250 0.477 0.00743 -0.0173 0.275 0.997 Value22=3.500 0.512 0.00798 -0.0189 0.196 0.998 Value23=3.750 0.546 0.00851 -0.0205 0.129 1.000 Value24=4.000 0.571 0.00895 -0.0198 0.085 1.000 Value25=4.250 0.594 0.00946 -0.0188 0.048 1.000 Value26=4.500 0.618 0.00992 -0.0178 0.032 1.000 Value27=4.750 0.641 0.01036 -0.0165 0.026 1.000 Value28=5.000 0.664 0.01082 -0.0152 0.023 1.000 Value29=5.250 0.686 0.01137 -0.0137 0.020 1.000 Value30=5.500 0.708 0.01185 -0.0122 0.018 1.000 Value31=5.750 0.728 0.01256 -0.0103 0.017 1.000 Value32=6.000 0.749 0.01319 -0.0085 0.016 1.000 Value33=6.250 0.769 0.01383 -0.0067 0.015 1.000 Value34=6.500 0.787 0.01493 -0.0045 0.014 1.000 Value35=6.750 0.809 0.01568 -0.0028 0.013 1.000 Value36=7.000 0.831 0.01650 -0.0012 0.012 1.000 Value37=7.250 0.850 0.01808 0.0007 0.011 1.000 Value38=7.500 0.871 0.01953 0.0023 0.010 1.000 Value39=7.750 0.891 0.02080 0.0036 0.009 1.000 Value40=8.000 0.906 0.02376 0.0060 0.008 1.000 Value41=8.250 0.915 0.02729 0.0085 0.008 1.000 Value42=8.500 0.923 0.03044 0.0106 0.008 1.000 Value43=8.750 0.930 0.03310 0.0124 0.007 1.000 Value44=9.000 0.927 0.03704 0.0146 0.007 1.000 Value45=9.250 0.913 0.04154 0.0169 0.007 1.000 Value46=9.500 0.894 0.04580 0.0186 0.007 1.000 Value47=9.750 0.874 0.05101 0.0180 0.007 1.000 Value48=10.000 0.807 0.07071 0.0048 0.008 1.000 Value49=10.250 0.792 0.08313 -0.0049 0.008 1.000 Value50=10.500 0.780 0.09105 -0.0098 0.009 1.000 Value51=10.750 0.770 0.09808 -0.0137 0.009 1.000 Value52=11.000 0.763 0.10453 -0.0170 0.009 1.000 Value53=11.250 0.757 0.11043 -0.0199 0.009 1.000 Value54=11.500 0.754 0.11551 -0.0223 0.009 1.000 [Set1-Polar3] ReynoldsNumber=1000000 MachNumber=0 NumberPoints=57 Values=Alpha Cl Cd Cm TU TL Value01=-2.000 -0.151 0.00561 -0.0161 0.929 0.473 Value02=-1.750 -0.128 0.00511 -0.0149 0.923 0.588 Value03=-1.500 -0.105 0.00466 -0.0137 0.917 0.696 Value04=-1.250 -0.080 0.00437 -0.0125 0.911 0.769 Value05=-1.000 -0.055 0.00419 -0.0114 0.905 0.820 Value06=-0.750 -0.028 0.00408 -0.0105 0.898 0.857 Value07=-0.500 -0.002 0.00403 -0.0096 0.890 0.882 Value08=-0.250 0.025 0.00400 -0.0089 0.882 0.901 Value09=0.000 0.052 0.00399 -0.0081 0.872 0.915 Value10=0.250 0.079 0.00399 -0.0072 0.859 0.929 Value11=0.500 0.105 0.00401 -0.0063 0.844 0.940 Value12=0.750 0.131 0.00405 -0.0052 0.822 0.949 Value13=1.000 0.157 0.00414 -0.0042 0.794 0.956 Value14=1.250 0.183 0.00428 -0.0033 0.760 0.963 Value15=1.500 0.209 0.00444 -0.0026 0.722 0.970 Value16=1.750 0.238 0.00464 -0.0025 0.678 0.975 Value17=2.000 0.270 0.00487 -0.0029 0.631 0.979 Value18=2.250 0.303 0.00515 -0.0038 0.574 0.982 Value19=2.500 0.337 0.00548 -0.0052 0.510 0.985 Value20=2.750 0.372 0.00595 -0.0067 0.418 0.986 Value21=3.000 0.405 0.00645 -0.0079 0.329 0.989 Value22=3.250 0.439 0.00689 -0.0094 0.259 0.990 Value23=3.500 0.474 0.00738 -0.0109 0.189 0.992 Value24=3.750 0.508 0.00785 -0.0123 0.130 0.994 Value25=4.000 0.542 0.00830 -0.0137 0.084 0.996 Value26=4.250 0.577 0.00878 -0.0150 0.046 0.997 Value27=4.500 0.611 0.00922 -0.0163 0.029 0.999 Value28=4.750 0.646 0.00964 -0.0175 0.022 1.000 Value29=5.000 0.672 0.01004 -0.0167 0.019 1.000 Value30=5.250 0.694 0.01052 -0.0154 0.017 1.000 Value31=5.500 0.717 0.01093 -0.0139 0.016 1.000 Value32=5.750 0.739 0.01140 -0.0124 0.015 1.000 Value33=6.000 0.759 0.01203 -0.0105 0.014 1.000 Value34=6.250 0.780 0.01259 -0.0087 0.013 1.000 Value35=6.500 0.801 0.01319 -0.0069 0.012 1.000 Value36=6.750 0.820 0.01401 -0.0048 0.011 1.000 Value37=7.000 0.841 0.01478 -0.0030 0.010 1.000 Value38=7.250 0.862 0.01561 -0.0014 0.009 1.000 Value39=7.500 0.883 0.01674 0.0003 0.008 1.000 Value40=7.750 0.906 0.01775 0.0016 0.008 1.000 Value41=8.000 0.924 0.01956 0.0033 0.007 1.000 Value42=8.250 0.939 0.02222 0.0056 0.006 1.000 Value43=8.500 0.948 0.02565 0.0081 0.006 1.000 Value44=8.750 0.956 0.02895 0.0103 0.006 1.000 Value45=9.000 0.959 0.03237 0.0124 0.005 1.000 Value46=9.250 0.956 0.03630 0.0146 0.005 1.000 Value47=9.500 0.942 0.04069 0.0169 0.005 1.000 Value48=9.750 0.921 0.04519 0.0185 0.005 1.000 Value49=10.000 0.896 0.05109 0.0173 0.005 1.000 Value50=10.250 0.824 0.07414 0.0005 0.006 1.000 Value51=10.500 0.806 0.08526 -0.0072 0.006 1.000 Value52=10.750 0.791 0.09365 -0.0122 0.006 1.000 Value53=11.000 0.779 0.10126 -0.0163 0.007 1.000 Value54=11.250 0.769 0.10845 -0.0198 0.007 1.000 Value55=11.500 0.761 0.11517 -0.0230 0.007 1.000 Value56=11.750 0.755 0.12150 -0.0258 0.007 1.000 Value57=12.000 0.751 0.12731 -0.0283 0.007 1.000 [Set1-Polar4] ReynoldsNumber=1500000 MachNumber=0 NumberPoints=56 Values=Alpha Cl Cd Cm TU TL Value01=-2.000 -0.159 0.00546 -0.0132 0.909 0.320 Value02=-1.750 -0.132 0.00501 -0.0128 0.903 0.421 Value03=-1.500 -0.106 0.00454 -0.0123 0.898 0.533 Value04=-1.250 -0.081 0.00411 -0.0116 0.891 0.639 Value05=-1.000 -0.054 0.00383 -0.0110 0.884 0.709 Value06=-0.750 -0.028 0.00361 -0.0104 0.875 0.767 Value07=-0.500 -0.001 0.00345 -0.0097 0.865 0.816 Value08=-0.250 0.026 0.00335 -0.0091 0.853 0.853 Value09=0.000 0.054 0.00333 -0.0085 0.836 0.877 Value10=0.250 0.081 0.00335 -0.0080 0.813 0.895 Value11=0.500 0.108 0.00343 -0.0073 0.783 0.910 Value12=0.750 0.135 0.00355 -0.0066 0.749 0.923 Value13=1.000 0.161 0.00371 -0.0059 0.711 0.933 Value14=1.250 0.188 0.00388 -0.0053 0.672 0.941 Value15=1.500 0.214 0.00408 -0.0046 0.629 0.948 Value16=1.750 0.240 0.00428 -0.0039 0.585 0.955 Value17=2.000 0.265 0.00453 -0.0031 0.533 0.961 Value18=2.250 0.291 0.00479 -0.0023 0.481 0.967 Value19=2.500 0.317 0.00509 -0.0016 0.421 0.972 Value20=2.750 0.342 0.00551 -0.0010 0.343 0.978 Value21=3.000 0.371 0.00588 -0.0010 0.278 0.982 Value22=3.250 0.402 0.00622 -0.0016 0.225 0.985 Value23=3.500 0.434 0.00663 -0.0025 0.166 0.987 Value24=3.750 0.467 0.00702 -0.0035 0.120 0.989 Value25=4.000 0.501 0.00741 -0.0048 0.081 0.990 Value26=4.250 0.535 0.00781 -0.0061 0.049 0.992 Value27=4.500 0.569 0.00819 -0.0072 0.029 0.993 Value28=4.750 0.604 0.00853 -0.0084 0.021 0.994 Value29=5.000 0.638 0.00891 -0.0094 0.017 0.996 Value30=5.250 0.673 0.00922 -0.0105 0.015 0.997 Value31=5.750 0.741 0.01004 -0.0125 0.012 0.999 Value32=6.000 0.774 0.01064 -0.0133 0.011 1.000 Value33=6.250 0.796 0.01102 -0.0118 0.010 1.000 Value34=6.500 0.818 0.01144 -0.0101 0.010 1.000 Value35=6.750 0.837 0.01215 -0.0080 0.009 1.000 Value36=7.000 0.859 0.01257 -0.0062 0.008 1.000 Value37=7.250 0.881 0.01303 -0.0046 0.007 1.000 Value38=7.500 0.901 0.01395 -0.0026 0.007 1.000 Value39=7.750 0.923 0.01471 -0.0011 0.006 1.000 Value40=8.000 0.947 0.01545 0.0001 0.006 1.000 Value41=8.250 0.966 0.01701 0.0019 0.005 1.000 Value42=8.500 0.985 0.01886 0.0037 0.005 1.000 Value43=8.750 1.003 0.02073 0.0054 0.004 1.000 Value44=9.000 1.023 0.02225 0.0068 0.004 1.000 Value45=9.250 1.028 0.02590 0.0093 0.004 1.000 Value46=9.500 1.018 0.03152 0.0126 0.004 1.000 Value47=9.750 0.995 0.03799 0.0156 0.003 1.000 Value48=10.000 0.968 0.04319 0.0183 0.003 1.000 Value49=10.250 0.944 0.04845 0.0185 0.003 1.000 Value50=10.500 0.924 0.05430 0.0157 0.004 1.000 Value51=10.750 0.911 0.06134 0.0097 0.004 1.000 Value52=11.000 0.903 0.07177 0.0008 0.004 1.000 Value53=11.250 0.814 0.09804 -0.0155 0.004 1.000 Value54=11.500 0.793 0.10791 -0.0205 0.004 1.000 Value55=11.750 0.778 0.11614 -0.0244 0.004 1.000 Value56=12.000 0.768 0.12358 -0.0277 0.004 1.000 [Set1-Polar5] ReynoldsNumber=2000000 MachNumber=0 NumberPoints=57 Values=Alpha Cl Cd Cm TU TL Value01=-2.000 -0.161 0.00532 -0.0121 0.896 0.242 Value02=-1.750 -0.134 0.00495 -0.0119 0.890 0.324 Value03=-1.500 -0.107 0.00454 -0.0116 0.883 0.421 Value04=-1.250 -0.080 0.00412 -0.0112 0.876 0.527 Value05=-1.000 -0.054 0.00376 -0.0108 0.867 0.624 Value06=-0.750 -0.026 0.00355 -0.0104 0.855 0.681 Value07=-0.500 0.001 0.00335 -0.0099 0.840 0.740 Value08=-0.250 0.028 0.00323 -0.0094 0.819 0.790 Value09=0.000 0.054 0.00317 -0.0087 0.792 0.834 Value10=0.250 0.081 0.00322 -0.0081 0.759 0.863 Value11=0.500 0.108 0.00331 -0.0076 0.724 0.883 Value12=0.750 0.136 0.00344 -0.0072 0.685 0.900 Value13=1.000 0.163 0.00358 -0.0067 0.648 0.913 Value14=1.250 0.190 0.00377 -0.0063 0.604 0.923 Value15=1.500 0.218 0.00395 -0.0060 0.561 0.932 Value16=1.750 0.245 0.00417 -0.0055 0.511 0.939 Value17=2.000 0.271 0.00442 -0.0051 0.458 0.946 Value18=2.250 0.298 0.00468 -0.0045 0.407 0.952 Value19=2.500 0.324 0.00503 -0.0039 0.338 0.958 Value20=2.750 0.349 0.00538 -0.0032 0.274 0.964 Value21=3.000 0.375 0.00566 -0.0025 0.230 0.969 Value22=3.250 0.400 0.00596 -0.0018 0.184 0.974 Value23=3.500 0.427 0.00629 -0.0013 0.138 0.979 Value24=3.750 0.455 0.00659 -0.0011 0.103 0.983 Value25=4.000 0.484 0.00690 -0.0012 0.072 0.986 Value26=4.250 0.515 0.00723 -0.0017 0.047 0.989 Value27=4.500 0.548 0.00756 -0.0025 0.029 0.991 Value28=4.750 0.582 0.00787 -0.0036 0.020 0.992 Value29=5.000 0.616 0.00816 -0.0046 0.016 0.993 Value30=5.250 0.650 0.00848 -0.0057 0.014 0.994 Value31=5.500 0.685 0.00878 -0.0067 0.012 0.995 Value32=5.750 0.719 0.00919 -0.0076 0.011 0.996 Value33=6.000 0.753 0.00954 -0.0085 0.010 0.997 Value34=6.250 0.786 0.01005 -0.0093 0.009 0.998 Value35=6.500 0.819 0.01049 -0.0100 0.009 0.999 Value36=6.750 0.851 0.01086 -0.0106 0.008 1.000 Value37=7.000 0.871 0.01151 -0.0084 0.007 1.000 Value38=7.250 0.893 0.01189 -0.0067 0.007 1.000 Value39=7.500 0.915 0.01234 -0.0049 0.006 1.000 Value40=7.750 0.936 0.01293 -0.0032 0.005 1.000 Value41=8.000 0.958 0.01375 -0.0016 0.005 1.000 Value42=8.250 0.982 0.01455 -0.0002 0.004 1.000 Value43=8.500 1.007 0.01523 0.0008 0.004 1.000 Value44=8.750 1.027 0.01672 0.0024 0.004 1.000 Value45=9.000 1.045 0.01861 0.0043 0.003 1.000 Value46=9.250 1.059 0.02119 0.0064 0.003 1.000 Value47=9.500 1.067 0.02444 0.0088 0.003 1.000 Value48=9.750 1.067 0.02852 0.0115 0.003 1.000 Value49=10.000 1.057 0.03357 0.0143 0.003 1.000 Value50=10.250 1.035 0.03894 0.0173 0.003 1.000 Value51=10.500 1.006 0.04409 0.0195 0.003 1.000 Value52=10.750 0.978 0.04989 0.0187 0.003 1.000 Value53=11.000 0.954 0.05703 0.0138 0.003 1.000 Value54=11.250 0.932 0.06767 0.0040 0.003 1.000 Value55=11.500 0.904 0.08289 -0.0066 0.003 1.000 Value56=11.750 0.881 0.09272 -0.0127 0.003 1.000 Value57=12.000 0.855 0.10299 -0.0184 0.003 1.000